FL YGTEKNISKA FORSOKSANSTALTEN The Aeronautical Research Institute of Sweden

FF A TN 1990-15

COORDINATES AND CALCULATIONS FOR THE FFA-Wl-xxx, FFA-W2-xxx AND FFA-W3-xxx SERIES OF AIRFOILS FOR HORIZONTAL AXIS WIND TURBINES

by

Anders Bjorck

Stockholm 1990

FlYGTEKNISKA FORSOKSANSTALTEN

The Aeonautical Research Institute of Sweden

Aerodynamics Department

FFA TN 1990-15

Coordinates and Calculations for the FFA-Wl-xxx,

FFA-W2-xxx and FFA-W3-xxx Series of Airfoils for

Horizontal Axis Wind Turbines

by

Anders Bjorck

SUMMARY

Airfoils for use on horizontal axis wind turbines have been designed. The airfoils are divided into three different series:

The first series, FFA-Wl-xxx, constitutes airfoils with thickness to chord ratios from 12.8% to 27. 1%. The design lift coefficients for the FFA-W1-xxx series range from 0.9 for the 12 . 8% airfoil, 1. 05 for a 15 . 2% airfoil to 1. 2 for the 27 . 1% airfoil .

Two airfoils in a second series FFA-W2-xxx are designed with design lift coefficients approximately 0 . 15 units lower than that for the FFA-W1-xxx series .

The third series of airfoils constitutes airfoils with thickness to chord ratios ranging from 19 . 5% to 36%. The 21 . 1% and 19.5% thick airfoils are designed to conform to thinner NACA 63-600 airfoils which are then to be used for the outer parts of the wind turbine blade. The thicker airfoils are designed to offer better aerodynamic performance for a given thickness to chord ratio than thick NACA 63-600 airfoils.

Sponsoring Agency: The National Energy Administration (STEV)

FFA TN 1990-15

CONTENTS

1. INTRODUCTION

2. ANALYTICAL TOOLS

2.1 Comparison with Wind Tunnel Tests

2.2 Application of the Calculalated Airfoil Data to Horizontal Axis Wind Turbines

3 . CHARACTERISTICS OF THE AIRFOILS

Page

5

5

6

8

9

3.1 The 15.2% Thick Airfoils FFA-W1-152 and FFA-W2-152 10

3.2 Thicker Airfoils in the FFA-W1 Series 12

3.3 The FFA-W2 Series 14

3. 4 The FFA-W3 Series 14

4 . COMPARISON WITH OTHER AIRFOILS 15

5 . PRESENTATATION OF DATA OF THE FFA AIRFOILS 17

6. CONCLUDING REMARKS 18

REFERENCES 19

TABLES 22

FIGURES 37-148

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l. INTRODUCTION

A number of airfoils for Horizontal Axis Wind Turbines, HAWTs, have been designed at FFA. The airfoils were initially designed for a 45 meter diameter HAWT. That wind turbine were to be operated at con­stant tip speed ratio and to be power controlled by yawing out of wind. With this rotor in mind the airfoils in the FFA-W1-xxx series were designed. Desirable characteristics of these airfoils are discussed in [1] and [2]. The FFA-airfoils are designed to produce structurally efficient airfoils with a design C1 that is higher than for common general aviation airfoils.

This technical note mainly provides coordinates and calculated drag polars for the FFA-airfoils. A short description is given of the computer programs that were used for the design process and cal­culations, and some of the characteristics of the airfoils are dis­cussed. Only calculated aerodynamic data for the FFA airfoils are presented. A 2-D wind tunnel test of the 15.2% thick FFA-W1-152 airfoil has been carried out and results from this test are pre­sented in [3].

2. ANALYTICAL TOOLS

The airfoil design and analysis codes ISES and XFOIL have been used for the design and analysis of the FFA-airfoils. ISES, developed at MIT by Drela and Giles [4,5], is based on a stream tube Euler equa­tion solver for the inviscid flow field. A two equation boundary layer formulation is used to calculate the boundary layer which is coupled to the inviscid flow field via the boundary layer displace­ment thickness. Boundary layer transition is determined by the en method [5] (n in the en method is designated Acrit) .

The ISES program is capable of calculating small regions of sepa­rated flow. The onset of separation on the airfoil suction side and the accompanying drag increase seem to be relatively well predicted. The de-cambering effect of a thick boundary layer or separation is also represented in the C1/a-curve. For some airfoils and Reynolds numbers even Clmax and stall seems to be rather well estimated.

Mark Drela has recently developed a new program XFO IL. XFOIL uses essentially the same boundary layer formulation as ISES, but the in­viscid flow field is calculated by a linear-vorticity stream func­tion panel method. Transonic flow analysis with shocks is not pos­sible with the panel method of XFOIL but the panel method is ap­preciably faster to run than the streamline Euler method of ISES. Calculations for wind turbine airfoils are well into the subsonic regime were no shocks appear and calculations with XFOIL instead of ISES has offered a considareble reduction in computing time.

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Both ISES and XFOIL have inverse design modes, where the velocity distribution over a part of the airfoil can be changed and the corresponding change in airfoil geometry calculated. XFOIL also has very nice features such as modifying the mean line by adding a �Cp (as function of the chord) to the pressure distribution.

2.1 Comparisons with Wind Tunnel Tests

------- -- -

Evangelista and Vemuru [7] show comparisons between ISES-calculations and wind tunnel results for an EPPLER 387, a NASA NLF (1)-1015 and a NASA NLF (1)-0416 airfoil. Comparisons between ISES-calculations and wind tunnel results for the FFA-W1-152 airfoil are found in [3) .

Results from ISES and XFOIL were checked against wind tunnel results for a number of airfoils. Fig. 1-7 show XFOIL calculations compared with wind tunnel results for three airfoils from the NACA 63-series and a NASA LS (1)-0421 airfoil.

XFOIL calculations were made with free transition and forced tran­sition. In reality transition is affected by such factors as surface quality, free stream turbulence and noise. Correlation with tran­sition studies during low turbulence environments and very smooth wave free surfaces indicate that values of Acrit=14 should be used to represent free flight aircraft conditions. A commonly used value of Acrit seems to be 9, which has been used for all free transition calculations presented in this report.

Fig.l-7 show that the minimum drag level, as calculated by XFOIL, is lower than the values taken from wind tunnel tests. The general characteristics of the drag polar is, however, rather well repre­sented.

In order to carry out comparison of other airfoils with the FFA­airfoils calculations with XFOIL have been made for 15% and 21% thick airfoils from the NASA LS (1) series, the FX 84-W. series and NACA 63-400 airfoils, see paragraph 4. Results with the one airfoil tested in different wind tunnels often show some variation. It therefore seems most just to compare different airfoils tested in the same way, or in this case to compare computations made with the same program using the same boundary layer parameters.

Calculations are also made using fixed transition. This is done in order to simulate a rough leading edge. The effect of roughness around the leading edge is dependent on the severeness, e.g. height, and the extension of the roughness. It is in no way obvious how to simulate roughness in calculations, and what degree of roughness that is to be s imulated. One way of simulating roughness in calcula­tions would be to introduce a jump in the boundary layer momentum thickness in addition to forcing transition. This has been practiced

FFA TN 1990-15 7

by Hill and Garrad [8] and seems sound. However, for the present study only forced transition was used. The transition has been forced at x/c=1% at the suction side and 10% at the pressure side. The desire has been to represent a "worst case" with XFOIL and ISES. As the angle of attack changes, the stagnation point will move around the leading edge. To be sure that the fixed transition position would be downstream of the stagnation point, for the angle of attack range used in the calculations, 10% was choosen at the pressure side and 1% at the suction side. Transition as far forward as 1% might not be realistic and has only been used to represent the mentioned "worst case".

The FFA-W1-152 airfoil has been wind tunnel tested with leading edge roughness. Roughness strips with a height of =0.7 mm at x/c=5% were used on an airfoil that had a 700 mm chord [3]. Results from this test compare rather well with ISES calculations with forced tran­sition at 1% on the suction side and at 10% on the pressure side.

Calculated results with forced transition compared to wind tunnel test results with NACA standard roughness indicate that the detri­mental effect on the drag level of the NACA standard roughness is worse than that of solely tripping the boundary layer. For the 15% thick NACA 63-airfoils a rather sharp suction peak occurs at the leading edge at high angles of attack. The free transition point therefore moves forwards almost to the 1% point for angles of attack around stall. Fixing transition at x/c=1% therefore has very little effect on the Clmax· Other airfoils produce a distinct trailing edge

separation subjected to an increase in angle of attack before a high leading edge suction peak appears. The maximum lift with free tran­sition is then reached with the transition position rearward of the 1% point. The effect of forcing transition at x/c=1% is then large, which is shown in e.g. Fig.8 and 9.

Results are shown for the NASA LS (1}-0421 MOD airfoil in Fig.7. XFOIL calculations are made with fixed transition at x/c=7 % at both the suction and the pressure side. The wind tunnel tests with "roughness on" are made with roughness strips at x/c=7.5% at both sides [10] . This roughness is sized only large enough to provoke transition and not to simulate any heavy insect contamination. The drag increase due to the roughness strip (tripping strip) is rather well captured by XFOIL for this case. This also exemplifies how dif­ferent the effects of the NACA standard roughness and the milder NASA roughness are. A review of the effects of roughness on airfoils has recently been given by Bragg and Gregoreck [12] were the lift loss due to roughness, on a NASA LS (1) -0413 airfoil, is shown to be substantial if tested with more severe roughness.

Fig.7 also shows that the maximum lift and stall characteristics are not correctly represented by the XFOIL calculations. The lift-curve s�ope, dC1/da, decreases as the boundary layer gets thicker and the trailing edge separation progresses forward. This is quite well

FFA TN 1990-15 8

reproduced in XFOIL calculations, e.g. Fig.6. However, the magnitude of dCl/da taken from XFOIL (and ISES) calculations seem to be slightly higher than values obtained from wind tunnel tests. When the separated regions get more extensive and the lift reaches its maximum value or drop (stall) , XFOIL calculations often appear to overestimate lift. In XFOIL, the wake trajectory for a viscous calculation case is taken from an inviscid solution at the same a. This is not strictly correct since viscous effects decrease lift and change the wake trajectory. It is believed that this effect is the cause of the differences shown in Fig.8.

2.2 Application of the Calculated Airfoil Data to Horizontal Axis Wind Turbines

Three-dimensional effects, such as span-wise pressure gradients, centrifugal forces and Coriolis forces will be present on a wind turbine blade. This will result in differences in, e.g., C1max and lift-curve slope. Differences between two- and three dimensional calculations are shown by S0rensen [13], [14]. Experimental work is done in Denmark [15], [16], in the U.S.A [17], [18], in England [19], [20] and in Holland [21]. Work is also currently done at FFA. A 5.35 meter diameter wind turbine has been wind tunnel tested in a large wind tunnel at CARDC in China [22]. One of the blades were equipped with 232 pressure taps so that Cp/x recordings could be

obtained for 8 different radial stations. This blade has recently been tested during non-rotating conditions at FFA. Results from this test will be used to obtain quantitative and qualitative differences in e.g. C1 between the rotating and non-rotating case.

It seems to be well established that C1max is increased for the inner parts of the blade. Results from Madsen and Rasmussen [16] indicate highly reduced lift-curve slope and C1max towards the tip.

The angle of attack in these data is derived from blade element­/momentum methods (Strip methods) . The change in lift-curve slope between 2-D and 3-D data can therefore very well be originating from an incompleteness in the estimation of the angle of attack by the blade element/momentum method. Results from [18] show results from tests with a rectangular untwisted blade equipped with the S809 airfoil developed at SERI [23]. Pressure measurements were made at the 80% radius station of the blade and the local angle of attack was measured by a wind vane ahead of the blade. These measurements were compared to 2-D tests and relatively good agreement is shown between the 2-D and 3-D case.

Many of the studies of 3-D effects are only yet in the sta�ting phase and reliable data are still to be awaited. In the light of the differences in, e.g., C1max between the 2-D case and the 3-D the uncertainty in C1max as predicted by XFOIL and the differences

between XFOIL- and ISES calculations seem to be of less importance. For the FFA-W1 airfoils and the FFA-W2-152 airfoil calculations with ISES are made. Differences in C1max between ISES and XFOIL calcula-

FFA TN 1990-15 9

tions are shown in Fig.31-36. It is believed that ISES calculations are more reliable. However, calculations at these high angles of at­tack must be viewed upon with somewhat critical eyes. For the thick­est airfoils the uncertainty is the greatest, but then again, the uncertainty about the differences between 2-D data and 3-D data is large for the root region.

No attempts are made to make corrections to the polars so that they apply to the 3-D case of a wind turbine.

Further uncertain data are Cm. The calculated values of Cm drop (the absolute values) when the trailing edge separation progresses for­ward. This is seen in, e.g., Fig.3 where the pitching moment drops from =-0.08 for attached flow to =-.04 for high angles of attack. Cm

taken from the wind tunnel test show the opposite trend. This drop in Cm which seems to be present of all XFOIL (and ISES) calculations

of the FFA-airfoils and must be considered to be unrealistic.

At high angles of attack the Cct values must also be viewed with some

caution.

-3 . CHARACTERISTICS OF THE AIRFOILS

Airfoils are designed with varying thickness to chord ratios re­flecting the need for different stations on the blade.

The helix angle is small for the outer parts of the blade (the lift vector is directed almost perpendicular to the turbine plane) and the L/D ratio is of utmost importance. As the helix angle gets larger towards the root, the L/D ratio gradually looses importance. Towards the root there is instead, for structural resons such as high cross section height and reasonably small chords, a need for thick airfoils for operation at high lift coefficients.

The FFA-W1 series is designed with best L/D ratios at rather high lift coefficients. However, the 12.8% percent thick airfoil designed for the blade tip has a slightly lower design c1 than the 15.2% thick airfoil. The reason why the tip airfoil has a lower design C1

is mainly the following: If the blade is given, e.g., a linear taper plan form, then the local lift coefficient should, for optimum performance decrease towards the tip. Also, airfoil drag with a rough leading edge would be higher if the airfoil were designed for a higher design C1, and low drag is of highest importance at the

blade tip wher the helixangle is small and the velocities are large.

The underlying specifications set up for the design of the FFA-W1 and FFA-W2 airfoils are described in [2) and a full discussion of the airfoil characteristics will therefore not be given here.

FFA TN 1990-15 10

3. 1 The 15.2% Thick Airfoils FFA-W1-152 and FFA-W2-152

The 15. 2% thick airfoils FFA-W1-152 and FFA-W2-152 are designed to have high L/D ratios. High L/D ratios are easiest attained by a rel­atively high C1 design. It is the product C1*C that is the important

characteristic at each blade radius of a wind turbine. Designing the blade for a lower C1 therefore results in larger chords. Larger chords give larger Reynolds numbers which favours the L/D ratio. Also, if the cross section height of the blade is kept constant, the relative thickness decreases with design C1 and thinner airfoils generally have lower drag. Together this makes L/D a rather weak function of design cl.

The choice of design C1 can therefore be made on structural consid­

erations. To support the blade designer with airfoils optimized at different design C1 the aim has been to design different series of airfoils characterized by the best L/D at different C1. So far only a 15. 2% and 21% thick section is designed in the lower C1 design

series FFA-W2-xxx.

If a blade element/momentum method is used to obtain optimum chord and twist distribution it is in fact the product C1*C that is determined at each blade radius. A large chord can be choosen if a low design C1 is choosen, or the chord can be decreased if the design C1 is increased (more cambered airfoils or local twist towards a higher angle of attack) . Different choises of design C1, i. e. design angle of attack, for the same airfoil will result in different values of the local blade chord, which will result in dif­ferent Reynolds numbers for the design case ( Wind speed and tip speed ratio) . Therefore, calculations should be carried out at con­stant C1*C for determination of at what lift coefficient best L/D

will be obtained for a given airfoil for use on horizontal axis wind turbines.

Fig. 10 and 11 show calculations for the 15. 2% thick airfoils at both constant Re, and with Re varying inversely with C1. It is seen that by making the the calculations at constant C1*c; i. e. at constant C1*Re, in comparison to a constant Re, the angle of attack range for a given high L/D is increased. Fig. 12 shows that a high L/D can be achieved both for the lower design C1 of the FFA-W2 airfoil as well as for the FFA-Wl airfoil. Fig. 13 shows both airfoils plotted superimposed on each other. (The design c1 for the FFA-W2 airfoils can not be characterized as low, but their design C1 is lower than that for the FFA-W1 airfoils)

If airfoil surfaces are sufficiently smooth, the laminar boundary layer will undergo separation in the adverse pressure gradient before transition occurs. Transition then occurs in the free shear layer and a transitional bubble is formed. This is the normal way transition occurs at airfoils at low Reynolds numbers (Re less than

FFA TN 1990-15 11

= 5 million) . The main problem with this bubble is the associated drag increase. This drag increase is proportional to the height of the bubble (B*) and the magnitude of the pressure jump at the rear part of the bubble where reattachment occurs (see e.g. [5] and [25]) .

For the thinner FFA-airfoils, where low drag is important, an "instability range" has been incorporated on the airfoil suction side. An instability range is a region of weak adverse pressure gradients that will promote the growth of boundary layer instability and transition, but were the gradients are small enough to avoid laminar separation. The "instability range" on the 15% airfoils are designed to minimize drag at Reynolds numbers of the order of 3 mil­lions. The instability range is rounded off at the aft part but ex­tends some distance beyond the point of laminar separation. In this way the pressure jump at the rear of the bubble, and thus the drag increase, will be kept small even if transition does not occur before separation. If the Reynolds number is decreased, the length of the laminar bubble will increase, and the pressure jump will be larger and cause a drag penalty. For the smooth surface condition of the airfoil, this effect sets the lower Re range for the airfoil to Re=2 million.

One purpose was to design the 15.2% thick airfoils so that high L/D ratios can be realised. Operational experience with wind turbine blades, however, indicates that the problem with too long transit­ional bubbles will not be the primary problem. Surface manufacturing irregularities, erosion of the leading edge, or the accumulation of dirt or insects are likely to cause premature transition. A study of the effects of different L/D ratios on the power coefficient [2], shows the utmost importance of an airfoil for which the degradation of the L/D ratio with, e.g., a rough leading edge is kept to a minimum. Care is therefore taken to give the airfoils good, or at least acceptable, performance as "rough airfoils".

The lower surface is designed so that =90% laminar flow should be achievable if the surface is smooth. The upper surface is designed with a roof top followed by the "instability range'' and a main pres­sure recovery to the trailing edge pressure. The length of the roof top is, however, matched in such a way that even if the boundary layer is subj�ct to premature transition and thickening due to a rough surface, the pressure recovery should be mild enough to avoid boundary layer separation for lift coefficients =0.1 units above the design lift coefficient. It is believed that this gives the best combination of high L/D due to laminar flow for the smooth surface case, and acceptable L/D with rough surfaces.

It is possible that better rough airfoil performance can be achieved if the airfoil is given more aft loading like e.g. a NACA 63-615 (a=l.O) airfoil. Introducing a certain aft loading will decrease the

velocity level of the roof top and reduce the average adverse pres-

FFA TN 1990-15 12

sure gradients. This is however incompatible with the requirements originally set up for design of the =15% thick FFA-airfoils to keep Crn more positive than =-0.06 (see [2]) .

The FFA-Wl-152 is designed for a higher design C1 than the NACA 63-615 airfoil. However, C1rnax is kept at the same level as, e.g., the NACA 63-615. The relative drop in C1rnax between smooth and rough airfoil is attempted to be kept as small as possible for the thinner FFA airfoils.

Care was also taken to avoid too abrupt stall characteristics. The pressure recovery has therefore been formed to have the shape param­eter, H, gradually increasing. It is hoped that this will lead to a separation gradually moving forward. A Stratford type of pressure recovery ( with a constant value of H) has been avoided. It is also likely that the existence of a roof top introduces gentler stall characteristics. This is seen for e.g. the NASA LS (l) and NASA LS (1) MOD airfoils [10] . The modification of the NASA LS (l) to obtain the MOD airfoil consisted in reducing the magnitude of the adverse pres­sure gradients aft of a roof top at C1=0.4. This modification en­hanced the L/D ratio at moderate to high lift coefficients (=C1>0.6)

and at low Re, but it also made the stall more abrupt. The adverse pressure gradients aft of the kink at x/c=0.5 is detrimental in the way that trailing edge separation starts at rather low angles of attack. However, the somewhat milder gradients in front of the kink sees to it that the separation movement is not too rapid and a gentle stall is obtained. For the modified airfoil, almost fully attached flow for angles of attack up to C1rnax is realised. Increas­

ing the angle of attack further however leads to a rather quick movement of the separation point to x/c=0.4 and a substantial loss in lift. Comparisons between the NACA 23015, which also lacks a roof top and a kink at higher a, and e.g 15% thick NACA 6-series airfoils also confirm that a roof top type of velocity distribution is favourable in order to avoid an abrupt stall.

The estimated C!rnax level from calculations and a rather constant

post stall lift level were confirmed during the wind tunnel test of the FFA-Wl-152 airfoil [3] , which is shown in Fig.9. (The airfoil that was wind tunnel tested is designated AK15v4, but is essentially the same airfoil as FFA-Wl-152.)

3. 2 Thicker Airfoils in the FFA-W1 Series

Airfoils with thickness to chord ratios up to 27. 1% have been de­signed in the FFA-Wl series. (The airfoils in the FFA-W3 series are used for thicker airfoils and the =21%, 24% and 27% airfoils from the FFA-W3 series can in principle replace the airfoils with equiva­lent thickness in the FFA-Wl series. ) The design C1 has been in­creased from 1.05 for the 15. 2% thick section to C1 design =1. 2 for

the 21. 1% thick section. For the thicker sections the objective has been to achieve as high as possible L/D with a rough surface.

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There exist several series of airfoils with varying thickness to chord ratios, such as e. g. the NACA 4-,5- and 6 digit series [9] , the NASA LS series [10] and the FX 84 series [24] . Varying thicknesses for these airfoils are in principle achieved by scaling the coordi­nates around the mean camber line. For airfoils with a t/c ratio of say 15% it is the suction side of the airfoil that is critical to boundary layer separation. If these airfoils are thickened by adding equal thickness on both the upper and lower side of the mean line, then equal thickness induced velocities are added on both the suc­tion and pressure sides of the airfoil. The increased maximum velocities and adverse pressure gradients on the pressure side do not normally introduce separation problems. However, the addition­ally increased adverse pressure gradients on the suction side are quite harmful. The margin to separation will be decreased and the drag rise will start at rather moderate lift coefficients, especially if the boundary layer is subject to premature transition. This behaviour is shown for all NACA airfoils and also for the FX 84 airfoils. The NASA LS (1) MOD airfoils show acceptable performance for t/c ratios up to 21%.

With modern design codes for airfoils it is easy to view the airfoil as an upper and lower side with corresponding velocity distribu­tions. Fig. 14 shows the FFA-W1 airfoils plotted superimposed on each other. It is assumed that the maximum thickness is warranted for x/c positions around 0.3. The thickness distribution is such that an ellipsoid like shaped beam, centred at x/c�0. 3 will fill much of the airfoil. The thickness has been added mainly to the lower surface to avoid increasing the maximum velocity and adverse pressure gradients on the airfoil suction side too much. On the upper surface the thickness has been moved forward to reduce the adverse pressure gradients further.

Variation of the geometry:

Calculations were made with slightly different geometries. The starting position of the pressure recovery on the suction side was varied and it seemed as if the best L/D ratios, especially with premature transition, were obtained with the shortest possible roof top. A gentle stall is hoped to be obtained anyway for the thicker airfoils (t/c>21%) . The stall characteristic requirements are also assumed to be lower towards the blade root.

In order to compensate for the loss in lift due to the low pressure at the maximum thickness position on the pressure side, the airfoils are given more aft loading.

If too much thickness is added to the upper side, this will cause too early separation on the suction side. Adding too much thickness to the lower side, together with the relatively aft back maximum thickness position on the lower side, will increase the adverse

FFA TN 1990-15 14

pressure gradients on the lower side too much. This will result in lower surface separation at low angles of attack as indicated in Fig.15b.

When an angle of attack range, in which the airfoil is to operate, is defined the aim is that the margin to separa�ion on the lower surface side at low angles of attack should be about the same as the margin to separation on the upper surface at high angles of attack. This is one basic idea of the design of the thick FFA-airfoils

The adverse pressure gradients on the lower side will be rather large for the thicker FFA-airfoils. If the airfoil surface is smooth enough the laminar separation bubble can be relatively thick since no sufficient instability range is present on the pressure side of the thicker airfoils. One risk, that is not verified, is that a laminar bubble will be an undesirable noise generator. This together with the separation risk at low angles of attack with a rough leading edge led to the differences between the �24% and 27% thick airfoils of the FFA-W3 and the equivalent airfoils of the FFA-W1 series. The adverse gradients on the lower side has been relaxed somewhat for the FFA-W3 series airfoils. Moving the maximum thick­ness forward on the lower side would also reduce the magnitude of the pressure gradients there. This would, however, reduce the building height of the airfoil around x/c�0.3.

3.3 The FFA-W2 Series

The objective was to design different series of airfoils with dif­ferent design C1, something like the NACA 6-series of airfoils. The FFA-W2-152 is designed with a lower design C1 than the FFA-W1-152 airfoil. The W2 airfoil is also designed to have a lower Clmax than

the W1 airfoil. The FFA-W2-210 airfoil is designed to have a lower design C1 and lower C1max than FFA-W1-211. No further airfoils are

yet made in this series. However, such airfoils can be made rela­tively easily by reducing the camber of the FFA-W1 airfoils.

3.4 The FFA-W3 Series

The NACA 63-615 and 63-618 airfoils are believed to have rather good performance'both as rough and smooth airfoils. The NACA 63 airfoils were considered during a study of a pitch regulated turbine with de­mands on slightly lower C1 design of the thinner airfoils than the

FFA-W1-152 and FFA-W1-182 have. For a pitch regulated turbine it seems that the requirements put up for the thinner FFA-W1 and FFA-W2 airfoils such as to have the stall to occur at C1max rather close to the design C1 is not applicable. Instead it is desirable to have a certain margin to C1max in order to avoid the situation were most of

the blade has angles of attack above stall. Pithing out of wind then increases power, which is the opposite of the normal operation mode of the regulation system.

FFA TN 1990-15 15

As the thickness is increased the rough airfoil performance of the NACA 6-series airfoil declines. An improvement in performance is be­lieved to be attainable if airfoils of the FFA-W1 type are used instead of scaling up NACA 63-600 airfoils to large thicknesses. If airfoil surfaces are perfectly smooth the difference might be small or even favouring the NACA airfoils of t/c around 21-25%. But if the airfoil surfaces are rough or if premature transition occurs, then the upper side boundary layer of the the NACA airfoils are likely to separate at too low angles of attack. This will cause high drag levels but also a highly reduced C1max·

The FFA-W1-211 airfoil was slightly modified to better conform to the thinner NACA 63-618 airfoil. The airfoil was given more aft loading and designated FFA-W3-211. Calculations with XFOIL give the FFA-W3-211 slightly higher Clmax than the corresponding FFA-W1 air­

foil. The =24% and 27% thick FFA-W3 airfoils have slightly more cam­ber than the corresponding FFA-W1 airfoils. The adverse pressure gradients aft of maximum thickness on the lower side are somewhat reduced. The FFA-W3 airfoils have slightly larger pitching moment coefficients.

The three 30% to 36% thick airfoils are made in such a way that an ellipsoid like shaped beam centred at x/c=0.3 is surrounded by, what is believed to be, an aerodynamic shape as advantageous as possible. The airfoils are given a finite thickness at the trailing edge since this is thought to enhance performance at high C1. The upper side consists of almost a straight line aft of x/c=0.65 (it can be made straight without changing the aerodynamics noticeably) . The lower side sho�ld be given a downwards pointing trailing edge, which could be made more marked than for the the given airfoil coordinates if "low" drag at high C1 is wanted. Results with e.g. "gurney'' flaps

[26] and split flaps contra plain flaps [9] indicate that a finite trailing edge thickness and a downwards pointing lower trailing edge should be favourable for thick wind turbine airfoils.

A 19.5% thick airfoil, FFA-W3-195, is produced by interpolating the mean lines and thickness distributions of the FFA-W3-211 airfoil and a NACA 63-618 (a=1.0) airfoil. (Actually, the original NACA airfoil coordinates were rotated 0. 3° anti-clock wise before the inter­polation, so that the leading edges of the NACA airfoil better should conform to the 21% thick FFA airfoil.)

4. COMPARISON WITH OTHER AIRFOILS

Calculations with XFOIL were done for a number of =15% thick and =21% thick airfoils. Beside the FFA-W1 airfoils the NACA 63-600, the NASA LS (1) and the FX 84 airfoils were choosen for a comparison.

The FX 84 series has good performance with smooth surfaces and gentle stalling characteristics but has poor performance with leading edge roughness. Especially for the 21% thick section the

FFA TN 1990-15 16

drag increase and loss in lift due to premature transition is marked.

The NACA LS (1) MOD airfoils have good performance with premature transition1 but has a very high C1max and sharp stall charac­teristics. Performance with smooth surfaces is rather modest.

The thinner NACA 63 airfoils are rather good airfoils both with smooth surfaces as well as with a roughened leading edge2• However, the performance with a rough leading edge decline as the thickness to chord ratios grow.

For the SERI airfoils [23] and the airfoils developed in England [8] no coordinates were available.

Calculations were done at Re=3 million with free transition and with fixed transition. Transition was fixed at x/c=1% at the suction side and at x/c=10% at the pressure side for the fixed transition case. All calculations were done at a Mach number of 0.15. The results are shown in Fig.16 and 17. Airfoil coordinates were obtained for an FFA-airfoil by taking 50% of the FFA-W1-211 and 50% of the FFA-W1-242 airfoil coordinates. This airfoil is considered to be more structurally equal to the =21% thick NASA, FX and NACA airfoils to which it is aerodynaically compared than the somewhat thinner FFA­W1-211 airfoil. The =21% thick airfoils are shown in Fig.18.

From Fig.16 it is seen that the FFA-W1-152 airfoil has the best L/D ratio for the free transition case. This is much due to the high value of C1 for which it is optimized. The FX airfoil has good per­formance with free transition. However, as the transition is fixed at x/c=1% at the suction side there is a substantial drag increase and substantial loss in lift for C1 greater than =0.7.

Fig.17 shows that the =22% thick FFA airfoil in comparison to the other airfoils have favourable performance at high lift coefficients with fixed transition. With free transition and for lift coef­ficients below unity the NACA and FX airfoils have lower drag than the FFA airfoil, but with fixed transition these airfoils have a substantial drag increase and loss in lift due to boundary layer separation on the suction side. The highest C1max value with fixed

transition is also indicated for the FFA airfoil.

1 If comparisons with airfoils tested in [9] are done it should be observed that the roughness used in wind tunnel tests of the LS airfoils [10] is not as severe as the NACA standrad roughness [9].

2 Hill & Garrad [8] come to the conclusion that the NACA 63 or 64 airfoils are hard to improve upon for the design of a low lift tip airfoil.

FFA TN 1990-15 17

5. PRESENTATION OF DATA OF THE FFA AIRFOILS

Data is presented in the following way:

1. Figures of the airfoils. (Fig.18-22)

2. Inviscid Cp distributions for the airfoils at lift coefficients C1=0 to C1=1.8. For each airfoil the Cp distribution is dis­

played for an inviscid case. An angle of attack close to design C1 is choosen for these calculations. The dashed curves show the inviscid Cp distribution and the full curves show the viscous Cp distributions. (Fig. 25-27)

3. Drag polars calculated with XFOIL and ISES. Each page consists of three plots. In the left plot the drag coefficient, Cct, is plotted versus the lift coefficient, C1. In the middle plot C1 and the pitching moment coefficient, Cm, is plotted versus the

angle of attack, a. In the right plot the transition position is plotted on the x-axis and c1 on the y-axis.

The different calculated cases are named in the following way: POL.Airfoil_rr_tt or POLAR.Airfoil_rr_tt. The Reynolds number is indicated by two digits where rr=Re*10-5• The number or letters tt indicate the transition mode. tt=9 means free transition with Acrit=9, tt=TU1 means that transition has been forced at x/c=1% at the suction side and x/c=10% at the pressure side (Xtrs=0.01 and Xtrp=0.1) . POL stands for XFOIL calculations and POLAR stands for ISES calculations. All calculations are made at a Mach number of 0.15.

The designation for the airfoils in the FFA-W1 series is a Wxxx, where xxx is the thickness number for the airfoil. For the FFA­W2 airfoils the designation is W2-xxx and for the FFA-W3 series the designation is W3-xxx.

4. Airfoil coordinates

5. Data for the calculated polars in digit form (contrary to plot­ted form) submitted in appendix.1

Drag polars are calculated only for Re=1,2 and 3 million. The air­foils are designed for the Reynolds number regime above Re=2 million and upwards. From a boundary layer separation point of view the lowest Reynolds numbers are the most critical. As the Reynolds number increases the drag decreases and C1max is possibly increased.

In order to reduce the number of calculations to be made, it was considered as most important to do the calculations at Reynolds num­bers up to Re=3 million.

Fig 26 shows the lift/drag ratio versus the lift coefficient for the FFA-W1 airfoils at Re=3 million. The calculations are made with

FFA TN 1990-15 18

XFOIL for both free transition and with fixed transition. Fig 27 shows a comparison between the 15.2% and 21.1% thick FFA-Wl airfoils and the FFA-W2 airfoils at Re=3 million.

Fig.28 and fig.29 show drag polars for the FFA-W1 airfoils at Re=3 million with the polars for all airfoils plotted in the same diagram.

Fig.30-35 show polars for the FFA-W1 airfoils

Fig.36-37 show polars for the FFA-W2 airfoils

Fig.38-45 show polars for the FFA-W3 airfoils

6.CONCLUDING REMARKS

The two-dimensional analysis and design codes ISES and XFOIL [4], [5], [6] have been used for the design of a number of airfoils

for wind turbine applications.

The first series, FFA-W1-xxx, constitutes airfoils with thickness to chord ratios from 12.8% to 27.1%. These airfoils are designed with a relatively high design lift coefficient. This will meet the require­ments for e.g. wind turbines designed for low tip speed ratios. The thinner airfoils are designed with requirements that high lift/drag ratios be realized with smooth surfaces and laminar flow, but with the constraint that good performance should be achieved even with a rough leading edge with insect contamination or/and manufacturing irregularities. The thicker airfoils are designed to overcome the weakness of high drag and low C1max that thick airfoils commonly

exhibit with rough leading edges. Calculations with XFOIL indicate that the rough airfoil characteristics of the 21.1% thick FFA-air­foil is superior to the NASA LS(1) -0421 MOD, the NACA 63-621, and the FX 84-W-218 airfoils. A wind tunnel test of the 15.2% thick air­foil has been carried out in which much of the computed performance was verified.

A 15.2% and a 21.1% thick airfoil have been designed with the same requirements as the FFA-Wl-xxx airfoils, but with a slightly lower design lift coefficient.

The FFA-W3 series has been designed to provide airfoils for pitch regulated turbines. The FFA-W3 series include airfoils with thick­ness to chord ratios up to 36%. A 19.5% thick airfoil have been made to conform with a 18% thick NACA 63-618 airfoil. It is assumed that NACA 63-6xx airfoils are used for thickness to chord ratios below 18%.

FFA TN 1990-15

REFERENCES

[ 1]

[ 2]

[ 3 ]

[ 4]

[ 5]

[ 6]

[7)

[8]

[9]

Bjorck, A.

Bjorck, A.

Bjorck, A.

Giles, M.B. Drela, M.

Drela, M. Giles, M.B.

Drela, M.

Evangelista, R. Vemuru, C.S.

Hill, D.C. Garrad, A.D.

Abbott, I.H. von Doenhoff, A.E.

[10] McGhee, R. J. Beasley, W.D.

19

"Airfoil Design For Horizontal Axis Wind Turbines", Symposium proceedings, IEA 2nd symposium on Aerodynamics of Wind Turbines.,Lyngby,Copenhagen,Denmark,October 1988

"Airfoil Design for Variable RPM Horizontal Axis Wind Turbines", Conference proceedings, EWEC'89, European Wind Energy Conference and Exhibition. Glasgow, Scotland, July 1989. Also FFA TN 1990-02

"Two-Dimensional Wind Tunnel Test and Comparison with Calculations for a 15.2% Thick Airfoil Section for Wind Turbines", FFA TN 1990-16

"Two-Dimensional Transonic Aerodynamic Design Method" AIAA Journal,Vol.2 5, No9, September 1987.

"Viscous-Invicsid Analysis of Transonic and Low Reynolds Number Airfoils.", AIAA Journal , Vol.2 5, NolO, October 1987.

"XFOIL documentation" Documentation received with the XFOIL-program, November 1988

"Evaluation of an Analysis Method for Low­Speed Airfoils by Comparison with Wind Tunnel Results. AIAA paper 89-0266, presented at 27th Aerospace meeting, January 1989, Reno, Nevada

"Design of Aerofoils for Wind Turbine use" Conference proceedings, EWEC'89, European Wind Energy Conference and Exhibition. Glasgow, Scotland, July 1989

Theory of Wing Sections, Dover Books 1959

"Wind-Tunnel Results for an Improved 21-Percent Thick Low-Speed Airfoil Section." NASA Technical Memorandum 78650, April 1978

FFA TN 1990-15

[11] Miley, S. J.

[12] Bragg, M. B. Gregorek, G. M.

[13] S0rensen, J. N.

[14] S0rensen, J. N.

[15] Madsen, A. H. Rasmussen, F.

[16] Madsen, A.

[17] Butterfield, C. P.

[ 18 ] Mus i a 1 , W . D . Butterfield, C. P. Jenks, M.D.

[19] Brown, C.J. Graham, J. M.R.

20

"A Catalog of Low Reynolds Number Airfoil Data for Wind Turbine Applications", Department of Aerospace Engineering, College Station, Texas, U. S. A. , 1982

"Environmentally Induced Surface Roughness Effects on Laminar Flow Airfoils: Implications for Flight Safety", AIAA paper 89-2049, Presented at AIAA/AHS/ASEE Aircraft Design, systems and Operations Conference, July 1989, Seattle, Washington

"A new Computational Model for Predicting 3-D stall", Symposium proceedings, IEA 1st symposium on Aerodynamics of Wind Turbines, October 1986, London, England

"Some Physical and Numerical Aspects of Wind Turbine Aerodynamics", Symposium proceedings, IEA 2nd symposium on Aerodynamics of Wind Turbines. , November 1988, Lyngby, Copenhagen, Denmark

"Derivation of Three-Dimensional Airfoil Data on Basis of Experiment and Theory", IEA 2nd symposium on Aerodynamics of Wind Turbines. , November 1988, Lyngby, Copenhagen, Denmark

"Measured Airfoil Characteristics of Three Blade Segments on a 19 m HAWT Rotor", 1989, Ris0 National Laboratory, DK-4000 Roskilde, Denmark

"Three-Dimensional Airfoil performance Measurements on a Rotating Wing", Conference proceedings, EWEC'89, European Wind Energy Conference and Exhibition. Glasgow, Scotland, July 1989

"A comparison of the Two- and Three dimensional S809 Airfoil Properties for Rough and Smooth HAWT Rotor operation", Ninth ASME Wind Energy Symposium, January 1990

"The Effect of Turbine Rotation on Maximum Lift Coef ficient", Conference proceedings, EWEC'89, European Wind Energy Conference and Exhibition. Glasgow, Scotland, July 1989

FFA TN 1990-15

[20] Barnsley, M.J. Wellicome, J.F.

[21] van Bussel, G.

[22] Ronsten, G. et. al.

[23] Tangler, J.L. Somers, D.M.

[24] Althaus, D.

[25] Drela, M,

[26] Liebeck, R.H.

21

"Design and Testing of a Horizontal Axis Wind Turbine Model for the Investigation of Stall Regulation Aerodynamics", Conference proceedings, EWEC'89, European Wind Energgy Conference and Exhibition. Glasgow, Scotland, july 1989

Contribution presented at IEA 2nd symposium on Aerodynamics of Wind Turbines., November 1988, Lyngby, Copenhagen , Denmark

"Pressure Measurements on a 5.35 m HAWT in CARDC 12*16 m Wind Tunnel Compared to Theoretical Pressure Distributions", Conference proceedings, EWE C'89, European Wind Energy Conference and Exhibition. Glasgow, Scotland, July 1989

"Status of the Special-Purpose Airfoil Families.", SERI/CP-217-3315, Conference proceedings, WINDPOWER'87, San Fransisco, U.S.A., 1987

"Polarmessungen an den profilen .... ", 12th meeting of experts-aerodynamic calculation methods for WECS, Copenhagen, Denmark, 1984

"Low-Reynolds-Number Airfoil Design for the M.I.T. Deadalus Prototype: A case study", Journal of Aircraft, Vol. 25, No 8, August 1988.

"On the Design of subsonic Airfoils for High Lift", AIAA paper 76-406, AIAA 9th Fluid and Plasma Dynamics Conference, San Diego, California, July 1976

FFA TN 1 9 9 0 - 1 5 22

TABLE 1 . Profile coordinate s .

A i r foi l : FFA-W1-12 8

x/c

0.0 0 0 0 6 0.0 013 2 0 .0 0 5 0 8 0.0 113 4 0.02 0 0 6 0.0 312 1 0.0 4 4 7 1 0.0 6 0 5 2 0.0 785 6 0 .0 987 3 0.12 0 95 0.14 510 0.17 10 7 0.1987 4 0.2 2 7 9 7 0.2 5862 0.2 9 0 5 5 0 .3 2 3 61 0.3 5 7 6 2 0.3 92 4 4 0 .4 2 789 0 .4 6 3 80 0 .5 0 0 0 0 0 . 5 3 6 3 3 0.572 5 9 0.6 086 3 0.64 4 2 6 0 .6 7 9 3 2 0 .7 13 6 3 0 .7 4 7 0 4 0.7 7 9 3 8 0 .810 5 0 0 . 84 0 2 5 0 .86848 0 . 895 0 7 0 . 9 1 987 0 . 94 2 7 8 0 . 9 63 68 0 . 982 4 8 0 . 9 9 9 0 8

yu /c

0 .0 0 111 0 .0 0 5 7 3 0.012 5 0 0 .019 6 7 0.0 2 7 17 0.0 3 4 9 4 0 .0 4 284 0.0 5 0 7 6 0.0 5860 0 .0 6 62 3 0 .0 7 3 5 3 0 .080 3 9 0.086 6 7 0.0 9 2 2 3 0 .0 9 6 9 6 0.10 0 7 4 0 .10 344 0 .10 4 91 0.10 5 0 7 0.10 386 0.10131 0.0 9 7 51 0 .0 92 5 9 0 .086 7 6 0.0 8 0 2 0 0.0 7 3 12 0.0 6 5 7 3 0 .0 582 0 0 .0 5 0 6 9 0 .0 4 3 3 7 0 .0 3 6 3 6 0.0 2 978 0 .0 2 3 7 3 0 .018 2 9 0 .0 1 3 5 3 0 . 0 0 95 0 0 .0 0 62 1 0 .0 0 3 6 6 0 .0 0183 0 .0 0 0 7 6

yl /c

0.0 0 111 -0 . 0 0 4 4 3 -0.0 0832 - 0.01190 -0 .014 9 9 -0 .017 5 3 -0.019 62 -0.02132 - 0.0 2 2 6 4 -0 .0 2 3 6 0 -0.0 2 4 2 7 -0.0 2 4 6 5 -0.0 2 4 7 7 -0 .02 4 6 6 -0.0 2 4 3 6 -0.0 2 3 91 -0.0 2 3 3 3 -0 .0 2 2 6 3 -0.0 218 4 -0.0 2 0 9 6 -0.0 2 0 0 4 -0 . 019 0 8 -0 .0180 9 -0.017 0 4 -0.0 1 5 9 5 -0.014 81 -0 .01363 -0.012 4 1 -0.0 1 112 -0 .0 0 9 7 6 -0.0 0 83 7 -0.0 0 6 98 - 0 .0 0 5 61 - 0.0 043 0 -0 . 0 0 315 - 0 . 0 0 2 2 0 -0 .0 0148 - 0.0 0 10 1 -0.0 0 0 7 8 - 0 .0 0 080

FFA TN 1 9 9 0 - 1 5 2 3

TABLE 2 . Profile coordinates .

Ai r foi l : FFA-W1-15 2

x/c

0 . 0 0 0 0 0 0 . 0 012 6 0 . 0 0 5 0 3 0 . 0 1 1 3 0 0 . 0 2 0 0 3 0 . 0 3118 0 . 0 4 4 7 0 0 . 0 6 0 5 2 0 . 0 7 85 7 0 . 0 987 7 0 . 12101 0 . 14 518 0 . 17 118 0 . 19888 0 . 2 2 814 0 . 2 5 882 0 . 2 9 0 7 8 0 . 3 2 386 0 . 3 5 7 91 0 . 3 9 2 7 6 0 . 4 2 82 5 0 . 4 6 419 0 . 5 0 0 4 3 0 . 5 3 6 7 9 0 . 5 7 3 0 9 0 . 6 0 9 1 7 0 . 6 4 4 83 0 . 6 7 9 92 0 . 7 14 2 7 0 . 7 4 7 7 1 0 . 780 0 9 0 . 8112 4 0 . 84 10 1 0 . 86 92 7 0 . 89 5 88 0 . 92 0 7 1 0 . 94 3 6 4 0 . 9 64 5 7 0 . 983 3 8 1 . 0 0 0 0 0

yu l e

0 . 0 0 0 0 0 0 . 0 0 6 6 6 0 . 0 1 4 16 0 . 0 2 2 3 9 0 . 0 310 2 0 . 0 3 988 0 . 0 4 886 0 . 0 5784 0 . 0 6 6 68 0 . 0 7 52 6 0 . 083 4 4 0 . 0 9110 0 . 0 9810 0 . 10 4 31 0 . 10 9 58 0 . 1 13 7 2 0 . 11 6 6 2 0 . 11818 0 . 1183 7 0 . 1 17 11 0 . 114 3 2 0 . 1 10 0 6 0 . 10 4 5 7 0 . 0 9810 0 . 0 9 0 88 0 . 0 83 10 0 . 0 7 4 9 7 0 . 0 6 6 67 0 . 0 5 838 0 . 0 5 0 2 8 0 . 0 4 2 4 9 0 . 0 3 5 1 3 0 . 0 2 83 0 0 . 0 2 2 1 2 0 . 0 1 6 65 0 . 0 1 1 9 4 0 . 0 0 80 3 0 . 0 0 4 92 0 . 0 0 2 5 8 0 . 0 0 0 98

yl /c

0 . 0 0 0 0 0 - 0 . 0 0 5 5 2 -0 . 010 0 2 -0 . 0 1 380 -0 . 017 17 -0 . 0 2 0 1 6 -0 . 0 2 2 7 6 -0 . 0 2 4 9 9 -0 . 0 2 6 9 3 -0 . 0 2 861 -0 . 0 3 0 0 6 -0 . 0 312 8 -0 . 0 3 2 2 9 -0 . 0 3 3 0 8 - 0 . 0 3 3 6 7 -0 . 0 3 4 0 4 -0 . 0 3 4 2 2 -0 . 0 3 4 16 -0 . 0 3 388 -0 . 0 3 3 3 7 -0 . 0 3 2 6 3 -0 . 0 3167 -0 . 0 3 0 4 7 - 0 . 0 2 9 0 3 -0 . 0 2 7 3 5 -0 . 0 2 5 4 8 -0 . 0 2 3 4 1 -0 . 0 2 1 1 2 -0 . 0 1 865 - 0 . 0 1 6 0 5 - 0 . 0 1 3 4 1 -0 . 0 1 0 82 - 0 . 0 0 84 1 -0 . 0 0 62 6 - 0 . 0 0 4 4 2 -0 . 0 0 2 9 4 -0 . 0 0 185 - 0 . 0 0 1 1 5 - 0 . 0 0 087 - 0 . 0 0 0 98

FFA TN 1 9 9 0 - 1 5 2 4

TABLE 3 . Profile coordinates .

Ai r fo i l : FFA-W1- 18 2

x/c

0 . 0 0 0 0 2 0 . 0 012 8 0 . 0 0 5 0 5 0 . 0 1131 0 . 0 2 0 0 4 0 . 0 311 9 0 . 0 4 4 7 1 0 . 0 6 0 5 4 0 . 0 7 8 5 9 0 . 0 987 8 0 . 12102 0 . 14 5 2 0 0 . 1712 0 0 . 19889 0 . 2 2 815 0 . 2 5883 0 . 2 9 0 7 9 0 . 3 2 3 87 0 . 3 5 7 92 0 . 392 7 7 0 . 4 2 82 6 0 . 4 6 4 2 0 0 . 5 0 0 4 4 0 . 5 3 680 0 . 5 7 310 0 . 6 0 917 0 . 64 4 84 0 . 6 7 9 9 3 0 . 7 142 8 0 . 7 4 7 7 2 0 . 7 80 0 9 0 . 8 112 4 0 . 84 1 0 2 0 . 8 6 92 8 0 . 8 9 588 0 . 9 2 0 7 1 0 . 9 4 3 65 0 . 9 6 4 5 7 0 . 983 3 8 1 . 0 0 0 0 0

yu/c

0 . 0 0 0 7 7 0 . 0 0 7 12 0 . 0 15 0 4 0 . 0 2 3 3 9 0 . 0 3 216 0 . 0 4 12 1 0 . 0 5 0 3 9 0 . 0 5 9 5 5 0 . 0 685 5 0 . 0 7 7 2 1 0 . 0 8 5 4 2 0 . 0 9 3 0 5 0 . 0 9 996 0 . 10 6 0 1 0 . 1110 7 0 . 115 01 0 . 11768 0 . 1189 7 0 . 1187 4 0 . 11689 0 . 113 5 6 0 . 10892 0 . 10 323 0 . 0 9 6 7 3 0 . 089 62 0 . 0 82 0 9 0 . 0 7 4 3 0 0 . 0 6 6 4 1 0 . 0 585 5 0 . 0 5 0 8 6 0 . 0 4 3 4 4 0 . 0 3 6 4 1 0 . 0 2 9 8 4 0 . 0 2 380 0 . 0 1 83 7 0 . 0 1 358 0 . 0 0 9 4 6 0 . 0 0 6 0 4 0 . 0 0 329 0 . 0 0 115

yl /c

0 . 0 0 0 7 7 - 0 . 0 0 623 - 0 . 0 1115 - 0 . 0 15 3 3 - 0 . 0 19 5 9 - 0 . 0 2388 - 0 . 0 2 82 5 - 0 . 0 3 2 6 6 - 0 . 0 3 7 0 8 - 0 . 0 4 14 3 - 0 . 0 4 5 6 3 - 0 . 0 4 9 6 0 - 0 . 0 5 3 2 1 - 0 . 0 5 6 3 9 - 0 . 0 5 9 0 4 - 0 . 0 610 5 - 0 . 0 6232 - 0 . 0 62 7 8 - 0 . 0 62 4 4 - 0 . 0 613 0 - 0 . 0 5 940 - 0 . 0 5 6 7 5 - 0 . 0 5 3 3 2 - 0 . 0 4 9 0 5 - 0 . 0 4 4 0 6 - 0 . 0 385 2 - 0 . 0 3 2 6 0 - 0 . 0 2 6 6 0 - 0 . 0 2 086 - 0 . 0 157 5 - 0 . 0 114 4 - 0 . 0 0 7 97 - 0 . 0 0 5 2 8 - 0 . 0 0 3 2 7 - 0 . 0 0 1 8 7 - 0 . 0 0101 - 0 . 0 0 0 6 0 - 0 . 0 0 0 5 7 - 0 . 0 0 081 - 0 . 0 0115

FFA TN 1 9 9 0-15 2 5

TABLE 4. Pro fi l e coordinates .

Airfoil : FFA-W1- 2 11

x!c

0 . 0 0 0 01 0 . 0 012 7 0 . 0 0 5 0 4 0 . 0113 0 0 . 0 2 0 0 3 0 . 0 3119 0 . 0 4 4 7 1 0 . 0 6 0 5 3 0 . 0 7 858 0 . 0 9878 0 . 12101 0 . 14 519 0 . 17119 0 . 19888 0 . 2 2 814 0 . 2 5 882 0 . 2 9 0 7 9 0 . 3 2 387 0 . 3 5 7 9 2 0 . 3 9 2 7 7 0 . 4 2 82 5 0 . 4 6 4 2 0 0 . 5 0 0 4 4 0 . 5 3 680 0 . 5 7 310 0 . 6 0 917 0 . 6 4 4 83 0 . 67 9 9 3 0 . 714 2 7 0 . 7 4 7 7 2 0 . 780 0 9 0 . 8112 4 0 . 84101 0 . 86 92 7 0 . 89588 0 . 9 2 0 71 0 . 9 4 3 64 0 . 9 6 4 5 7 0 . 983 3 8 1 . 0 0 0 0 0

yu l e

- 0 . 0 0 0 5 2 0 . 0 0 7 7 9 0 . 01619 0 . 0 2 5 0 4 0 . 0 3 4 2 1 0 . 04 358 0 . 0 5 3 0 4 0 . 0 62 4 4 0 . 0 7 1 6 3 0 . 0 80 4 6 0 . 08878 0 . 0 9 6 4 2 0 . 10 3 2 3 0 . 10 9 0 5 0 . 113 7 2 0 . 117 0 6 0 . 11891 0 . 119 2 0 0 . 117 95 0 . 115 3 5 0 . 1115 6 0 . 10 6 7 7 0 . 10114 0 . 0 9 4 83 0 . 0 87 9 9 0 . 080 7 4 0 . 0 7 319 0 . 0 65 5 7 0 . 0 5802 0 . 0 5 0 6 6 0 . 0 4 35 8 0 . 0 3 686 0 . 0 3 0 5 4 0 . 0 2 4 68 0 . 0 1 9 3 2 0 . 0 14 5 0 0 . 0 10 2 7 0 . 0 0 6 6 3 0 . 0 0 3 62 0 . 0 0114

yl /c

- 0 . 0 0 0 5 2 - 0 . 0 0 651 - 0 . 012 9 3 - 0 . 01937 - 0 . 0 2 6 0 3 - 0 . 0 3 2 92 - 0 . 0 3 9 9 6 - 0 . 0 4 7 0 2 - 0 . 0 5 4 0 3 - 0 . 0 6 087 - 0 . 0 6 7 3 9 - 0 . 0 7 3 4 6 - 0 . 0 7 893 - 0 . 083 65 - 0 . 087 4 2 - 0 . 0 9 0 0 7 - 0 . 0 914 9 - 0 . 0 9152 - 0 . 089 9 4 - 0 . 08657 - 0 . 0814 1 - 0 . 0 7 4 68 - 0 . 0 6 6 65 - 0 . 0 5 7 71 - 0 . 0 4 83 2 - 0 . 0 3 9 0 3 - 0 . 0 3 0 3 3 - 0 . 0 2 2 5 5 - 0 . 01588 - 0 . 0 10 4 2 - 0 . 0 0 611 - 0 . 0 0 2 88 - 0 . 0 0 0 64

0 . 0 0 0 71 0 . 0 013 0 0 . 0 012 9 0 . 0 0 089 0 . 0 0 0 2 4

- 0 . 0 0 0 5 7 - 0 . 0 014 8

FFA TN 1990 - 1 5 2 6

TABLE 5 . Pro f i le coordinates .

Ai r fo i l : FFA-W1- 2 4 2

x/c

0.0 0 0 0 3 0.0 012 9 0 .0 0 5 0 6 0.0113 2 0.0 2 0 0 5 0.0 312 1 0 .0 4 4 7 3 0 .0 6 0 5 5 0 .0 7 8 6 0 0 .0 987 9 0 .1210 3 0.14 521 0 .1712 0 0.19890 0 .2 281 6 0 .25884 0 .2 90 80 0.3 2 388 0 .3 5 7 93 0 .392 7 8 0 .4 2 82 6 0 .4 6 4 2 1 0 .5 0 0 4 4 0 .5 3 680 0 .5 7 310 0 . 6 0 917 0 .6 4 4 84 0.67993 0 .7 14 2 8 0 .74 7 7 1 0 .780 0 9 0 .8112 3 0 .84 10 1 0 .8692 7 0 .8 95 88 0 .92 0 7 1 0 .94 3 6 4 0 . 96 4 5 6 0 .98 3 3 7 0 .99999

yul e

0.0 0 138 0 .0 0 98 4 0 .0 195 3 0 .0 2 94 5 0.0 394 6 0 .0 4 95 3 0 .0 5958 0 .0 6939 0 .0 7 87 7 0.087 5 2 0.095 4 5 0.10 2 4 3 0 .10 83 4 0 .11310 0 .116 62 0 .11884 0 .11975 0 .11939 0.117 7 9 0.115 01 0 .11117 0 .10 640 0 .10 0 87 0 .0 94 75 0.0882 0 0.0813 6 0 .0 74 3 6 0 .0 6 7 3 2 0.0 6 0 3 4 0 .0 5 35 2 0 .0 4 695 0 .0 4 0 65 0 .0 3 4 6 4 0 .0 2 894 0 .0 2 3 5 9 0.01862 0 .014 0 9 0 .010 0 2 0 .0 0 6 3 9 0 .0 0 315

yl /c

0 .0 0138 -0.0 0 7 94 -0 .015 78 -0.0 2 3 6 7 -0.0 317 8 -0 .040 38 -0.0 4 93 5 -0.0585 4 -0.0 6 7 83 -0.0 7 7 0 8 -0.0 86 08 -0 .094 61 -0.10 2 4 2 -0 .10928 -0.114 91 -0.11905 -0 .1214 5 -0 .12 191 -0.12 0 2 6 -0 .11652 -0.110 7 7 -0 .10 3 0 5 -0.093 5 4 -0.082 6 3 -0 .0 7 0 5 7 -0.0 5 7 8 6 -0.0 4 5 19 -0.0 3 3 5 9 -0 .0 2 3 4 5 -0.01496 -0.0 0828 -0.0 0 3 31

0.0 0 013 0.0 0 2 17 0.0 0 2 97 0.0 0 2 7 2 0.0 0165 0 .0 0 0 0 8

-0.0 0164 -0.0 0 316

FFA TN 1 9 9 0 - 15 2 7

TABLE 6 . P rofi le coordinates .

Ai r foil : FFA-W1-2 7 1

x!c

0 . 0 0 0 0 0 0 . 0 0 1 2 6 0 . 0 0 5 0 3 0 . 0 1 1 3 0 0 . 0 2 0 0 3 0 . 0 3 1 1 8 0 . 0 4 4 7 0 0 . 0 6 0 5 2 0 . 0 7 85 7 0 . 0 987 7 0 . 1 2 1 0 1 0 . 1 4 5 1 8 0 . 1 7 1 1 8 0 . 1 9888 0 . 2 2 81 4 0 . 2 5882 0 . 2 9 0 7 8 0 . 3 2 386 0 . 3 5 7 9 1 0 . 3 92 7 6 0 . 4 2 82 5 0 . 4 6 4 1 9 0 . 5 0 0 4 3 0 . 5 3 6 7 9 0 . 5 7 3 0 9 0 . 6 0 9 1 7 0 . 6 4 4 83 0 . 6 7 9 92 0 . 7 1 4 2 7 0 . 7 4 7 7 1 0 . 780 0 9 0 . 81 1 2 4 0 . 84 1 0 1 0 . 86 9 2 7 0 . 89588 0 . 92 0 7 1 0 . 9 4 3 64 0 . 9 6 4 5 7 0 . 983 38 1 . 0 0 0 0 0

yu l e

0 . 0 0 0 0 0 0 . 0 1 1 6 3 0 . 0 2 2 86 0 . 0 3 3 84 0 . 0 4 4 5 7 0 . 0 5 5 1 8 0 . 0 65 65 0 . 0 7 5 85 0 . 0 85 5 9 0 . 0 9 4 68 0 . 1 0 2 9 3 0.1 1 0 1 9 0 . 1 1 6 3 1 0 . 1 2 1 1 8 0 . 1 2 4 7 5 0 . 1 2 6 9 9 0 . 1 2 7 87 0 . 1 2 7 4 6 0 . 1 2 5 84 0 . 1 2 3 0 8 0 . 1 1 9 3 0 0 . 1 1 4 6 1 0 . 1 0 9 1 3 0 . 1 0 3 0 1 0 . 0 9 6 3 9 0 . 0 89 3 9 0 . 082 1 0 0 . 0 7 4 7 0 0 . 0 6 7 3 4 0 . 0 6 0 1 1 0 . 0 5 3 1 2 0 . 0 4 6 4 6 0 . 0 4 0 1 6 0 . 0 3 4 2 6 0 . 0 2 87 9 0 . 0 2 3 67 0 . 0 1 894 0 . 0 1 4 62 0 . 0 1 0 7 3 0 . 0 0 7 3 0

yl /c

0 . 0 0 0 0 0 -0 . 0 1 1 58 -0 . 0 2 1 3 4 -0 . 0 3 0 83 - 0 . 0 4 0 6 9 -0 . 0 5 1 1 1 - 0 . 0 6 1 9 6 -0 . 0 7 2 9 7 -0 . 0 83 97 -0 . 0 9 4 7 6 - 0 . 1 0 5 0 5 -0 . 1 1 4 65 -0 . 1 2 3 3 0 -0 . 1 3 0 7 2 -0 . 1 3 6 6 4 - 0 . 1 4 0 7 7 -0 . 1 4 288 -0 . 1 4 ;2 7 8 - 0 . 1 4 0 3 6 - 0 . 1 3 5 6 1 - 0 . 1 2 8 6 1 -0 . 1 1 95 7 -0 . 1 0 87 2 -0 . 0 9 6 3 8 -0 . 0 83 0 0 -0 . 0 6 9 1 2 - 0 . 0 5 5 4 0 - 0 . 0 4 2 4 1 - 0 . 0 3 0 7 1 - 0 . 0 2 0 7 5 - 0 . 0 1 2 7 3 - 0 . 0 0 67 5 - 0 . 0 0 2 87 -0 . 0 0 0 9 6 -0 . 0 0 0 5 9 -0 . 0 0 1 3 2 - 0 . 0 0 2 6 9 - 0 . 0 0 4 3 4 -0 . 0 0 5 9 9 - 0 . 0 0 7 3 4

FFA TN 1 9 9 0 - 1 5 2 8

TABLE 7 . Pro fi l e coordinate s .

Ai r foi l : FFA-W2 -15 2

x/c

0 . 0 0 0 0 0 0 . 0 012 6 0 . 0 0 5 0 3 0 . 0 112 9 0 . 0 2 0 0 1 0 . 0 3115 0 . 0 4 4 6 6 0 . 0 6 0 4 7 0 . 0 7 8 5 0 0 . 0 9 8 6 8 0 . 12 0 9 0 0 . 14 5 0 5 0 . 1710 3 0 . 19 8 7 0 0 . 2 2 7 9 3 0 . 2 5 8 5 9 0 . 290 5 2 0 . 3 2 3 5 7 0 . 3 5 7 5 9 0 . 3 92 4 1 0 . 4 2 7 8 6 0 . 4 6 3 7 8 0 . 4 9 9 9 9 0 . 5 3 6 3 1 0 . 5 7 2 5 8 0 . 6 0 8 62 0 . 6 4 4 2 5 0 . 6 7 9 3 1 0 . 7 13 6 3 0 . 7 4 7 0 4 0 . 7 7 9 3 9 0 . 8 10 5 1 0 . 8 4 0 2 6 0 . 8 6 8 4 9 0 . 8 95 0 8 0 . 91 9 8 9 0 . 9 4 2 8 0 0 . 9 6 3 7 0 0 . 9 8 2 5 0 0 . 9 9 910

yu /c

0 . 0 0 0 0 0 0 . 0 0 5 4 4 0 . 0 117 4 0 . 018 9 2 0 . 0 2 6 6 4 0 . 0 3 4 67 0 . 0 4 2 8 1 0 . 0 5 0 9 6 0 . 0 5 9 0 1 0 . 0 6 6 8 5 0 . 0 7 4 4 1 0 . 0 8 15 9 0 . 0 8 8 3 0 0 . 0 9 4 40 0 . 0 9 9 7 7 0 . 10 4 2 6 0 . 10 7 7 5 0 . 11011 0 . 11119 0 . 110 9 2 0 . 10 92 0 0 . 10 6 0 2 0 . 10 14 3 0 . 0 95 6 3 0 . 0 8 8 8 2 0 . 0 8 13 0 0 . 0 7 3 3 3 0 . 0 6515 0 . 0 5 6 97 0 . 0 4 8 9 9 0 . 0 4 1 3 5 0 . 0 3 4 15 0 . 0 2 7 5 0 0 . 0 2 14 7 0 . 0 1614 0 . 0 115 5 0 . 0 0 7 7 4 0 . 0 0 4 7 2 0 . 0 0 2 4 9 0 . 0 0 0 95

yl /c

0 . 0 0 0 0 0 -0 . 0 0 5 5 6 - 0 . 010 4 2 - 0 . 0 14 71 - 0 . 018 5 3 -0 . 0 2 2 0 2 -0 . 0 2 5 2 2 - 0 . 02 816 -0 . 0 3 0 8 6 -0 . 0 3 3 3 4 -0 . 0 3 5 5 6 -0 . 0 3 7 4 8 -0 . 0 3 9 0 9 - 0 . 0 4 0 3 7 -0 . 0 4 1 31 -0 . 0 4191 -0 . 0 4 2 16 -0 . 0 4 2 0 8 - 0 . 0 4 16 9 -0 . 0 410 0 - 0 . 0 4 0 0 4 - 0 . 0 3 8 8 0 -0 . 0 3 7 3 0 -0 . 0 3 5 5 0 - 0 . 0 3 3 4 4 -0 . 0 3114 - 0 . 0 2 8 62 - 0 . 0 2 5 9 0 -0 . 0 2 3 0 1 -0 . 019 9 8 - 0 . 016 91 - 0 . 0 1 3 8 9 -0 . 01102 - 0 . 0 0 8 3 7 - 0 . 0 0 6 0 2 - 0 . 0 0 4 0 7 - 0 . 0 0 2 5 7 - 0 . 0 015 6 - 0 . 0 0 102 - 0 . 0 0 0 93

FFA TN 1 9 9 0 - 1 5 2 9

TABLE 8 . Pro f i l e coordinates .

Airfoi l : FFA-W2 - 2 1 0

x/c

0 . 0 0 0 0 0 0 . 0 0 1 2 6 0 . 0 0 5 0 3 0 . 0 1 1 3 0 0 . 0 2 0 0 3 0 . 0 3 1 1 8 0 . 0 4 4 7 0 0 . 0 6 0 5 2 0 . 0 7 8 5 7 0 . 0 9 8 7 7 0 . 1 2 1 0 1 0 . 1 4 5 1 8 0 . 1 7 1 1 8 0 . 1 9 8 8 8 0 . 2 2 8 1 4 0 . 2 5 8 8 2 0 . 2 9 0 7 8 0 . 3 2 3 8 6 0 . 3 5 7 9 1 0 . 3 92 7 6 0 . 4 2 8 2 5 0 . 4 6 4 1 9 0 . 5 0 0 4 3 0 . 5 3 6 7 9 0 . 5 7 3 0 9 0 . 6 0 9 1 7 0 . 6 4 4 8 3 0 . 6 7 9 92 0 . 7 1 4 2 7 0 . 7 4 7 7 1 0 . 7 8 0 0 9 0 . 8 1 1 2 4 0 . 8 4 1 0 1 0 . 8 6 9 2 7 0 . 8 95 8 8 0 . 92 0 7 1 0 . 94 3 6 4 0 . 96 4 5 7 0 . 98 3 3 8 1 . 0 0 0 0 0

yu /c

0 . 0 0 0 0 0 0 . 0 0 7 7 5 0 . 0 1 5 5 9 0 . 0 2 3 8 1 0 . 0 3 2 2 8 0 . 0 4 0 9 4 0 . 0 4 9 6 7 0 . 0 5 8 3 5 0 . 0 6 6 8 8 0 . 0 7 5 1 1 0 . 0 8 2 9 1 0 . 0 9 0 1 5 0 . 0 9 6 6 9 0 . 1 0 2 3 8 0 . 1 0 7 0 8 0 . 1 1 0 63 0 . 1 1 2 9 0 0 . 1 1 3 7 6 0 . 1 1 3 1 5 0 . 1 1 1 0 9 0 . 1 0 7 6 6 0 . 1 0 2 9 8 0 . 0 9 7 2 3 0 . 0 9 0 6 3 0 . 0 8 3 4 2 0 . 0 7 5 7 8 0 . 0 6 7 95 0 . 0 6 0 1 5 0 . 0 5 2 5 4 0 . 0 4 5 2 4 0 . 0 3 8 3 8 0 . 0 3 2 0 1 0 . 0 2 6 1 8 0 . 0 2 0 9 0 0 . 0 1 6 1 8 0 . 0 1 2 0 5 0 . 0 0 8 5 0 0 . 0 0 5 5 3 0 . 0 0 3 1 5 0 . 0 0 1 2 9

yl /c

0 . 0 0 0 0 0 - 0 . 0 0 7 0 5 - 0 . 0 1 3 2 0 - 0 . 0 1 95 1 - 0 . 0 2 62 5 - 0 . 0 3 3 3 8 - 0 . 0 4 0 7 1 - 0 . 0 4 8 1 0 - 0 . 0 5 5 4 5 - 0 . 0 62 6 6 - 0 . 0 6 95 5 - 0 . 0 7 5 9 8 - 0 . 0 8 1 8 1 - 0 . 0 8 6 8 9 - 0 . 0 9 1 0 3 - 0 . 0 9 4 0 8 - 0 . 0 95 9 6 - 0 . 0 9 6 6 0 - 0 . 0 95 9 1 - 0 . 0 9 3 8 1 - 0 . 0 9 0 3 1 - 0 . 0 8 5 4 9 - 0 . 0 7 9 4 7 - 0 . 0 7 2 4 3 - 0 . 0 6 4 5 6 - 0 . 0 5 6 1 7 - 0 . 0 4 7 62 - 0 . 0 3 92 5 - 0 . 0 3 1 3 7 - 0 . 0 2 4 2 5 - 0 . 0 1 8 1 0 - 0 . 0 1 3 0 2 - 0 . 0 0 9 0 1 - 0 . 0 0 6 0 0 - 0 . 0 0 3 8 5 - 0 . 0 02 4 3 - 0 . 0 0 1 5 7 - 0 . 0 0 1 1 4 - 0 . 0 0 1 0 6 - 0 . 0 0 1 2 9

FFA TN 1 9 9 0 - 1 5 3 0

TABLE 9 . P ro f i le coordinate s .

Ai r foi l : S O % NACA 6 3 - 6 1 8 AND 5 0 % FFA-W3 - 2 1 1

x / c

0 . 0 0 0 0 0 0 . 0 0 1 2 6 0 . 0 0 5 0 3 0 . 0 1 1 3 0 0 . 0 2 0 0 3 0 . 0 3 1 1 8 0 . 0 4 4 7 0 0 . 0 6 0 5 2 0 . 0 7 8 5 7 0 . 0 9 8 7 7 0 . 1 2 1 0 1 0 . 1 4 5 1 8 0 . 1 7 1 1 8 0 . 1 9 8 8 8 0 . 2 2 8 1 4 0 . 2 5 8 8 2 0 . 2 9 0 7 8 0 . 3 2 3 8 6 0 . 3 5 7 9 1 0 . 3 92 7 6 0 . 4 2 8 2 5 0 . 4 6 4 1 9 0 . 5 0 0 4 3 0 . 5 3 6 7 9 0 . 5 7 3 0 9 0 . 6 0 9 1 7 0 . 64 4 8 3 0 . 6 7 9 92 0 . 7 1 4 2 7 0 . 7 4 7 7 1 0 . 7 8 0 0 9 0 . 8 1 1 2 4 0 . 8 4 1 0 1 0 . 8 6 9 2 7 0 . 8 95 8 8 0 . 92 0 7 1 0 . 94 3 6 4 0 . 9 6 4 5 7 0 . 9 8 3 3 8 1 . 0 0 0 0 0

yu / c

0 . 0 0 0 0 0 0 . 0 0 7 6 1 0 . 0 1 5 4 9 0 . 0 2 3 8 8 0 . 0 3 2 5 1 0 . 0 4 1 3 7 0 . 0 5 0 3 8 0 . 0 5 9 3 5 0 . 0 6 8 1 3 0 . 0 7 6 5 9 0 . 0 8 4 6 0 0 . 0 92 0 5 0 . 0 9 8 8 0 0 . 1 0 4 7 4 0 . 1 0 9 7 2 0 . 1 1 3 5 9 0 . 1 1 62 4 0 . 1 1 7 5 8 0 . 1 1 7 5 4 0 . 1 1 6 1 6 0 . 1 1 3 5 5 0 . 1 0 9 8 5 0 . 1 0 5 1 6 0 . 0 9 9 6 3 0 . 0 9 3 4 1 0 . 0 8 6 6 0 0 . 0 7 9 3 4 0 . 0 7 1 8 3 0 . 0 64 2 0 0 . 0 5 6 6 0 0 . 0 4 9 1 6 0 . 0 4 2 0 0 0 . 0 3 5 2 3 0 . 0 2 8 8 5 0 . 0 2 2 9 3 0 . 0 1 7 5 4 0 . 0 1 2 65 0 . 0 0 8 2 2 0 . 0 0 4 2 5 0 . 0 0 0 65

y l / c

0 . 0 0 0 0 0 - 0 . 0 0 6 6 9 - 0 . 0 1 3 0 2 - 0 . 0 1 92 5 - 0 . 0 2 5 4 9 - 0 . 0 3 1 5 4 - 0 . 0 3 7 5 2 - 0 . 0 4 3 3 9 - 0 . 0 4 9 0 8 - 0 . 0 5 4 5 3 - 0 . 0 5 9 6 1 - 0 . 0 6 4 2 5 - 0 . 0 6 8 3 9 - 0 . 0 7 1 93 - 0 . 0 7 4 7 1 - 0 . 0 7 6 6 6 - 0 . 0 7 7 6 9 - 0 . 0 7 7 6 8 - 0 . 0 7 6 4 7 - 0 . 0 7 3 9 4 - 0 . 0 7 0 1 2 - 0 . 0 65 0 5 - 0 . 0 5 8 8 1 - 0 . 0 5 1 7 3 - 0 . 0 4 4 1 8 - 0 . 0 3 6 4 4 - 0 . 0 2 8 8 3 - 0 . 0 2 1 62 - 0 . 0 1 5 0 4 - 0 . 0 0 92 4 - 0 . 0 0 4 3 1 - 0 . 0 0 0 3 3

0 . 0 0 2 6 6 0 . 0 0 4 6 6 0 . 0 0 5 7 4 0 . 0 0 5 9 7 0 . 0 0 5 3 2 0 . 0 0 3 8 5 0 . 0 0 1 7 8

- 0 . 0 0 0 65

FFA TN 1 9 9 0 - 1 5 3 1

TABLE 1 0 . P ro f i l e coordinate s .

Ai r foi l : FFA-W3 - 2 1 1

x/ c

0 . 0 0 0 0 0 0 . 0 0 1 2 6 0 . 0 0 5 0 3 0 . 0 1 1 3 0 0 . 0 2 0 0 3 0 . 0 3 1 1 8 0 . 0 4 4 7 0 0 . 0 6 0 5 2 0 . 0 7 8 5 7 0 . 0 9 8 7 7 0 . 1 2 1 0 1 0 . 1 4 5 1 8 0 . 1 7 1 1 8 0 . 1 9 8 8 8 0 . 2 2 8 1 4 0 . 2 5 8 8 2 0 . 2 9 0 7 8 0 . 3 2 3 8 6 0 . 3 5 7 9 1 0 . 3 92 7 6 0 . 4 2 8 2 5 0 . 4 6 4 1 9 0 . 5 0 0 4 3 0 . 5 3 6 7 9 0 . 5 7 3 0 9 0 . 6 0 9 1 7 0 . 6 4 4 8 3 0 . 6 7 9 9 2 0 . 7 1 4 2 7 0 . 7 4 7 7 1 0 . 7 8 0 0 9 0 . 8 1 1 2 4 0 . 8 4 1 0 1 0 . 8 6 9 2 7 0 . 8 95 8 8 0 . 92 0 7 1 0 . 9 4 3 64 0 . 9 6 4 5 7 0 . 9 8 3 3 8 1 . 0 0 0 0 0

yu / c

0 . 0 0 0 0 0 0 . 0 0 7 7 8 0 . 0 1 6 1 6 0 . 0 2 5 0 0 0 . 0 3 4 1 6 0 . 0 4 3 5 2 0 . 0 5 2 9 6 0 . 0 6 2 3 4 0 . 0 7 1 5 1 0 . 0 8 0 3 1 0 . 0 8 8 6 0 0 . 0 9 62 1 0 . 1 0 2 9 9 0 . 1 0 8 7 8 0 . 1 1 3 4 2 0 . 1 1 6 7 3 0 . 1 1 8 5 4 0 . 1 1 8 8 0 0 . 1 1 7 5 2 0 . 1 1 4 8 9 0 . 1 1 1 0 8 0 . 1 0 62 7 0 . 1 0 0 62 0 . 0 9 4 2 9 0 . 0 8 7 4 6 0 . 0 8 0 2 1 0 . 0 7 2 6 8 0 . 0 65 0 9 0 . 0 5 7 5 8 0 . 0 5 0 2 9 0 . 0 4 3 3 1 0 . 0 3 6 7 5 0 . 0 3 0 6 6 0 . 0 2 5 0 1 0 . 0 1 9 8 4 0 . 0 1 5 1 5 0 . 0 1 0 9 6 0 . 0 0 7 2 9 0 . 0 0 4 1 4 0 . 0 0 1 3 1

y l / c

0 . 0 0 0 0 0 - 0 . 0 0 65 2 - 0 . 0 1 2 9 5 - 0 . 0 1 9 3 9 - 0 . 0 2 6 0 6 - 0 . 0 3 2 9 8 - 0 . 0 4 0 0 3 - 0 . 0 4 7 1 1 - 0 . 0 5 4 1 4 - 0 . 0 6 0 9 9 - 0 . 0 67 5 3 - 0 . 0 7 3 6 0 - 0 . 0 7 9 0 8 - 0 . 0 8 3 7 9 - 0 . 0 8 7 5 7 - 0 . 0 9 0 3 0 - 0 . 0 9 1 8 5 - 0 . 0 92 0 4 - 0 . 0 9 0 7 0 - 0 . 0 8 7 7 3 - 0 . 0 8 3 0 6 - 0 . 0 7 6 6 7 - 0 . 0 6 8 65 - 0 . 0 5 9 5 0 - 0 . 0 4 9 7 9 - 0 . 0 3 9 95 - 0 . 0 3 0 4 5 - 0 . 0 2 1 6 9 - 0 . 0 1 3 9 8 - 0 . 0 0 7 4 7 - 0 . 0 0 2 1 9

0 . 0 0 1 7 8 0 . 0 0 4 4 7 0 . 0 0 6 0 0 0 . 0 0 64 7 0 . 0 0 5 9 9 0 . 0 0 4 7 0 0 . 0 0 2 8 4 0 . 0 0 0 7 4

- 0 . 0 0 1 3 1

FFA TN 1 9 9 0 - 1 5 3 2

TABLE 1 1 . Pro f i le coordinate s .

Ai r foi l : FFA-W3 - 2 4 1

x / c

0 . 0 0 0 0 4 0 . 0 0 1 3 0 0 . 0 0 5 0 7 0 . 0 1 1 3 3 0 . 0 2 0 0 6 0 . 0 3 1 2 2 0 . 0 4 4 7 4 0 . 0 6 0 5 6 0 . 0 7 8 6 1 0 . 0 9 8 8 0 0 . 1 2 1 0 4 0 . 1 4 5 2 2 0 . 1 7 1 2 1 0 . 1 9 8 9 1 0 . 2 2 8 1 7 0 . 2 5 8 8 5 0 . 2 9 0 8 1 0 . 32 3 8 9 0 . 35 7 9 4 0 . 3 92 7 9 0 . 4 2 8 2 7 0 . 4 6 4 2 2 0 . 5 0 0 4 5 0 . 5 3 6 8 1 0 . 5 7 3 1 1 0 . 6 0 9 1 8 0 . 6 4 4 8 5 0 . 6 7 9 9 4 0 . 7 1 4 2 8 0 . 7 4 7 7 2 0 . 7 8 0 1 0 0 . 8 1 1 2 4 0 . 8 4 1 0 2 0 . 8 6 9 2 8 0 . 8 95 8 9 0 . 9 2 0 7 2 0 . 9 4 3 65 0 . 9 6 4 5 7 0 . 9 8 3 3 8 1 . 0 0 0 0 0

yu l e

0 . 0 0 1 6 0 0 . 0 0 9 5 6 0 . 0 2 0 0 5 0 . 0 3 0 3 3 0 . 0 4 0 8 7 0 . 0 5 1 3 5 0 . 0 6 1 7 0 0 . 0 7 1 7 6 0 . 0 8 1 3 9 0 . 0 9 0 4 4 0 . 0 9 8 7 3 0 . 1 0 6 1 3 0 . 1 1 2 4 7 0 . 1 1 7 6 4 0 . 1 2 1 5 3 0 . 1 2 4 0 9 0 . 1 2 5 2 6 0 . 1 2 5 0 4 0 . 1 2 3 5 0 0 . 1 2 0 7 6 0 . 1 1 6 9 6 0 . 1 1 2 2 3 0 . 1 0 6 7 0 0 . 1 0 0 5 2 0 . 0 9 3 8 2 0 . 0 8 6 7 2 0 . 0 7 9 3 5 0 . 0 7 1 8 7 0 . 0 6 4 4 1 0 . 0 5 7 0 7 0 . 0 4 9 9 6 0 . 0 4 3 1 6 0 . 0 3 6 7 3 0 . 0 3 0 7 0 0 . 0 2 5 1 0 0 . 0 1 9 9 6 0 . 0 1 5 2 9 0 . 0 1 1 0 7 0 . 0 0 7 2 7 0 . 0 0 3 9 1

y l / c

0 . 0 0 1 6 0 - 0 . 0 0 9 0 3 - 0 . 0 1 7 0 0 - 0 . 0 2 5 5 0 - 0 . 0 3 4 2 7 - 0 . 0 4 3 3 4 - 0 . 0 5 2 5 8 - 0 . 0 6 1 8 8 - 0 . 0 7 1 0 4 - 0 . 0 7 9 8 5 - 0 . 0 8 8 1 1 - 0 . 0 95 6 0 - 0 . 1 0 2 1 3 - 0 . 1 0 7 5 4 - 0 . 1 1 1 6 7 - 0 . 1 1 4 4 1 - 0 . 1 1 5 6 7 - 0 . 1 1 5 3 1 - 0 . 1 1 3 2 4 - 0 . 1 0 9 3 8 - 0 . 1 0 3 7 0 - 0 . 0 9 6 2 3 - 0 . 0 8 7 0 6 - 0 . 0 7 65 1 - 0 . 0 65 0 2 - 0 . 0 5 3 0 8 - 0 . 0 4 1 2 7 - 0 . 0 3 0 1 5 - 0 . 0 2 0 2 4 - 0 . 0 1 1 8 3 - 0 . 0 0 5 1 4 - 0 . 0 0 0 3 0

0 . 0 0 2 9 1 0 . 0 0 4 7 3 0 . 0 0 5 2 8 0 . 0 0 4 6 6 0 . 0 0 3 1 1 0 . 0 0 0 9 6

- 0 . 0 0 1 4 0 - 0 . 0 0 3 6 0

FFA TN 1 9 9 0 - 1 5 3 3

TABLE 1 2 . Profile coordinates .

A i r fo i l : FFA-W3 - 2 7 0

x / c

0 . 0 0 0 0 5 0 . 0 0 1 3 1 0 . 0 0 5 0 8 0 . 0 1 1 3 5 0 . 0 2 0 0 9 0 . 0 3 1 2 5 0 . 0 4 4 7 8 0 . 0 6 0 62 0 . 0 7 8 6 9 0 . 0 9 8 9 0 0 . 1 2 1 1 5 0 . 1 4 5 3 5 0 . 1 7 1 3 7 0 . 1 9 9 0 9 0 . 2 2 8 3 7 0 . 2 5 9 0 8 0 . 2 9 1 0 7 0 . 3 2 4 1 8 0 . 3 5 8 2 5 0 . 3 9 3 1 3 0 . 4 2 8 6 4 0 . 4 6 4 62 0 . 5 0 0 8 9 0 . 5 3 7 2 8 0 . 5 7 3 6 1 0 . 6 0 9 7 1 0 . 64 5 4 1 0 . 6 8 0 5 3 0 . 7 1 4 9 0 0 . 7 4 8 3 7 0 . 7 8 0 7 7 0 . 8 1 1 95 0 . 8 4 1 7 5 0 . 8 7 0 0 3 0 . 8 9 6 6 6 0 . 92 1 5 1 0 . 94 4 4 6 0 . 9 65 4 0 0 . 9 8 4 2 3 1 . 0 0 0 8 6

yu / c

0 . 0 0 2 0 9 0 . 0 1 0 7 4 0 . 0 2 2 5 1 0 . 0 3 4 2 0 0 . 0 4 5 9 3 0 . 0 5 7 5 7 0 . 0 6 8 9 6 0 . 0 7 9 9 6 0 . 0 9 0 4 3 0 . 1 0 0 1 8 0 . 1 0 9 0 4 0 . 1 1 6 8 3 0 . 1 2 3 4 2 0 . 1 2 8 6 8 0 . 1 3 2 5 3 0 . 1 3 4 9 5 0 . 1 3 5 92 0 . 1 3 5 4 8 0 . 1 3 3 7 0 0 . 1 3 0 7 0 0 . 1 2 65 8 0 . 1 2 1 4 7 0 . 1 1 5 5 0 0 . 1 0 8 8 2 0 . 1 0 1 5 6 0 . 0 9 3 8 8 0 . 0 8 5 9 4 0 . 0 7 7 8 8 0 . 0 6 9 8 5 0 . 0 6 1 9 7 0 . 0 5 4 3 4 0 . 0 4 7 0 4 0 . 0 4 0 1 4 0 . 0 3 3 6 8 0 . 0 2 7 7 0 0 . 0 2 2 2 0 0 . 0 1 7 2 1 0 . 0 1 2 6 9 0 . 0 0 8 5 8 0 . 0 0 4 95

y l / c

0 . 0 0 2 0 9 - 0 . 0 1 0 3 8 - 0 . 0 2 0 4 4 - 0 . 0 3 0 3 0 - 0 . 0 4 0 67 - 0 . 0 5 1 2 9 - 0 . 0 62 1 5 - 0 . 0 7 3 0 4 - 0 . 0 8 3 7 5 - 0 . 0 9 4 0 0 - 0 . 1 0 3 5 6 - 0 . 1 1 2 1 5 - 0 . 1 1 95 7 - 0 . 1 2 5 63 - 0 . 1 3 0 1 9 - 0 . 1 3 3 1 2 - 0 . 1 3 4 3 2 - 0 . 1 3 3 7 1 - 0 . 1 3 1 2 1 - 0 . 1 2 6 7 5 - 0 . 1 2 0 32 - 0 . 1 1 1 9 6 - 0 . 1 0 1 8 1 - 0 . 0 9 0 1 0 - 0 . 0 7 7 2 3 - 0 . 0 6 3 7 5 - 0 . 0 5 0 3 0 - 0 . 0 3 7 5 5 - 0 . 0 2 6 1 0 - 0 . 0 1 6 3 6 - 0 . 0 0 8 5 9 - 0 . 0 0 2 9 8

0 . 0 0 0 7 6 0 . 0 0 2 9 9 0 . 0 0 3 7 7 0 . 0 0 3 2 4 0 . 0 0 1 6 8

- 0 . 0 0 0 5 2 - 0 . 0 0 2 95 - 0 . 0 0 5 1 7

FFA TN 1 9 9 0 - 1 5 3 4

TABLE 1 3 . Pro f i le coordinate s .

Airfoi l : FFA-W3 - 3 0 1

x / c

0 . 0 0 0 0 1 0 . 0 0 1 2 7 0 . 0 0 5 0 4 0 . 0 1 1 3 1 0 . 0 2 0 0 4 0 . 0 3 1 1 9 0 . 0 4 4 7 1 0 . 0 6 0 5 3 0 . 0 7 8 5 9 0 . 0 9 8 7 8 0 . 1 2 1 0 2 0 . 1 4 5 1 9 0 . 1 7 1 1 9 0 . 1 9 8 8 9 0 . 2 2 8 1 4 0 . 2 5 8 8 3 0 . 2 9 0 7 9 0 . 32 3 8 7 0 . 3 5 7 9 2 0 . 3 92 7 7 0 . 4 2 8 2 5 0 . 4 6 4 2 0 0 . 5 0 0 4 4 0 . 5 3 6 8 0 0 . 5 7 3 1 0 0 . 6 0 9 1 7 0 . 6 4 4 8 4 0 . 6 7 9 9 3 0 . 7 1 4 2 8 0 . 7 4 7 7 2 0 . 7 8 0 0 9 0 . 8 1 1 2 4 0 . 8 4 1 0 1 0 . 8 6 9 2 7 0 . 8 95 8 8 0 . 92 0 7 1 0 . 9 4 3 6 4 0 . 9 6 4 5 7 0 . 9 8 3 3 8 1 . 0 0 0 0 0

yu l e

- 0 . 0 0 1 1 9 0 . 0 1 3 2 6 0 . 0 2 6 6 7 0 . 0 4 0 0 1 0 . 0 5 3 3 9 0 . 0 6 6 5 5 0 . 0 7 9 3 8 0 . 0 9 1 67 0 . 1 0 3 2 3 0 . 1 1 3 8 5 0 . 1 2 3 3 2 0 . 1 3 1 4 6 0 . 1 3 8 1 4 0 . 1 4 32 5 0 . 1 4 6 7 3 0 . 1 4 8 6 6 0 . 1 4 9 0 8 0 . 1 4 8 0 7 0 . 1 4 5 7 8 0 . 1 4 2 3 0 0 . 1 3 7 7 6 0 . 1 3 2 2 9 0 . 1 2 6 0 1 0 . 1 1 9 0 9 0 . 1 1 1 6 9 0 . 1 0 3 9 1 0 . 0 95 8 7 0 . 0 8 7 6 6 0 . 0 7 9 3 9 0 . 0 7 1 1 6 0 . 0 6 3 0 9 0 . 0 5 5 2 8 0 . 0 4 7 8 0 0 . 0 4 0 7 4 0 . 0 3 4 1 7 0 . 0 2 8 1 2 0 . 0 2 2 6 6 0 . 0 1 7 7 5 0 . 0 1 3 3 3 0 . 0 0 93 7

y l / c

- 0 . 0 0 1 1 9 - 0 . 0 1 2 5 6 - 0 . 0 2 5 0 2 - 0 . 0 3 7 6 4 - 0 . 0 5 0 3 5 - 0 . 0 6 3 1 2 - 0 . 0 7 5 8 2 - 0 . 0 8 8 2 5 - 0 . 1 0 0 1 8 - 0 . 1 1 1 3 6 - 0 . 1 2 1 5 5 - 0 . 1 3 0 5 2 - 0 . 1 3 8 1 0 - 0 . 1 4 4 1 1 - 0 . 1 4 8 4 7 - 0 . 1 5 1 0 8 - 0 . 1 5 1 8 8 - 0 . 1 5 0 8 0 - 0 . 1 4 7 8 0 - 0 . 1 4 2 8 3 - 0 . 1 3 5 9 1 - 0 . 1 2 7 1 0 - 0 . 1 1 65 2 - 0 . 1 0 4 4 2 - 0 . 0 9 1 1 6 - 0 . 0 7 7 2 2 - 0 . 0 6 3 1 8 - 0 . 0 4 9 6 6 - 0 . 0 3 7 2 2 - 0 . 0 2 63 1 - 0 . 0 1 7 1 5 - 0 . 0 1 0 0 2 - 0 . 0 0 4 7 9 - 0 . 0 0 1 3 4

0 . 0 0 0 4 0 0 . 0 0 0 5 8

- 0 . 0 0 0 5 1 - 0 . 0 0 2 6 1 - 0 . 0 0 5 5 8 - 0 . 0 0 8 9 1

FFA TN 1 9 9 0 - 1 5 35

TABLE 1 4 . Pro f i le coordinate s .

Ai r foi l : FFA-W3 - 3 3 2

x ! c

0 . 0 0 0 0 1 0 . 0 0 1 2 7 0 . 0 0 5 0 4 0 . 0 1 1 3 1 0 . 0 2 0 0 4 0 . 0 3 1 1 9 0 . 0 4 4 7 0 0 . 0 6 0 5 3 0 . 0 7 8 5 8 0 . 0 9 8 7 7 0 . 1 2 1 0 0 0 . 1 4 5 1 8 0 . 1 7 1 1 7 0 . 1 9 8 8 6 0 . 2 2 8 1 2 0 . 2 5 8 8 0 0 . 2 9 0 7 6 0 . 3 2 3 8 4 0 . 35 7 8 8 0 . 3 92 7 3 0 . 4 2 8 2 1 0 . 4 6 4 1 5 0 . 5 0 0 3 8 0 . 5 3 6 7 4 0 . 5 7 3 0 4 0 . 6 0 9 1 0 0 . 6 4 4 7 6 0 . 67 9 8 5 0 . 7 1 4 2 0 0 . 7 4 7 6 3 0 . 7 8 0 0 0 0 . 8 1 1 1 5 0 . 8 4 0 92 0 . 8 6 9 1 8 0 . 8 95 7 8 0 . 92 0 6 1 0 . 9 4 3 5 4 0 . 9 6 4 4 6 0 . 9 8 3 2 7 0 . 9 9 9 8 9

yu / c

0 . 0 0 1 4 6 0 . 0 1 5 1 9 0 . 0 3 0 3 2 0 . 0 4 5 3 9 0 . 0 6 0 3 5 0 . 0 7 5 0 5 0 . 0 8 9 3 0 0 . 1 0 2 8 8 0 . 1 1 5 5 3 0 . 1 2 7 0 1 0 . 1 3 7 0 9 0 . 1 4 5 5 7 0 . 1 5 2 3 3 0 . 1 5 7 2 9 0 . 1 6 0 4 4 0 . 1 6 1 8 5 0 . 1 6 1 62 0 . 1 5 9 8 9 0 . 1 5 6 8 0 0 . 1 5 2 5 3 0 . 1 4 7 2 9 0 . 1 4 1 1 7 0 . 1 3 4 3 0 0 . 1 2 6 8 3 0 . 1 1 8 9 0 0 . 1 1 0 6 4 0 . 1 0 2 1 9 0 . 0 9 3 6 6 0 . 0 8 5 1 4 0 . 0 7 67 5 0 . 0 6 8 5 5 0 . 0 6 0 6 4 0 . 0 5 3 0 8 0 . 0 4 5 9 3 0 . 0 3 92 6 0 . 0 3 3 0 9 0 . 0 2 7 4 5 0 . 0 2 2 2 9 0 . 0 1 7 5 4 0 . 0 1 3 2 5

y l / c

0 . 0 0 1 4 6 - 0 . 0 1 52 5 - 0 . 0 3 0 4 1 - 0 . 0 4 5 5 5 - 0 . 0 6 0 6 4 - 0 . 0 7 5 5 3 - 0 . 0 9 0 0 6 - 0 . 1 0 4 0 2 - 0 . 1 1 7 1 7 - 0 . 1 2 92 7 - 0 . 1 4 0 1 0 - 0 . 1 4 9 4 5 - 0 . 1 5 7 1 7 - 0 . 1 6 3 1 5 - 0 . 1 6 7 3 1 - 0 . 1 6 95 9 - 0 . 1 6 9 9 8 - 0 . 1 6 8 4 3 - 0 . 1 6 4 9 3 - 0 . 1 5 94 6 - 0 . 1 5 2 0 5 - 0 . 1 4 2 7 7 - 0 . 1 3 1 7 7 - 0 . 1 1 92 8 - 0 . 1 0 5 6 3 - 0 . 0 9 1 2 3 - 0 . 0 7 6 6 0 - 0 . 0 62 3 0 - 0 . 0 4 8 8 8 - 0 . 0 3 6 8 3 - 0 . 0 2 62 4 - 0 . 0 1 7 6 1 - 0 . 0 1 0 8 8 - 0 . 0 0 62 0 - 0 . 0 0 3 5 1 - 0 . 0 0 2 62 - 0 . 0 0 3 2 4 - 0 . 0 0 5 2 4 - 0 . 0 0 8 7 5 - 0 . 0 1 3 1 9

FFA TN 1 9 9 0 - 1 5 3 6

TABLE 1 5 . Pro f i l e coordinates .

Ai r fo i l : FFA-W3 - 3 6 0

x / c

0 . 0 0 0 1 2 0 . 0 0 1 3 8 0 . 0 0 5 1 5 0 . 0 1 1 4 1 0 . 0 2 0 1 4 0 . 0 3 1 2 9 0 . 0 4 4 8 1 0 . 0 6 0 6 3 0 . 0 7 8 6 8 0 . 0 9 8 8 7 0 . 1 2 1 1 1 0 . 1 4 5 2 8 0 . 1 7 1 2 8 0 . 1 9 8 9 7 0 . 2 2 8 2 3 0 . 2 5 8 9 1 0 . 2 9 0 8 6 0 . 3 2 3 9 4 0 . 3 5 7 9 9 0 . 3 9 2 8 3 0 . 4 2 8 3 1 0 . 4 6 4 2 6 0 . 5 0 0 4 9 0 . 5 3 6 8 5 0 . 5 7 3 1 4 0 . 6 0 9 2 1 0 . 6 4 4 8 7 0 . 6 7 9 9 6 0 . 7 1 4 3 1 0 . 7 4 7 7 4 0 . 7 8 0 1 1 0 . 8 1 1 2 6 0 . 8 4 1 0 3 0 . 8 6 9 2 9 0 . 8 95 8 9 0 . 9 2 0 7 2 0 . 9 4 3 65 0 . 9 6 4 5 7 0 . 9 8 3 3 9 1 . 0 0 0 0 0

yu / c

0 . 0 0 6 1 2 0 . 0 1 7 5 5 0 . 0 4 1 4 0 0 . 0 5 9 5 0 0 . 0 7 7 1 6 0 . 0 9 4 0 5 0 . 1 1 0 0 1 0 . 1 2 4 7 4 0 . 1 3 8 0 4 0 . 1 4 9 8 2 0 . 1 5 9 9 6 0 . 1 6 8 4 4 0 . 1 7 5 1 2 0 . 1 7 9 9 4 0 . 1 8 2 9 1 0 . 1 8 4 1 4 0 . 1 8 3 7 0 0 . 1 8 1 7 1 0 . 1 7 8 2 5 0 . 1 7 3 4 7 0 . 1 6 7 4 9 0 . 1 6 0 4 8 0 . 1 5 2 6 2 0 . 1 4 4 0 8 0 . 1 3 5 0 5 0 . 1 2 5 6 8 0 . 1 1 6 1 1 0 . 1 0 6 4 7 0 . 0 9 6 8 7 0 . 0 8 7 4 0 0 . 0 7 8 1 5 0 . 0 6 9 2 0 0 . 0 6 0 6 3 0 . 0 5 2 5 1 0 . 0 4 4 8 9 0 . 0 3 7 8 3 0 . 0 3 1 3 7 0 . 0 2 5 4 3 0 . 0 1 9 9 7 0 . 0 1 5 0 3

y l / c

0 . 0 0 6 1 2 - 0 . 0 1 4 5 9 - 0 . 0 3 6 2 4 - 0 . 0 5 3 3 0 - 0 . 0 7 0 0 6 - 0 . 0 8 5 8 7 - 0 . 1 0 0 6 4 - 0 . 1 1 4 4 0 - 0 . 1 2 6 9 5 - 0 . 1 3 8 2 1 - 0 . 1 4 8 1 8 - 0 . 1 5 6 8 3 - 0 . 1 6 4 0 2 - 0 . 1 6 9 7 0 - 0 . 1 7 3 7 5 - 0 . 1 7 6 0 3 - 0 . 1 7 6 4 3 - 0 . 1 7 4 8 8 - 0 . 1 7 1 3 4 - 0 . 1 6 5 7 8 - 0 . 1 5 8 1 6 - 0 . 1 4 8 4 8 - 0 . 1 3 7 0 5 - 0 . 1 2 4 1 6 - 0 . 1 1 0 0 9 - 0 . 0 9 5 2 2 - 0 . 0 8 0 0 0 - 0 . 0 6 5 0 0 - 0 . 0 5 0 8 3 - 0 . 0 3 8 0 7 - 0 . 0 2 7 1 3 - 0 . 0 1 8 1 6 - 0 . 0 1 1 2 0 - 0 . 0 0 6 3 6 - 0 . 0 0 3 6 1 - 0 . 0 0 2 7 3 - 0 . 0 0 3 4 2 - 0 . 0 0 5 5 5 - 0 . 0 0 92 8 - 0 . 0 1 3 9 3

"! -

� -

10 0

0 0

--0.000

-

C) A

--

Data from Abbot & Doenhoff at Re=6E6, smooth airfoi l

Data from Abbot & Doenhoff at Re=6E6 with standard roughness

XFOIL calculations at Re=6E6, free transition with Acrit=9

XFOIL calculations at Re=6E6, forced transition at Xtrs=O.Ol and Xtrp=O. l

I - . . - I !-- C) ----

� �--1-- " I I I I :Al" l I I � "1 1 9

/ "' A

v v b / A ,.

IJb C9 / A .

:3 1 I 1 :60 1 I I ,rT\ r= . . C) I A M A . b I � � . A .

I � I C) A C) � I I I I I I I I � --- - - -- L _ _ _.____ ____J..__ - --

0.005 0.010 O.ot5 0.020 0.025 -3 0 3 6 9 1 2 1 5 1 8 Cd Alpha

F ig . l XFOIL calculations compared with wind tunne l te s t re sults f rom [ 9 ] for the NACA 6 3 - 6 1 5 a i rfo i l .

� : I / I "! -

� -

10 0

�--------�---------1- 0

0.0 0.5 xtr/c

0

1 .0

-u

1-tj 1-tj �

1-3 z

1--' 1.0 1.0 0

I 1--' lJl

w .......

"1 -

q -

tr) 0

0 0

0.000

C) A

0.005

Data from Miley at Re=2E6, smooth airfoil

Data from Miley at Re=2E6 with standard roughness

XFOIL calculations at Re=2E6, free transition with Acrit=9

XFOIL calculations at Re=2E6, forced transition at Xtrs=O.Ol and Xtrp=O. l

v 1/m � V!J) / ( C) .

I p . . L C) I (T)

A . C) I /!),.

� C) .

I ; C) I / �

\ C) . A

�C) /!:>.

A "' A '-J

-t...--I-"' . . - . . -.-

/ " v· A

= A ...... �

I I I I I :;;;;+ I � "1 1 9

� I I I A'�'CJ� I I I I � 9

0 � I l�ar _ _ r _ _ r _ �l�� l d a I

:3f I I I I I I I :3

�---------+----------;-"1 -

q -

ll') 0

I I / I \ I � 0

0.010 0.015 0.020 0.025 -3 0 3 6 9 Alpha

12 15 1 8 0.0 0.5 xtr/c

1 .0 Cd

Fig . 2 XFOIL calculations compared with wind tunnel test re sults from [ 1 1 ] for the NACA 6 3 - 6 1 5 a i rfoi l .

-u

1-tj 1-tj ::t>' t-3 z ...... 1.0 1.0 0 I

...... Ul

w <X>

"1 -

c:

II') ci

0 ci

0.000

(!) Data from Miley at Re=3E6, smooth airfoil

XFOIL calculations at Re=3E6, free transition with Acrit=9

XFOIL calculations at Re=3E6, forced transi�ion at Xtrs=O.Ol and Xtrp=O. l

a � � � /

I p . . C) I

I.J (') � u

I\(')"' \ m �

:::::::: 1--� -� ....-<!5 C) • • / .

I

I I j I I J �I

0

"1 -

c: -

II') ci

0 0

C'"l 9 �---------+----------�"1

hj hj :J::i

1-3 z

I-' 1.0 1.0 0

I I-' Lll

� E 1 � 1 1 r5 _ �

u . \ r u

d I I

IV 1 :2

0 0

�--��---r��------� 0 0

0.005 0.010 0.015 0.020 0.025 -3 0 3 6 9 12 15 18 0.0 0.5 xtr/c

l .O Cd Alpha

F ig . 3 XFOIL calculations compa red with wind tunne l test re sults from [ 1 1 ] for the NACA 6 3 - 4 1 5 airfo i l .

"1 -

c: -

.,., 0

0 0

.- ,

-

0.000

(!) A

I

I

Data from Abbot & Doenhoff at Re=6E6, smooth airfoil

Data from Abbot & Doenhoff at Re=6E6 with standard roughness

XFOIL calculations at Re=6E6, free transition with Acrit=9 . XFOIL calculations at Re=6E6, forced transition at Xtrs=O.Ol and Xtrp=O. l

/� :::::-

�I L ; _, .' A .

• • !-- ""! --t A

-----t c: -

r/�p �'�AA � AI. A

f 6 J!)' "' I" ..... l,6 . .

I C) b I A b . � ; � ! t_ � i .I� \ I

---+

-t

'-

u .,., 0

0 0

jl �- . . � � <D C9 r=-· J u � -�

II_ - -

� 9

N 9

-0

I

0 0

0.005 0.010 0.015 0.020 0.025 -3 0 3 6 9 1 2 15 1 8 Cd Alpha

F ig . 4 XFOIL calculations compared with wind tunne l tes t re sults from [ 9 ] for the NACA 6 3 - 4 1 5 a i r fo i l .

E u

! I /- I "1 -

�� 1 / 1 3 0

I I �I 1 :2

I 1/ I \ I C:

0.0 0.5 xtr/c

0

1 .0

t-rj t-rj :t:'

t-3 z

1--' 1.0 1.0 0 I

1--' Ul

""' 0

"1 -

C1 -

tn 0

C1 0

0.000

(!)

0.005

Data from Abbot & Doenhoff at Re=3E6, smooth airfoil

XFOIL calculations at Re=3E6, free transition with Acrit=9

XFOIL calculations at Re=3E6, forced transition at Xtrs=O.Ol and Xtrp=O. l

r c

I� 0 (!) 0 0

0

� v

�

/ . . .....- · ·

..,· ,/

li j

.

I . .

! i I

I 0.010 0.015

Cd

----' - -0.020

I - · · 1 1 I I I 1 I

I

0.025

0

"1 -

C1 -

10 c:i

0 c:i

-3 0 3 6 9 Alpha

('<) 9

M 9

-c:i

I

0 c:i

1 2 1 5 1 8

F ig . S XFOIL calculations compared with wind tunnel test re sults from [ 9 ] for the NACA 6 3 - 4 2 1 a i rfo i l .

E u

r----------;-----------+-"1 -

I I \ I I 1 5 � ! \II I ' i u 1 :9

I I / 1 \ I C1

0.0 0.5 xtr/c

0

1 .0

-u

tTj 1-Ij >' 1-3 z I-' � � 0 I

I-' lJl

A I-'

"1 ......

q ......

10 0

q 0

'--

0.000

(!) A

Data from Abbot & Doenhoff at Re=6E6, smooth airfoil

Data from Abbot & Doenhoff at Re=6E6 with standard roughness

XFOIL calculations at Re=6E6, free transition with Acrit=9

XFOIL calculations at Re=6E6, forced transition at Xtrs=O.Ol and Xtrp=O. l

"1 1 I I I I I :b I s; � --(9 --f..--� r--

� ? . . f.-- · · ---

"' - · ·

. "1 ......

1-tj 1-tj :t:' 1-3 z I-' � 1..0 0 I

I-' Ul

'- / .

. . I

A qi I I /1' /&'f I I I C'! I I ' I I I q

9 0 � I I Jf"J �L I I I ci a I ! V 1 � 0

�

(9 (9 (9 (9 (9

�

0.005

. � .

I 4� • A . / A I

' A A

. A i I A � r I I I I I I I �

--··-

0.010 0.015 Cd

---

0.020 0.025 -3 0 3 6 9 Alpha

12 15 18

F ig . 6 XFOIL calculations compared with wind tunne l te st results from [ 9 ] for the NACA 6 3 - 4 2 1 a i rfo i l .

I I / 1 \ I q

0.0 0.5 xtr/c

0

1 .0

"1 -

C1 -

V) 0

0 0

r-

0.000

C) A

1 0.005

Data from McGhee & Beasley at Re=4E6, Roughness off

Data from McGhee & Beasley at Re=4E6, Roughness on

XFOIL calculations at Re=4E6, free transition with Acrit=9

XFOIL calculations at Re=4E6, forced transition at Xtrs=0.07 and Xtrp=0.07

lc l:..

\C) \

� l.--lr----.,.--- .. �P... / _A -

v _ v.,.. L C) .4. 0':1 •

v l: f C) .. � D /A /C) ,t:

C) A j � AI D A.

-1 f2 ! A �"' � I \ .

\ I I 0.010 O.D15 0.020

Cd

-<

--l

-��

0.025

� I I I I /J;6 ts I I �

5 1 I VeS I I I I I � 9 0 �LZ1Jl l I l d 8

I

� I I I I I I I I � -3 0 3 6 9

Alpha 12 15 18

F ig . 7 XFOIL calculations compared wi th wind tunne l te s t results from [ 1 0 ] for the NASA LS ( l ) - 0 4 2 1 MOD airfo i l .

I i\ I I I "'! -

I � \ I I 1 5

I I \ 1 1 \ I l d0

r+�----��------� 0

0.0 0.5 xtr/c

0

1 .0

1-Ij 1-Ij �

t-3 z

I-' "' 1.0 0 I

I-' V1

""' w

FFA TN 1 9 9 0 - 1 5 4 4

0

0

C! c

"' 0

XFOIL calculations at Re=3E6, free rransition with Acrit=9

XFOIL calculations at Re=3E6, forced transition at Xtrs=O.Ol and Xtrp=O. l

---- ISES calculations at Re=3E6, free transition with Acrit=9

I I I I I i

I I I I

I � / I I I

I i I

ISES calculations at Re=3E6, forced transition at Xtrs=O.Ol and Xtrp=O. l

! I ! i

i !

� ,% �

J� I ! I I I I '

I

! I I I I ..Ar-n I 1 � 1 i � 66 ; I _;,1··-r ! I � � I

I I I I ' I I

I

I I

� I ! ' I

I I I I I I I

I . . " I i I I I I I I I

I I

I I '

I I I

N c:?

c 0

E u

-4 -2 0 2 4 6 8 10 12 14 16 18

Fig . 8

lm tTl ,..,..,

,} � ,-

�

Alpha

Compari son between I SES and XFOI L calculat ions for the AK1 5 v4 a i rfo i l ( e s sentially the same ai rfo i l as

the FFA-Wl - 1 5 2 ) .

Wind tunnel test at Re=3E6 with smooth airfoil

Wind tunnel test at Re=3E6 with roughness strips at x/c=S%

ISES calculations at Re=3E6, free transition with Acrit=9

ISES calculations at Re=3E6, forced transition at Xtrs=O.Ol and Xtrp=O.I

� � �.C I (T) (l} hr:lt"!l "' "' l .m.

� ' I.:) U iJC)C) .�

A �· � � C) C) trl'

�.,J w """ ..... .... v.........a !!f!J ( PC)U ' � � �

l6 . . 1

-4 -2 0 2 4 6 8 10 12 14 16 18 20 22 24 26 Alpha

F i g . 9 Compari son be tween ISES and wind tunne l re su l t s [ 3 ] for the AK1 5v4 a i rfo i l .

0 c--i

"1 -

� -

lrl 0

- · · - · · - FFA-W1-1 52, constant Re=3E6

FFA-W1- 1 52. Re*Cl=3E6

� -� /

J '(

l !J . I .

� I'-\

1\ '

-

0 c--i

"1

- o U ,....;

lrl 0

-r-: II

I L_

v I

I J ,_

-

1/ I v IV

I I

_j II

....

L.

� � ......

--

- -

"<t c:) .

C"l c:)

I

8 � u q

-9

'\ �

v I,

I I --

r� tl \

..,.. / . -

-

� · .-'

- . 0.000 0.005 0.010

Cd 0.015 0.020 -3 0 3 6 9 1 2 1 5 0.0 0.5

xtr/c Alpha

Fig . l O a XFOIL c alculations for the FFA-Wl - 1 5 2 ai rfo i l at a cons tant Re= 3 mi l l ion and calculat ions at Re x CL=3 mi ll ion .

I � J V,l .;, · / ,/

... 1 .0

0 c--i

"1 -

o -,....; U

lrl 0

tlj tlj �

1-3 z

I-' 1.0 1.0 0 I

I-' U1

""" U1

FFA TN 1 9 9 0 - 1 5 4 6

1 80

1 60

1 40

1 20

1 00

8 0

60

40

20/

I . .

0

/ .

- · · - · · - FFA-W 1 - 1 52, constant Re=3E6 FFA-W 1 - 152, Re*Cl=3E6

V/ � � / ,··

0 ,/

I I .

v .. / L I .

/

w·v j

.'

. 'h'

j �· I

lj . i

/ I .

1/

� '

� \ 1\

\ � 1 ', . \ \

''

0.2 0.4 0.6 0.8 1 .0 1 .2 1.4 1 .6 CL

Fig . l Ob The l i f t/drag ratio versus C1 . XFOIL calcula­t ions for the FFA-Wl- 1 5 2 at a cons tant Re= 3 mi l l ion and calculat ions at Re x C1 = 3 mi l l ion .

0 C"i

"1 .....

� .....

lr) d

- · · - · · - FFA-W2- 1 52, Constant Re=3E6

FFA-W2-1 52, Re*Cl=3E6

-. � -

� _... -

,.,... � I

�· I t ! \ \ .

\ . .

· --

0 C"i

lr)

- o u �

V') d

-

I

J v

v 1-I 1-" 1-" r-

- � :;....

I I v v

v I

---

I I I :

• • f-': �

"<t d I

� d

I

E f'! U 9

..... 9

'-

"'\ I"-�

' L. -

- � I-- v 1.:. · [7 .

17 . . . _A 0.000 0.005 0.010

Cd 0.015 0.020 -3 0 3 6 9 1 2 1 5 0.0 0.5

xtr/c Alpha

Fig . l la XFOIL calculations for the FFA-W2 - 1 5 2 airfo i l at a cons tant Re=3 mi l l ion and calculations at Re x C1=3 mi l l ion .

t--

---! ----1

-� 1 7f -1

J v,� It

--j

I 1 .0

0 C"i

"!

� o .....

V') d

1-tj 1-tj :;c:. 1-j z I--' \0 \0 0 I

I--' lJl

ol:» -..J

FFA TN 1 9 9 0 - 1 5 4 8

1 80

1 60

140

1 20

1 00

80

60

40

20

0 0.2

FFA-W2- 1 52, constant Re=3E6 FFA-W2- 1 52, Re*Cl=3E6

� � \ ./ V . v \ I / .'

/ I ' i/

v . ·� I I \ v·

I \\ I

/ \

0.4 0.6 0. 8 1.0 1 .2 CL

\ . \ ;

\\ \

\I\ \

1 .4 1 .6

Fig . l lb The l i f t/drag rat io ve rsus C1 . XFOIL calculations for the FFA-W2 - 1 5 2 airfo i l at a cons tant Re=3 mi l l ion and calculationd at Re x C1= 3 mi l l ion .

5

FFA TN 1 9 9 0 - 1 5 4 9

- · · - · · - FFA-W2-152, Cl*Re=3E6 FFA-Wl -152, Cl*Re=3E6

1 80

/ " " . .

. \ 1 60 /

. . .

/ .

\ .

I \ 1 40 I .

\ I .

. \ I 1 20

I \ .

. \ .

I 1 00 .

. . \ I .

. \ I 80

� . \ / .

. . \ .

I .

60 \ .

\ .

.

40 \ .

\ .

.

20 \

0�----�------�------�----�------�------�----�----� 0.2 0.4 0.6 0.8 1 .0

Cl 1 .2 1 .4 1 .6

F i g . l 2 The l i ft/drag ratio versus C1 for the FFA-Wl- 1 5 2 and the FFA-W2 - 1 5 2 a irfoil when calculat ions are made at Re x C1= 3 mi l l ion .

1 .8

FFA-Wl -1 52

- · · - · · - FFA-W2-152

- ---- - - -- - - - - · . .. . . . . · · - · · - · · - · · - · ·

:;::;..-- ··

=-----· ·

='"""

" "

F ig . l 3 The FFA-Wl- 1 5 2 and FFA-W2 - 1 5 2 a i r fo i l s plotted supe rimpo sed o n each other .

1-rj 1-rj :t:' t-3 z 1-' 1.0 1.0 0 I 1-'

U1

U1 0

FFA-W 1-27 1 - - - - - FFA-W1 -242

--- - - FFA-W1-21 1

------------- FFA-W 1 - 1 82 FFA-W1 -1 52

- · · - · · - FFA-W1-1 28

F ig . l 4 The FFA-Wl -xxx airfo i l s p lotted superimpo sed on each othe r .

1-rj '"':! :t:' t-3 :::1 I-' '-0 '-0 0 I

I-' Ul

Ul I-'

FFA TN 1 9 9 0 - 1 5 , ..... .. ...

I

·2.0

·1 .S Cp -1.0

..o.s

0.0

o.s

1.0

5 2

FFA-W1-271 MAOl =0.1SO

RE = 1 .000 X 10 6 ALFA = 8.000

Cl = 1 . 1 1 7

CM = -0.076

CD = 0.02278

LJD = 49.04

- - -

Fig . l 5 a The FFA-Wl - 2 7 1 airfoi l . Calculat ions at an angle of attack s l ightly above the de s i gn angle of at­tack . Re=l mi l l ion and the tran s i tion i s forced at x/c=5 % at both s i de s o f the airfoil .

• z.o FFA-W1-271

·l.S ..

Cp .. ' -1.0

..o.s

0.0

o.s

1.0

' ' ' ' ' ' '

MAOl =O.!SO

RE = 1 .000 X 10 6 ALFA = 2.000

Cl = 0.428

CM = ..0.062

CD = 0.01914

LJD• .. 22.34

Fig . 1 5b Calculations at a low angle o f attack at Re= 3 mi ll ion and wi th forced tran s i t ion at 5 % x/c on both s ides o f the airfo i l .

=

"'! -

� -

V) 0

0 0

0.000

FFA-W l - 1 52 FX 84-W- 1 5 1

NACA 63-615

NASA LS(l )-041 5-MOD

· -

-- · · - - · ·

. .......-/. -- · · I-- "

/ . .. ............... 1;::' •• -···· ..

............. ...............

v; rr /":. . ...........

....

/ .. � I--.... -··

.· ... ··· +-:::: -

I w-·-- . -.1: v _ ... . ... � - f- -"' ··J"' . .1/ --.·· ......

f . t) v _ / v· / v . : r, : ; ff' . .i i� .

, \ . .

\\\ .

I "1 I I I I 71' /...-:"'J>4"" J �

9 {/······· ""! .f

� I I I //.·'l'/t-"' h•-.J I I \ -. -\\ I ! I if t � 0 I

0 ���[ 1 I d c "1 0 . - . - ,.-....:.:.:.. . . : ......... / 0

I

I\ g r I I I I I I g H---------��---------1- 0 0

0.005 0.010 0.015 Cd

��-0.020 0.025 -3 0 3 6 9

Alpha 1 2 15 0.0 0.5

xtr/c

F ig . l 6 XFOIL calculations for four �1 5 % thick a ir fo i l s . Re= 3 mi l l ion , and M=O . l S .

l ) Free tran s i tion and Acri t=9 . 2 ) Forced tran s i tion at x/c=l% at the suction s ide and

x/c=l O % at the pre ssure s ide .

1 .0

-u

1-Ij 1-Ij :t:' t-3 z 1--' 1.0 1.0 0 I

1--' lJl

lJl w

"'! ......

� ......

II') 0

0 0

50% FFA-W1-21 1 and 50% FFA-W l -242 - - - - - FX 84-W-21 8 ......................... NACA 63-621

- · · - · · - NASA LS(l )-0421 -MOD

- ---- - - -- -·--·� - ---r-

� I I I I . ··f/ Y,.. I d I

:3 1 I 1.:.=77/l .. / :p I rd I

0 1---- - - --Ji<J.� I I "1 ··�J� :5 o r .,_.... -:-..... �d

8 I

� I I I I I I I � . . . . . .

0.000 0.005 0.010 0.015 0.020 0.025 -3 0 3 6 9 Alpha

1 2 15 0.0 0.5 xtr/c Cd

F i g . 1 7 XFOIL calculations for four R:�2 1 % thick ai rfoi l s . Re=3 mi l l ion , M=O . 1 5 .

1 ) Free t rans i t ion and Acrit= 9 . 2 ) Forced trans i tion at x/c= l % at the suction s i de and at

x/c=l O % at the pres sure side .

{ --

1 .0

"1

q '

lr) 0

q 0

-u

l'tj l'tj ::t:'

t-3 z

I-' 1..0 1..0 0 I I-'

U1

U1 ,j::.

FFA TN 1 9 9 0 - 1 5 5 5

LS( 1 )-042 1 MOD

FX 84-W-2 1 8

NACA 63-62 1

Interpolated airfoil , 50% FFA-W 1 -2 1 1 and 50% FFA-W 1 -242

F ig . l 8 The four airfo i l s used in the calculat ions presented in Fi g . l 7 .

FFA TN 1 9 9 0 - 1 5 5 6

F i g . l 9 FFA Wl -xxx airfo i l s .

FFA TN 1 9 9 0 - 1 5 5 7

F i g . 2 0 FFA-W3-xxx airfo i l s .

FFA TN 1 9 9 0 - 1 5 5 8

Fig . 2 1 FFA-W3 -xxx airfo i l s .

FFA-W3-360 - - - FFA-W3-332

- - - - - FFA-W3-301 - - - - - - - - - - - - - FFA-W3-270 - · · - · · - FFA-W3-241

FFA-W3-21 1

------------- 50% FFA-W3-21 1 and 50% NACA 63-6 1 8

Fig . 2 2 The FFA-W3 -xxx plotted superimposed on each other .

� � � 1-3 z ...... � � 0 I

...... U1

U1 �

FF TN 1 9 9 0 - 1 5 6 0

-2.0 FFA-Wl-128 MACH = 0. 150

ALFA a.. CM -1 .5 -2.706 0.0000 -0.046

- 1 .071 0.2000 -0.048

Cp 0.568 0.4000 -0.05 1 2.210 0.6000 -0.054 3.854 0.8000 -0.056

-1.0 5.500 1.0000 -0.059 7.148 1.2000 -0.062 8.799 1.4000 -0.066

10.45 1 1.6000 -0.069 -0.5 12.104 1.8000 -0.072

F ig . 2 3 a

0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 6 1

-2.0 FFA-Wl -128 MACH = 0. 1 50

RE = 3.000 X 1 0 6 ALFA = 5.000

-1 .5 CL = 0.926

CM = -0.058

Cp CD = 0.00535

-1 .0 LID = 173.23

-0.5 Fig . 2 3b

0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 6 2

-2.0 FFA-Wl- 152

MACH = 0. 1 50 ALFA CL CM

-1 .5 -2.985 0.()()()() -0.05 1 - 1 378 0.2000 -0.053

Cp 0.232 0.4000 -0.057 1.845 0,6000 -0.060

- 1 .0 3.460 0.8000 -0.064 5.078 I.()()()() -0.068 6.699 1.2000 -0.072 8.323 1.4000 -0.076 9.950 1.6000 -0.080 -0.5

ll.579 1.8000 -0.084

F i g . 2 3 c

0.0

0.5

1 .0

-2.0

-1 .5

Cp -1 .0

-0.5

0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 6 3

FFA-Wl- 152 MACH = 0. 1 50

RE = 3.000 X 10 6 ALFA = 6.000

CL = 1 .085

CM = -0.067

CD = 0.00629

LID = 1 72.62

F i g . 2 3 d

FFA TN 1 9 9 0 - 1 5 6 4

-2.0 FFA-Wl- 182 MACH = 0. 1 50

ALFA __fL_ CM -1 .5 -2.807 0.0000 -0.056

-1.219 0.2000 -0.060

Cp 0.370 0.4000 -0.064 1 .962 0.6000 -0.068

- 1 .0 3556 0.8000 -0.072 5.152 1.0000 -0.076 6.750 1.2000 -0.080

8351 1.4000 -0.084 9.954 1.6000 -0.088

-0.5 1 1 .560 1.8000 -0.092

F i g . 2 3e 0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 6 5

-2.0 FFA-Wl- 182 MACH = 0. 1 50

RE = 3.000 X 10 6 ALFA = 6.000

- 1 .5 CL = 1 .073

CM = -0.074

Cp � \ CD = 0.00692

� LID = 1 55.09 �

-1 .0

F i g . 2 3 f -0.5

0.0

0.5

1 .0 c ___ �----=�---

FFA TN 1 9 9 0 - 1 5 6 6

-2.0 FFA-Wl-21 1 MACH = 0. 1 50

ALFA CL ___QL_ -1.5 -2.741 0.0000 -0.072

-1 .176 0.2000 -0.076

Cp 0.390 0.4000 -0.080 1.958 0.6000 -0.083

- 1 .0 3.528 0.8000 -0.087 5.099 1.0000 -0.09 1 6.674 1.2000 -0.094

8.250 1.4000 -0.098 9.829 1.6000 -0. 101

-0.5 1 1 .4 1 1 1.8000 -0. 104

Fig . 2 3g

0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 6 7

-2.0 FFA-W1-21 1 MACH = 0. 1 50

... - - - - ..

RE = 3.000 X 1 0 6 ALFA = 6.000

-1 .5 CL = 1 .072

CM = -0.087

Cp CD = 0.00778

LID = 1 37.73 -1 .0

F i g . 2 3h -0.5

0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 6 8

-2.0 FFA-Wl -242 MACH = 0.150 ALFA CL CM

-1 .5 -2554 0.0000 -0.079 - 1 .023 0.2000 -0.083

Cp 0509 0.4000 -0.087 2.042 0.6000 -0.092

-1 .0 3576 0.8000 -0.096 5 . 1 12 1.0000 -0.100

6.65 1 1.2000 -0.104

8.192 1.4000 -0.107 9.735 1.6000 -0. 1 1 1

-0.5 1.8000 -0. 1 14

Fi g . 2 3 i

0.0

0.5

1 .0

-2.0

-1 .5

Cp -1 .0

-0.5

0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 6 9

FFA-Wl-242 MACH = 0. 1 50

RE = 3.000 X 10 6 ALFA = 6.000

CL = 1 .058

CM = -0.093

CD = 0.00901

LID = 1 1 7.36

F i g . 2 3 j

FFA TN 1 9 9 0 - 1 5 7 0

-2.0 FFA-Wl-27 1

MACH = 0.150

� a.. CM -1.5 -2376 0.0000 -0.084

-0.880 0.2000 -0.089

Cp 0.617 0.4000 -0.094 2. 1 15 0.6000 -0.099 3.614 0.8000 -0.103 - 1 .0 5.115 1 .0000 -0.108 6.618 1.2000 -0. 112

8.123 1.4000 -0. 1 1 6 9.63 1 1.6000 -0.120

-0.5 1.8000 -0. 123

F i g 2 3 k 0.0

0.5

1 .0

-2.0

-1 .5

Cp -1 .0

-0.5

0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5

\ \

7 1

:-..

FFA-Wl-271

MACH =0.150 RE = 3.000 X 10 6 ALFA = 6.000 CL = 1 .064 CM = -0.103 CD = 0.01016 LID = 104.70

Fi g . 2 3 1

FF TN 1 9 9 0 - 1 5 7 2

-2.0 FFA-W2-1 52

MACH = 0.150

ALFA CL ___QL -1 . 5 -2.469 0.0000 -0.046

-0.859 0.2000 -0.049

Cp 0.755 0.4000 -0.053 2.370 0.6000 -0.057

-1.0 3.988 0.8000 -0.061

5.608 1.0000 -0.065 7.23 1 1.2000 -0.069 8.855 1.4000 -0.073

10.481 1.6000 -0.077 -0.5 12.108 1.8000 -0.08 1

0.0 Fi g . 2 4 a

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 7 3

-2.0 FFA-W2-1 52

MACH = 0.150 RE = 3.000 X 10 6 ALFA = 5.000

-1.5 CL = 0.907 CM = -0.061

Cp CD = 0.00547

LID = 165.79 -1 .0

-0.5

F i g . 2 4 b 0.0

0.5

1 .0 --------------

FFA TN 1 9 9 0 - 1 5 74

-2.0 FFA-W2-210

MACH = 0.150

� CL CM

-1.5 - 1.573 0.0000 -0.039 -0.009 0.2000 -0.044

Cp 1 .556 0.4000 -0.048 3.122 0.6000 -0.052

-1.0 4.690 0.8000 -0.056 6.259 1.0000 -0.061 7.829 1.2000 -0.064 9.401 1.4000 -0.068

10.975 1.6000 -0.072 -0.5 12.55 1 1.8000 -0.075

Fi g . 2 4 c 0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 7 5

-2.0 FFA-W2-210 MACH =0.150 RE = 3.000 X 10 6 ALFA = 6.000

-1 .5 CL = 0.934 CM = -0.055

Cp CD = 0.00731 LID = 127.72

-1 .0

-0.5

0.0 Fi g . 2 4 d

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 7 6

-2.0 50% NACA 63-618 AND 50% FFA-W3-2 MACH = 0.000

ALFA CL CM

-1 .5 -3.882 0.0000 -0.103 -2.280 0.2000 -0.107

Cp -0.677 0.4000 -0.1 1 1 0.928 0.6000 -0. 115

-1 .0 2537 0.8000 -0. 1 1 8 4.152 1.0000 -0.122 5.773 1.2000 -0.126 7.401 1.4000 -0.130 9.039 1.6000 -0.133

-0.5 1.8000 -0.137

Fig . 2 5 a 0.0

0.5

1 .0

-2.0

-1 .5

Cp -1 .0

-0.5

0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5

_ .. . - - .. - - - -

c_

7 7

50% NACA 63-618 AND 50% FFA-W3-2 MACH = 0.150 RE = 3.000 X 10 6 ALFA = 5.500 CL = 1 . 1 15 CM = -0.1 14 CD = 0.00759 LID = 146.80

Fig . 2 5 b

FFA TN 1 9 9 0 - 1 5 7 8

-2.0 FFA-W3-21 1 MACH = 0.150 ALFA _____£L_ ___Q:L.

-1 .5 -3.205 0.()()()() -0.087 -1.638 0.2000 -0.090

Cp -0.069 0.4000 -0.094 1 500 0.6000 -0.098

-1 .0 3.072 0.8000 -0. 101 4.646 1.()()()() -0.105 6.223 1.2000 -0.108 7.802 1.4000 -0. 1 12 9383 1.6000 -0. 1 1 5

-0.5 1.8000 -0.1 1 8

0.0 Fig . 2 5 c

0.5

1 .0

FFA TN 1 9 9 0- 1 5 7 9

-2.0 FFA-W3-21 1 MACH = 0.150 RE = 3.000 X 10 6 ALFA = 6.000

-1 .5 CL = 1 .125 CM = -0.101

Cp CD = 0.00788

LID = 142.78 -1.0 !>.

!>.

-0.5

0.0 Fig . 2 5 d

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 8 0

-2.0 FFA-W3-241 MACH = 0.150

ALFA Cl. CM

-1.5 -3.154 0.()()()() -0.095

- 1.626 0.2000 -0.100

Cp -0.097 0.4000 -0.104

1.433 0.6000 -0.108

2.965 0.8000 -0. 1 12 -1.0

4.499 1.()()()() -0. 116

6.035 1.2000 -0. 1 19

7.575 1.4000 -0.123

9.117 1.6000 -0.126

-0.5 1.8000 -0.129

Fig . 2 5e 0.0

0.5

1 .0

---� �----

FFA TN 1 9 9 0 - 1 5 8 1

-2.0 FFA-W3-241 MACH =0.150 RE = 3.000 X 10 6 ALFA = 6.000

-1 .5 CL = 1 .141 CM = -0. 1 1 1

Cp CD = 0.00915

LID = 124.66 -1 .0

-0.5

0.0 Fig . 2 5 f

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 8 2

-2.0 FFA-W3-270 MACH = 0.150

ALFA Cl.. _QL_ -1 .5 -3.099 0.0000 -0.097

-1.604 0.2000 -0.102

Cp -0.107 0.4000 -0.107

1.390 0.6000 -0.1 12

2.890 0.8000 -0. 117 -1.0

4.391 1.0000 -0.121

5.895 1.2000 -0. 125

7.401 1.4000 -0.129

8.9 1 1 1.6000 -0.133

-0.5 1.8000 -0.137

0.0 Fi g . 2 5 g

0.5

1 .0

---· ·---

FFA TN 1 9 9 0 - 1 5 8 3

-2.0 FFA-W3-270 MACH = 0.150 RE = 3.000 X 10 6 ALFA = 6.000

-1.5 CL = 1 .144 CM = -0. 1 1 5

Cp CD = 0.00991

LID = 1 15.52 -1.0

-0.5

Fig . 2 5h 0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 8 4

-2.0 FFA-W3-301 MACH = 0.150

ALFA _9:._ CM -1 .5 -3394 0.0000 -0.108

-1.936 0.2000 -0.113

Cp -0.478 0.4000 -0.119

0.982 0.6000 -0.124

-1.0 2.444 0.8000 -0.130

3.907 1.0000 -0.135

5373 1.2000 -0.140

6.841 1.4000 -0.144

8312 1.6000 -0.149

-0.5 1.8000 -0.153

0.0 Fig . 2 5 i

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 8 5

-2.0 FFA-W3-301 MACH = 0.150 RE = 3.000 X 10 6 ALFA = 6.000

-1.5 CL = 1 .201 CM = -0.1 29

Cp CD = 0.01 1 55 LID = 103.98

-1 .0

-0.5

0.0 Fi g . 2 5 j

- -

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 8 6

-2.0 FFA-W3-332

MACH = 0.150

� CL ___QL -1 .5 -3.620 0.()()()() -0. 1 1 4

-2.197 0.2000 -0.120

Cp -0.773 0.4000 -0.127

0.653 0.6000 -0.133

-1 .0 2.079 0.8000 -0. 138

3508 1.()()()() -0.144

4.939 1.2000 -0.150

1.4000 -0.155

1.6000 -0.160

-0.5 1.8000 -0.164

Fig . 2 5k 0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 8 7

-2.0 FFA-W3-332 MACH =0.150 RE = 3.000 X 10 6 ALFA = 6.000

-1.5 :-. CL = 1.238

� CM = -0.136 Cp � CD = 0.01309 :..

LID = 94.62 -1.0

-0.5

Fig . 2 5 1 0.0

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 8 8

0.5

1 .0

FFA TN 1 9 9 0 - 1 5 8 9

-2.0 FFA-W3-360

MACH = O.OOO RE = 3.000 X 10 6 ALFA = 6.000

-1 .5 CL = 1.309 CM = -0. 145

Cp CD = 0.01412

LID = 9269 -1.0

-0.5

0.0 F ig . 2 5n

- -

0.5

1 .0

FFA TN 1 9 9 0- 1 5 9 0

1 80

1 60

140

120

1 00

80

60

40

- - - - - - - - - POL.W128_30_9 and POL.W128_30_TU1 - - - - - - - - - - - - - POL.W271_30_9 and POL.W27 1_30_TU1 - ··-· ·-··-··-·· POL.W242_30_9 and POL.W242_30_TU1 - - - POL.W21 1_30_9 and POL.W21 1_30_TU1 - · · - · · - POL.W182_30_9 and POL.W182_30_TU1

POL.W152_30_9 and POL.W152_30_TU1 - - - - - - - - - POL.W1 28_30_9 and POL.W128_30_TU1

\ \ \

\ \ \ \ \ \

\ '

\ \ \ ' ' ' ' '

·,

o�-------r-------.--------r-------�------�------�--------�------4 0.2 0.4 0.6 0.8 1 .0

Cl 1.2 1 .4 1 .6

Fig . 2 6 The l i ft/drag ratio versus c1 • XFOIL calculation s for the FFA-Wl-xxx airfo i l s at Re= 3 mi l l ion and M=O . 1 5 .

1 ) Free transition with Acrit= 9 . 2 ) Forced tran s ition at x/c=l % at the suct ion s i de

and x/c=l O % at the pre s sure s i de .

1 .8

FFA TN 1 9 9 0 - 1 5 9 1

- · · -e- · · - POL.W2_210_30_9 and POL.W2_210_30_TU1 e POL.W2_152_30_9 and POL.W2_152_30_TU1

- · · - · · - POL.W2 1 1_30_9 and POL.W21 1_30_TU1 ---- POL.W152_30_9 and POL.W152_30_TU1

180 �------------------------------------------------------.

1 60

140

120

100

80

60

40

- - - - � . .

\ . . \ . \

.

\

0+-----�------�----�------�----�------�----�----� 0.2 0.4 0.6 0.8 1 .0

Cl 1 .2 1 .4

Fig . 2 7 The l i ft/drag ratio versus c1 • Compari son o f FFA-Wl airfo i l s and FFA-W2 airfoi l s .

1 .6 1 .8

"'! ....

q ....

VI 0

q 0

- - - - - - - - - - - - - POL.W271_30_9 -··-··-··-··-·· POL.W242_30_9 - - - POL.W21 1_30_9 - · · - · · - POL.W1 82_30_9

POL.W152_30_9 - -------- POL.W128_30_9

� - - - -=-... :.=.:--.. -.. t"'"" r"'" !."'_" .,:.:' f'"" ,_.., I .

_,:1-r -1-- - - - - -.� ,., . . -

�j:?.; , ,. v (' i/"t """

�l;" j_ ,' • If i ,l l_ I ,,'/ I I

1 i : I • .1 i I

i i I i I \ I

� i : !� I I

\ \' : \ \ _:

, ...... : I IU ' � I I r\

\l � t . '"' � �'·r__ ...

0

k?f�

I�

5 1 1 1 1 1 1 1 1 100 1 1 1 1 1 1 1 1 1 1 1 1 � � d I I I I I IJJitf.m.t±�.dJ I I I I I � �·1-fi�l. l"'•'t--

m-� F4""'1-l-r �

I I I r ""T"""'' · �I

�i lilf 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 � f.l. 1 /JL �-; fti 0.000 0.005 0.010 0.015

Cd 0.020 0.025 0.030 -6 -3 0 3 6 9

Alpha 12 15 18

Fig . 2 8 FFA-Wl-xxx airfo i l s . XFOIL c alcul ations at Re=3 mi l l ion , M=O . lS , free transition and Acrit=9 .

8

l'tj l'tj ;r:,o t-3 z I-' 1.0 1.0 0 I I-' U1

1.0 N

"'! -

0 -

11"1 0

0 0

0.000 0.005

POL.W271_30_TU1

POL.W242_30_ TUl

POL.W21 1_30_TU1

POL.W1 82_30_ TUl

POL.W152_30_TU1

POL.W1 28_30_TU1

· ' "

�· �

/ ')

! VI I J : / 1 I

1 1/ i I I I r / . I I ;

·�· � I , . "

i \

0.010

/ /. r-'/ �, r'l' / w. :I I I

If : I I

i I

i I I I

0.015 Cd

I/ I

I I

�-- - -- · � -

� --� ... � - - -.. ..

.. ,

0.020

-

- -

0.025

1.-• - -

1- ·

'

' I I 0

I I

0.030

"'! -

C! -

It") 0

0 0

I I

r--""" f-r--r-- I. r- .

:v -6 -3

I

I

0

"

/�- ,..... : ��� � ..

If

� 1; ·� )}/

- - - .. 'j; -,... - 1-I-.. • -f - - -

3 6 9 Alpha

-:-jii.:: -

.:. .:-1::.

-..!.

12 15 18

Fig . 2 9 FFA-Wl-xxx airfo i l s . XFOIL calculations at Re= 3 mi l l ion , M=O . 1 5 , forced transition at x/c=l % at the suct ion s ide and x/c=l O % at the pre s sure s ide .

M

<:?

N <:?

-�

0 0

E u

ttj ttj � 8 z 1-' \0 \0 0

I 1-' Ul

\0 w

FFA TN 1 9 9 0- 1 5 9 4

I:> 0' 1

.... � · -� �' .

\I' !\ ,\ l\� ..1.

f-;:::; . . . . ,........ \ ' .·�/ ? '.1

II � I\.' · I/

-�

W:) ro-

\ It' . I \ _\ j \ 'I' \ I� �

""'' "'

"' !'-.. � ....... .... loll.

"'

0' 1 I:>

I i I .

I \ \ . \ i\

� \ � \ \

� r\. � ...

I': 1=::. r- · -I- . �

O"l 0'1

o·o

. . -:::;;; -r-:;;..

�\ �·

-

o·o

11 j 1 I

["-... c--. j_ � l_ '

o·o

. -1- ' . -....._. ..

o·o

- -

"'""" r-...

� / -It_' •

�-- -r- ""

0 0

00 -

"' -

C"l -

0'1

� ....o ..C:

0..

(")

0

(") I

\0 I

s 0

8 0

-<

cO 0 C"1 . tJ'> ·r-1 11-t

0 C"i

"l -

q -

V') d

0 d

- - - - - POL W 1 28 10 9 . - -

- · · - · · - POL.W1 28_10_TU1

r T I I I

- -

. .... - . . 1-- • .

1.. .v . .

I / . .

-

. ,·

I 1 / I .

..... I -

'---- ; ' I -

i -y 1. l '

I -

1- \.

1

-;;;;;;

t--t---

-

-

-

-

I I J I I 1 I I I I I I I

0.00 0.01 0.02 Cd

0.03 0.04

-u

q N

"l -

q -

V') d

0 0

-1- 1-"'"'"

1./ I)

I

-6 -3

v 1--fft-v

0

J ,

�:-·

""�-" J' _L " �

�,. 1!.'

I J

I )

1-"' r- . - . . .. i-="1"'·

3 6 9 Alpha

Fig . 3 0 b

� t:= . .. �o-n .

1-f- .I-"""' I

I I I

12 15 18

"<t c?

� C?

N 9

-c?

0 0

E u

1 \ """

I'

L / J

i l II I I

0.0

1-...

! \ \ '

' � -t-

0.5 xtr/c

' ' ' '

,. -- f-""

I

I ,/

1 .0

0 C"i

"l -

q -

V') d

0 d

"tj 1-rj :t:" t-3 z ...... \0 \0 0 J

...... Ul

\0 - Ul u

FFA TN 1 9 9 0 - 1 5

-:::::> 0\ � o1 o1

('(')I ('(')I 00 00 N N - -� � � �

o·z

o·z

L ""'"""' ....

£·o-

\ I''"'

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I s suing organ i sa t ion Document No .

FFA TN 1 9 9 0 - 1 5 Date Security

The Aeronautical Re search Institute of Sweden Aerodynamic s Department P . O . Box 1 1 0 2 1

Apri l 1 9 9 0 UNCLASSIFIED

S - 1 6 1 11 B ROMMA Sponsor ing agency Proj ec t No .

The National Energy Adminis tration ( STEV)

Fdok

T i t l e

AU- 3 2 3 1

No . of pages

1 4 8 Order/cont�ac t

5 0 6 2 6 6 - 4/ 8 9 - 0 6 - 2 2 S TEV 8 9 / 9 0

Test programme

COORDINATES AND CALCULATIONS FOR THE FFA-Wl-xxx , FFA-W2 -xxx AND FFA-W3-xxx SERIES OF AI RFOILS FOR HORI Z ONTAL AXIS WIND TURBINES

Autho r ( s ) Work perf ormed by

Anders Bj orck Anders B j orck Checked by Approved by c . -A� J 'A ;hL&,Nh?# <t'} 'C ��s ta\[,.�;;nv--

1 Btirn Montgome&(e Head , Aerodynami c s A2 ��----------------------------------�-------------------------------

Ab strac t s -----1

Airfo i l s for use on hor i z ontal axi s wind turbines have been de­s i gne d . The airfoi l s a re devided into three d i f ferent serie s :

I The first serie s , FFA-Wl-xxx , constitute s airfo i l s with thicknes s to chord ratios from 1 2 . 8 % to 2 7 . 1 % . The des i gn l i ft coeffic ients fo r the FFA-Wl-xxx series range from 0 . 9 for the 1 2 . 8 % airfoi l , 1 . 0 5 for a 1 5 . 2 % airfo i l to 1 . 2 for the 2 7 . 1 % a irfo i l .

Two ai rfoi l s in a se cond series FFA-W2 -xxx are des i gned with de­s i gn l i ft coe fficients approximate ly 0 . 1 5 units lower than that for the FFA-Wl-xxx serie s .

The third series o f airfoi l s constitute s airfo i l s with thickne s s t o chord ratios ranging from 1 9 . 5 % t o 3 6 % . The 2 1 . 1 % and 1 9 . 5 % thick airfo i l s are de s i gned to conform to thinner NACA 6 3 - 6 0 0 airfo i l s which are then to be used for the outer parts o f the wind turbine bl ade . The thicker airfo i l s are de s i gned to o ffer better aerodynamic performance for a given thickne s s to chord ratio than thick NACA 6 3 - 6 0 0 airfo i l s .

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STEV FFA Copy No .

1 - 1 0 1 1- 9 0

FL YGTEKNISKA FORSOKSANSTALTEN The Aeronautical Research Institute of Sweden

FF A TN 1990-15

APPENDIX

COORDINATES AND CALCULATIONS FOR THE

FFA-Wl-xxx, FFA-W2-xxx AND FFA-W3-xxx SERIES

OF AIRFOILS FOR HORIZONTAL AXIS WIND

TURBINES

by

Anders Bjorck

Stockholm 1990

FLYGTEKNISKA F�RS�KSANSTALTEN

The Aeronautical Research Institute of Sweden

Aerodynamics Department

FFA TN 1 9 9 0 - 1 5

APPENDIX

COORDINATES AND CALCULATIONS FOR THE FFA-Wl-xxx, FFA-W2-xxx AND

FFA-W3-xxx SERIES OF AIRFOILS FOR HORIZONTAL AXIS WIND TURBINES

by

Anders Bjorck

CONTENTS Page

Polars for the FFA-Wl- series 1 - 4 2

Polars for the FFA-W2 -series 4 3 - 5 4

Polars for the FFA-W3-series 5 5 - 8 9

FFA TN 1 9 9 0 - 1 5 1 POLAR.W152_3 0_ 9; 1

ISES polar driver Version l. 3

Calculated polar for: Airfoil FFA-W1- 152

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1 0 . 0 0 0 1. 4 17 9 0. 0 13 4 6 0. 0 0 0 0 0 - 0. 0 6 1 8 0. 13 0 1 1. 0 0 0 0 1 0. 2 5 0 1. 4 1 65 0. 0 1485 0. 0 0 0 0 0 - 0. 0 6 03 0. 1 1 92 1.0 0 0 0 1 0.5 0 0 1. 4 132 0. 0 1 653 0. 0 0 0 0 0 - 0. 05 9 0 0. 1 0 97 1. 0 0 0 0 1 0.75 0 1. 4 02 6 0. 0 1 8 4 6 0. 0 0 0 0 0 - 0. 05 6 1 0. 1 0 2 6 1. 0 0 0 0 1 0. 8 6 1 1. 3 9 8 9 0. 0 1 9 43 0. 0 0 0 0 0 - 0. 055 4 0. 0 9 9 4 1. 0 0 0 0

FFA TN 1 9 9 0 - 1 5 2 POLAR.W152_ 3 0_TU1;1

ISES polar driver Version 1. 3

Calculated polar for: Airfoil FFA-W1- 152

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Mach • 0. 15 0 Re .. 3. 0 00 e 6 Acrit .. 9.000

alpha CL CD CDi CM S xtr P xtr ------- -------- --------- ----- ---- -------- ------- -------

4 . 00 0 0. 80 6 8 0. 0 1 1 75 0. 0 0 000 - 0. 0 603 0. 0 1 0 0 0. 1 0 0 0 4 . 500 0. 8 605 0. 0 1 2 0 8 0. 0 0 0 00 - 0. 0 6 07 0. 0 1 0 0 0.1 0 0 0 5.00 0 0. 9 137 0. 0 1 2 45 0. 0 0 000 - 0. 0 6 1 1 0. 0 1 0 0 0. 1 0 00 5. 5 0 0 0. 9 657 0. 0 1 2 8 6 0. 0 0 000 - 0. 0 61 3 0. 0 1 0 0 0. 1 0 00 6. 0 0 0 1.0 1 6 4 0. 0 1 3 3 1 0. 0 0 000 - 0. 0 6 1 4 0. 0 10 0 0. 1 0 00 6.250 1. 0 40 4 0. 0 1 35 6 0. 0 0 0 0 0 - 0. 0 6 1 4 0. 0 1 0 0 0. 1 0 0 0 6.500 1. 0 6 44 0. 01 3 8 3 0. 0 0 000 - 0.0 613 0. 0 1 00 0. 1 0 00 6.750 1. 0 879 0. 0 1 4 1 1 0. 0 0000 - 0.0 6 1 1 0. 0 1 0 0 0. 1 0 0 0 7. 0 00 1. 1 10 4 0. 0 1 4 4 2 0. 0 0 000 -0.0 609 0.0 1 00 0. 1 000 7.250 1. 1 325 0.01 47 6 0. 00000 -0. 0 607 0. 0 1 00 0. 1 0 00 7.5 0 0 1. 15 17 0.0 1519 0.00000 -0.0 60 1 0. 01 00 0. 1 0 00 7.75 0 1. 159 8 0. 0 15 87 0. 00000 -0. 05 84 0. 0 100 0. 10 00 8. 0 00 1. 1 697 0.0 1 6 6 8 0.0 0000 - 0. 0575 0.0 100 0. 1 0 00 8.250 1. 1 7 85 0.0 17 62 0. 0 0000 - 0.05 65 0. 01 00 0. 10 00 8.5 0 0 1. 1 8 3 6 0.0 1 87 1 0. 00 000 - 0. 055 1 0. 0 1 00 0. 1 000 8.750 1. 1 93 6 0.0 1990 0. 00000 - 0. 0555 0. 0 100 0.1 0 00 9. 0 00 1. 1937 0. 0 2 1 2 8 0. 0 0000 - 0. 05 2 4 0. 0 1 00 0. 1 0 00 9.250 1. 19 8 8 0. 02278 0. 00000 - 0. 0529 0. 0 1 00 0. 1 0 00 9.5 0 0 1.200 8 0. 0 2 4 3 8 0. 00000 -0. 05 19 0. 0 1 00 0. 1 0 00 9.750 1. 1 9 8 2 0. 0 2 6 0 2 0.00000 - 0. 0 4 8 1 0. 0 1 00 0. 1 0 00 9. 82 4 1.1 9 8 6 0. 0 2 6 6 2 0.00 000 - 0. 049 1 0. 0 1 00 0. 1 0 0 0 9. 8 9 8 1.2 0 62 0. 0 27 11 0. 00 000 -0. 05 2 8 0. 0 1 0 0 0. 1 000 9. 972 1. 200 8 0.02759 0.00000 -0. 0 493 0. 0 1 00 0.1000

1 0. 0 8 3 1. 1 9 85 0.02 84 8 0.00000 - 0.0 47 8 0.0 1 00 0. 1 000 1 0.25 0 1. 2 0 2 4 0. 0297 1 0.00000 - 0. 0 4 89 0. 01 00 0. 1 000 10.5 0 0 1.2007 0. 0 3 1 6 0 0.00000 -0. 0 474 0. 0 1 00 0. 1 00 0 1 0. 6 1 1 1.2 0 3 1 0. 0 32 4 8 0.00000 - 0. 0 4 8 4 0. 0 100 0. 1 00 0 1 0.722 1. 1 9 95 0. 0 3 32 6 0. 00000 - 0. 0 453 0. 0 1 00 0. 1 0 0 0 1 0. 8 3 3 1. 1 9 47 0. 03 4 2 6 0.000 00 - 0. 0 4 3 0 0. 0 1 00 0. 1 0 0 0 1 1. 0 0 0 1.2 0 80 0. 0 355 0 0.00 000 - 0. 04 87 0. 0 1 00 0. 1 0 00

3.5 0 0 0.75 15 0. 0 1 1 45 0. 00 0 00 - 0. 0599 0. 0 1 00 0. 1 0 0 0 3. 0 0 0 0. 6 95 1 0. 0 1 1 17 0. 0 0 0 0 0 - 0. 05 95 0. 0 1 0 0 0. 1 0 0 0 2.5 0 0 0. 6 3 9 8 0 . 0 1092 0. 0 0 00 0 - 0. 0 5 87 0. 0 1 0 0 0.1 0 00 2. 0 0 0 0.5 8 33 0 . 0 1070 0. 0 0 0 00 - 0. 05 8 1 0. 0 1 0 0 0. 1 0 0 0 1.5 0 0 0.5257 0. 0 1 050 0. 0 0 000 - 0. 0575 0. 0 1 0 0 0. 1 0 0 0 1.0 0 0 0. 4 6 8 4 0.01031 0. 0 0 0 00 - 0. 05 69 0. 0 1 0 0 0. 1 0 0 0 0.5 0 0 0. 4 1 13 0. 0 1 0 1 4 0. 0 0 0 00 - 0. 05 6 1 0. 0 1 00 0. 1 0 0 0 0. 0 0 0 0.3535 0. 0 1 00 0 0. 0 0 0 0 0 - 0. 0555 0. 0 1 0 0 0. 1 0 0 0

- 0.5 0 0 0.2 955 0. 0 09 87 0. 0 0 0 0 0 - 0. 05 4 8 0. 0 1 00 0. 1 0 00 - 1. 0 0 0 0. 2 372 0. 0 0 97 6 0. 0 0 0 0 0 - 0. 05 4 1 0. 0 1 0 0 0.1 0 0 0 -1. 5 0 0 0. 17 9 1 0. 0 0 975 0. 0 0 0 0 0 - 0. 05 3 4 0. 0 1 0 0 0. 0 829 -2.00 0 0. 1 2 1 0 0. 0 0 9 8 0 0. 0 0 0 0 0 - 0. 0 527 0. 0 1 0 0 0. 05 8 8 -2 .50 0 0. 0 6 2 9 0. 0 0 9 87 0. 0 0 0 0 0 - 0. 0 5 2 1 0. 0 1 0 0 0. 0 432 -3.000 0. 0 0 4 8 0. 0 0 99 4 0. 0 0 0 0 0 - 0. 05 15 0. 0 1 0 0 0. 0 327 -3.066 - 0. 0 0 2 9 0. 0 0 9 9 6 0. 0 00 0 0 - 0. 051 4 0. 01 0 0 0 . 0 3 0 7 -3.095 - 0. 0 0 62 0. 0 0 9 9 9 0. 0 0 0 0 0 -o . 05 1 4 0. 0 1 0 0 0. 0 2 9 8

FFA TN 1990-1 5 3 PO LAR.Wl82_ 30_ 9; 1

ISES polar driver Version 1. 3

Cal culated polar for: A IRFO IL FFA-W1 - 1 8 2

Vortex + doublet far field Entropy conserved

Mach • 0. 15 0 Re 3. 0 0 0 e 6 A crit "' 9. 0 0 0

alpha CL CD CDi CM S xtr P xtr ------- -------- --------- ------ --- -------- ------- -------

1.0 0 0 0. 45 65 0. 0 05 8 3 0. 0 0 0 0 0 - 0. 06 2 6 0. 45 2 4 0.57 8 1 1.5 0 0 0.5 1 7 2 0.0 05 85 0. 0 0 0 0 0 - 0. 0 6 3 6 0. 4 4 87 0.5 8 65 2.0 0 0 0.5777 0. 0 05 8 8 0. 0 0 0 0 0 - 0. 0 6 47 0. 4 4 35 0.5 95 8 2.5 0 0 0. 6 375 0. 0 0 6 0 4 0. 0 0 0 0 0 - 0. 0 657 0. 4 3 6 6 0. 6 027 3.0 0 0 0. 6 97 8 0. 0 0 6 0 8 0. 0 0 0 0 0 - 0. 0 6 67 0.4 322 0. 6 1 05 3.5 0 0 0.757 9 0. 0 0 6 15 0. 0 0 0 0 0 - 0. 0 677 0. 4 2 65 0. 6 177 4.0 0 0 0. 8 1 6 8 0. 0 0 635 0. 0 0 0 0 0 - 0. 0 6 87 0. 4 1 9 1 0. 6 252 4.5 0 0 0. 877 0 0. 0 0 6 4 0 0. 0 0 0 0 0 - 0. 0 6 97 0. 4 1 3 8 0. 6 3 07 5.0 0 0 0. 9 357 0. 0 0 657 0. 0 0 0 0 0 - 0. 07 0 6 0. 4 0 47 0. 6 3 8 3 5.5 0 0 0. 9 9 4 9 0. 0 0 67 1 0. 0 0 0 0 0 - 0. 07 1 6 0.3 9 6 9 0. 6 4 35 6.0 0 0 l. 0525 0. 0 0 6 95 0. 0 0 0 0 0 -o. 072 4 0.3 8 5 4 0. 65 1 3 6.5 0 0 1. 1 1 0 4 0. 0 07 1 9 0. 0 0 0 0 0 - 0. 0 7 3 2 0. 37 0 8 0. 65 7 1 7.00 0 1. 1 6 6 9 0. 0 07 4 9 0. 0 0 0 0 0 - 0. 0 7 3 9 0. 35 0 3 0. 6 6 33 7.5 0 0 1. 2 2 1 6 0. 0 07 9 6 0. 0 0 0 0 0 - 0. 07 4 4 0. 32 6 6 0. 6 6 9 9 7.75 0 1.2 475 0. 0 0 8 3 1 0.0 0 0 0 0 - 0. 07 45 0. 3 0 9 3 0. 672 4 8.0 0 0 1. 2 7 37 0. 0 0 8 6 3 0. 0 0 0 0 0 - 0. 07 47 0.2 9 4 6 0.67 4 9 8.25 0 1.2 9 8 2 0. 0 0 9 0 2 0. 0 0 0 0 0 - 0. 07 4 6 0.2725 0. 67 8 4 8.500 l. 32 1 9 0. 0 0 9 4 9 0. 0 0 0 0 0 - 0. 0 7 45 0.2525 0. 6 8 2 1 8 . 7 5 0 1.3 4 4 8 0.0 0 9 97 0. 0 0 0 0 0 - 0. 0 7 4 3 0.2 32 6 0. 6 85 0 9. 0 0 0 l. 3 6 6 3 0. 0 1 053 0.0 0 0 0 0 - 0 . 07 3 9 0.2 1 1 1 0. 6 8 75 9. 1 67 1. 37 9 6 0. 0 1 0 95 0. 0 0 0 0 0 - 0. 07 35 0. 1 9 67 0. 6 8 92 9.3 33 l. 3 92 2 0 . 0 1 1 4 0 0. 0 0 0 0 0 - 0. 0 7 3 1 0. 1 8 1 8 0. 6 9 1 2 9. 5 0 0 l. 4 0 3 6 0. 0 1 1 8 4 0. 0 0 0 0 0 - 0. 0 7 2 4 0. 1 67 6 0. 6 9 3 6 9 . 7 5 0 1. 4 1 9 6 0. 0 1 255 0. 0 0 0 0 0 -o. 0715 0. 1 4 8 2 0. 6 9 6 8

1 0. 0 0 0 l. 4 3 3 3 0. 0 1 3 2 8 0. 0 0 0 0 0 - 0. 07 0 2 0. 1 3 1 0 0. 6 9 9 9 1 0. 2 5 0 l. 4 37 1 0. 0 1 4 1 1 0. 0 0 0 0 0 - 0. 0 675 0. 1 1 8 4 0.7 0 27 1 0.5 0 0 1. 4 3 3 4 0. 0 1525 0. 0 0 0 0 0 - 0. 0 6 4 6 0. 1 0 8 3 0.7057 1 0. 7 5 0 l. 4 275 0. 0 1 67 6 0. 0 0 0 0 0 - 0. 0 62 2 0. 0 9 9 8 0.7 0 95 1 1. 00 0 l. 4 2 2 9 0. 0 1 85 6 0. 0 0 0 0 0 - 0. 0 6 1 3 0. 0 927 0. 7 1 2 9 1 1. 2 5 0 1. 4 0 85 0.0 2 0 92 0. 0 0 0 0 0 - 0. 05 87 0. 0 87 0 0. 7 15 8 1 1.50 0 1. 4 0 4 9 0. 0 2 3 3 1 0. 0 0 0 0 0 - 0. 0 6 0 9 0. 0 8 2 0 0 . 7 1 8 1 1 1. 667 1. 3 85 0 0. 0 25 1 9 0. 0 0 0 0 0 - 0. 05 4 1 0. 07 95 0. 7 2 0 0 1 1.833 l . 37 6 8 0. 0 27 2 6 0. 0 0 0 0 0 - 0. 055 6 0. 0 772 0.7 2 2 3 1 2. 00 0 l . 37 3 9 0. 0 2 9 2 6 0. 0 0 0 0 0 - 0. 05 9 0 0. 07 47 0. 7 2 4 4 1 2. 167 l. 3 6 0 1 0. 0 3 1 2 1 0. 0 0 0 0 0 - 0. 05 4 3 0. 072 0 0. 7 2 6 4 1 2. 333 1. 352 1 0. 0 3 3 3 2 0. 0 0 0 0 0 - 0. 05 4 4 0.0 6 9 6 0. 7 2 83 1 2. 44 4 1. 3 4 3 1 0. 0 3 4 8 1 0. 0 0 0 0 0 - 0. 0535 0. 0 6 85 0.7 2 9 3 1 2.5113 1. 3 2 65 0. 0 3 6 6 6 0. 0 0 0 0 0 - 0. 0 4 8 4 0. 0 6 6 6 0. 7 3 1 1 1 2.75 0 l. 3 2 6 9 0. 0 3 8 9 6 0. 0 0 0 0 0 - 0. 05 3 3 0. 0 6 4 2 0. 7 3 2 6 1 2. 79 9 1.3 2 0 8 0.0 3 9 6 1 0. 0 0 0 0 0 - 0. 05 0 7 0. 0 6 3 6 0.7 3 3 3 1 2. 8<!1 9 1. 3 3 2 2 0. 0 4 0 1 4 0.0 0 0 0 0 - 0. 05 7 1 0. 0 62 7 0. 7 3 4 1 1 2. 89 8 l. 3 3 0 6 0. 0 4 0 67 0. 0 0 0 0 0 - 0. 05 6 6 0. 0 6 1 9 0.7 3 4 8 1 2.972 1. 3 1 6 3 0. 0 4 152 0. 0 0 0 0 0 -0. 05 0 4 0. 0 6 1 1 0. 7 357 1 3. 08 3 1. 3 15 4 0. 0 4 3 0 4 0. 0 0 0 0 0 - 0. 05 3 9 0. 0 6 0 2 0. 7 3 7 1 13.105 1.3 1 05 0. 0 4 32 9 0. 0 0 0 0 0 - 0. 05 1 4 0. 05 9 9 0.7 3 7 4 13.12 8 1.3 1 4 0 0.0 4 355 0. 0 0 0 0 0 - 0. 053 7 0. 05 9 4 0.73 77 13.15 0 1.3 0 1 0 0. 0 4 3 77 0. 0 0 0 0 0 - 0. 0 4 6 8 0. 05 9 1 0.7 3 8 0 13.195 1.3 1 0 9 0. 0 4 4 2 2 0. 0 0 0 0 0 - 0. 05 2 9 0. 05 8 6 0.7 3 85 13.24 1 1.2 9 6 3 0. 0 45 02 0. 0 0 0 0 0 - 0. 0 4 63 0. 05 8 0 0. 7 3 9 1 13.302 1.2 8 6 8 0. 0 45 9 1 0. 0 0 0 0 0 - 0. 0 4 3 2 0. 05 7 4 0.7 3 9 8 13.39 9 1.3 0 3 6 0. 0 4 7 1 1 0. 0 0 0 0 0 - 0. 0 5 4 2 0. 05 6 1 0. 7 4 0 9 1 3.50 0 1.3 0 3 0 0. 0 4 85 7 0. 0 0 0 0 0 - 0. 055 4 0. 05 4 4 0. 7 4 2 3 1 3.75 0 1.2 8 45 0. 05 1 61 0. 0 0 0 0 0 - 0. 0 4 8 4 0.05 1 6 0.7 45 0 1 3. 8 6 1 1.27 1 0 0. 05 2 9 8 0. 0 0 0 0 0 - 0. 0 4 4 0 0. 05 0 8 0. 7 45 9

·FFA TN 1 990- 1 5 4

ISES polar dr iver Version 1. 3

Calculated polar for: AIRFOI L FFA-W1-2 1 1

vortex + doublet far field Entropy conserved

Mach • 0. 15 0 Re .. 3. 0 0 0 e 6 Acrit = 9. 0 0 0

a lpha CL CD ------- -------- ----------1 4 . 9 6 3 0 0 - 0. 7 1 9 0 0 0. 07 8 8 0 - 1 4. 8 8 9 0 0 - 0.7 1 97 0 0. 077 4 8 - 1 4. 8 27 0 0 - 0.777 1 0 0. 07 6 6 6 - 1 4.77 1 0 0 - 0.7 6 0 30 0. 075 8 0 - 1 4.722 0 0 - 0.7 8 2 4 0 0. 07 4 8 2 - 1 4. 673 0 0 - 0. 7 3 4 3 0 0. 07 4 0 0 - 1 4.62 3 0 0 - 0.74 0 0 0 0.072 9 6 -1 4.57 4 0 0 - 0.7 3 95 0 0. 072 07 - 1 4.5 0 0 0 0 - 0.75 65 0 0. 07 0 8 4 - 1 4. 3 3 3 0 0 - 0.752 6 0 0. 0 67 6 8 - 14.2 4 1 0 0 - 0.75 37 0 0. 0 6 6 1 8 - 1 4. 157 0 0 - 0.7 8 1 3 0 0. 0 6 4 9 8 - 1 4. 0 8 3 0 0 - 0. 8 0 9 8 0 0. 0 6 3 8 8 - 1 3. 97 2 0 0 - 0.7 6 3 3 0 0. 0 6 1 9 9 - 1 3. 8 6 1 0 0 - 0.7 64 0 0 0. 0 6 04 0 - 1 3.75 0 0 0 - 0.7 9 3 6 0 0. 05 8 83 - 1 3.5 8 3 0 0 - 0.7 9 9 2 0 0. 05 65 2 - 1 3. 472 0 0 - 0.77 8 0 0 0. 0555 3 - 1 3. 3 6 1 0 0 - 0.7 8 2 1 0 0. 05 4 4 0 - 1 3.25 0 0 0 - 0.7 9 0 4 0 0. 05 3 0 8 - 1 3. 0 0 0 0 0 - 0.7 9 17 0 0. 05 05 3 - 12.75 0 0 0 - 0.7 9 1 4 0 0. 0 4 8 1 9 - 1 2.5 0 0 0 0 - 0.7 93 8 0 0. 0 4 6 1 0 - 1 2.25 0 0 0 - 0.7 9 0 3 0 0. 04 42 0 - 1 2. 0 0 0 0 0 - 0.7 84 6 0 0. 0 42 07 - 1 1. 8 3 3 0 0 - 0.7 87 3 0 0. 0 4 1 0 3 - 1 1. 6 67 0 0 - 0.7 85 0 0 0. 0 3 9 8 6 - 1 1.5 0 0 0 0 - 0.7 845 0 0. 0 3 8 6 0 - 1 1.25 0 0 0 - 0.7 84 8 0 0. 0 3 6 84 - 1 1. 0 0 0 0 0 - 0.77 45 0 0. 0 3524 - 1 0.75 0 0 0 - 0.77 6 2 0 0.0 3 3 3 8 - 1 0.5 0 0 0 0 - 0.77 2 8 0 0. 0 3 1 8 1 - 1 0.25 0 0 0 - 0.7777 0 0. 0 2 9 9 8 -1 0. 00 0 0 0 - 0.77 1 0 0 0. 0 2 8 37

- 9.75 0 0 0 - 0.77 4 4 0 0. 0 2 65 9 - 9.5 0 0 0 0 - 0.7 8 03 0 0. 0 2 4 6 6 - 9.25 0 0 0 - 0.7 8 95 0 0. 0 225 9 -9. 0 0 0 0 0 - 0.77 87 0 0. 0 2 07 3 - 8.75 0 0 0 - 0.7 6 0 8 0 0. 01 85 4 - 8.5 0 0 0 0 - 0.7 35 1 0 0. 0 1 65 3 - 8.25 0 0 0 - 0.7 0 6 0 0 0. 0 1 4 8 1 - 8. 0 0 0 0 0 - 0. 67 3 0 0 0. 0 1 31 8 -7.75 0 0 0 - 0. 6 3 8 6 0 0. 0 1173 -7 . 5 0 0 0 0 - 0. 6 075 0 0. 0 11 0 9 - 7. 1 67 0 0 - 0.5 654 0 0. 0 0 9 9 1 -6. 9 4 4 0 0 - 0.537 4 0 0. 0 0 9 0 1 - 6 . 7 2 2 0 0 - 0.5 0 95 0 0. 0 0 8 0 6 -6 . 5 0 0 0 0 - 0 . 4 8 2 0 0 0. 0 07 4 5 -6 . 0 0 0 0 0 - 0.4 2 0 2 0 0. 0 0 674 - 5 . 50 0 0 0 - 0. 3 5 87 0 0. 0 0 645 - 5. 0 0 0 0 0 - 0. 2 97 0 0 0. 0 0 6 3 0 - 4.5 0 0 0 0 -0. 2 353 0 0. 0 0 62 4 - 4. 0 0 0 0 0 -0. 1 7 35 0 0.0 0 6 1 8 - 3.5 0 0 0 0 - 0. 1 1 1 6 0 0. 0 0 6 1 6 - 3. 0 0 0 0 0 - 0. 05 0 2 0 0.0 0 6 25 -2.5 0 0 0 0 0. 0 1 17 0 0. 0 0 6 3 0 -2 . 0 0 0 0 0 0. 07 35 0 0 . 0 06 24 - 1 . 5 0 0 0 0 0 . 1 35 1 0 0. 0 0 625 - 1 . 0 0 0 0 0 0. 1 9 66 0 0. 0 0 6 34 - 0 . 5 0 0 0 0 0.25 8 0 0 0 . 0 0 644

0 . 0 0 0 0 0 0.3 1 92 0 0 . 0 0 65 3 0 .5 0 0 0. 3 8 1 0 0. 0 0 6 4 6

CDi CM --------- --------

0. 0 0 0 0 0 - 0. 0 17 1 0 0. 0 0 0 0 0 - 0. 0 1 87 0 0. 0 0 0 0 0 0. 0 0 1 8 0 0. 0 0 0 0 0 - 0. 0 0 62 0 0. 0 0 0 0 0 0. 0 0 0 8 0 0. 0 0 0 0 0 - 0. 0 1 8 1 0 0. 0 0 0 0 0 - 0. 0 172 0 0. 0 0 0 0 0 - 0. 0 1 8 9 0 0. 0 0 0 0 0 - 0. 0 1 3 8 0 0. 0 0 0 0 0 - 0. 0 1 92 0 0. 0 0 0 0 0 - 0. 0 2 0 6 0 0. 0 0 0 0 0 - 0. 0 1 1 8 0 0. 0 0 0 0 0 - 0. 0 0 2 6 0 0. 0 0 0 0 0 - 0. 02 2 6 0 0. 0 0 0 0 0 - 0. 0 2 37 0 0. 0 0 0 0 0 - 0. 0 1 42 0 0. 0 0 0 0 0 - 0. 0 1 4 1 0 0. 0 0 0 0 0 - 0. 0 2 1 9 0 0. 0 0 0 0 0 - 0. 0 2 1 3 0 0. 0 0 0 0 0 - 0. 0 1 9 6 0 0. 00 0 0 0 - 0. 0 1 97 0 0. 0 0 0 0 0 - 0. 0 1 9 9 0 0. 0 0 0 0 0 - 0. 0 1 9 4 0 0.0 0 0 0 0 - 0. 0 1 9 9 0 0. 0 0 0 0 0 - 0. 0 2 1 6 0 0. 0 0 0 0 0 - 0. 0 1 9 9 0 0. 0 0 0 0 0 - 0. 0 2 0 4 0 0. 0 0 0 0 0 - 0. 0 1 9 8 0 0. 0 0 0 0 0 - 0. 01 95 0 0. 0 0 0 0 0 - 0. 0 2 17 0 0. 0 0 0 0 0 - 0. 0 2 0 8 0 0. 0 0 0 0 0 - 0. 02 0 7 0 0. 0 0 0 0 0 - 0. 0 1 9 6 0 0. 0 0 0 0 0 - 0. 02 0 8 0 0. 0 0 0 0 0 - 0. 0 1 9 8 0 0. 0 0 0 0 0 - 0. 0 1 9 4 0 0. 0 0 0 0 0 - 0. 0 1 8 9 0 0. 0 0 0 0 0 - 0. 02 11 0 0. 0 0 0 0 0 - 0. 025 9 0 0. 0 0 0 0 0 - 0. 0 3 1 8 0 0. 0 0 0 0 0 - 0. 0 3 67 0 0. 0 0 0 0 0 - 0. 0 4 2 0 0 0. 0 0 0 0 0 - 0. 0 4 67 0 0. 0 0 0 0 0 - 0. 0 4 8 8 0 0. 0 0 0 0 0 - 0. 052 1 0 0. 0 0 0 0 0 - 0. 05 4 3 0 0. 0 0 0 0 0 - 0. 05 6 4 0 0. 0 0 0 0 0 - 0 . 0 57 8 0 0. 00 0 0 0 - 0. 0 5 9 8 0 0. 0 0 0 0 0 -0. 0 6 1 2 0 0. 0 0 0 0 0 - 0. 0 6 2 5 0 0. 0 0 0 0 0 - 0. 0 6 35 0 0. 0 0 0 0 0 - 0. 0 6 47 0 0 . 0 0 0 0 0 - 0. 0 65 8 0 0. 0 0 0 0 0 - 0. 0 6 67 0 0. 0 0 0 0 0 - 0. 0 67 8 0 0. 0 0 00 0 - 0. 0 6 9 0 0 0. 0 0 0 0 0 - 0. 07 0 1 0 0. 0 0 0 0 0 - 0. 07 1 1 0 0. 0 0 0 0 0 - 0. 072 0 0 0. 0 0 0 0 0 - 0. 07 3 1 0

0. 0 0 0 0 0 - 0. 0742

S xtr P xtr ------- -------

0.77 95 0 0. 0 1 4 8 0 0.77 67 0 0. 0 1 4 8 0 0.77 4 3 0 0. 0 1 4 9 0 0 . 772 4 0 0. 0 1 4 9 0 0.77 0 4 0 0. 0 15 0 0 0.7 6 8 9 0 0. 0 15 0 0 0.7 67 6 0 0. 015 0 0 0.765 9 0 0. 0 15 0 0 0.7 6 3 3 0 0. 0 15 1 0 0. 757 1 0 0. 0 15 2 0 0.75 45 0 0. 0 153 0 0.752 0 0 0. 0 154 0 0.7 4 6 9 0 0. 0 155 0 0.7 4 3 1 0 0. 015 6 0 0.7 4 0 0 0 0. 0 15 8 0 0.7 3 6 6 0 0. 0 15 9 0 0.7 3 0 6 0 0. 0 1 6 1 0 0. 727 3 0 0. 0 1 6 4 0 0. 72 4 2 0 0. 01 6 6 0 0. 7 2 0 8 0 0. 0 1 67 0 0.7 1 3 2 0 0. 0 17 3 0 0.7 05 1 0 0. 0 17 8 0 0. 6 9 8 3 0 0. 0 1 84 0 0. 6 9 05 0 0. 01 9 0 0 0. 6 8 2 1 0 0. 0 1 9 6 0 0. 676 9 0 0. 0 2 0 0 0 0. 672 8 0 0. 02 0 4 0 0. 6 6 8 4 0 0. 0 2 0 8 0 0. 6 6 11 0 0. 0 2 1 2 0 0. 6551 0 0. 0 2 2 0 0 0. 6 47 9 0 0. 02270 0. 6 4 2 0 0 0. 0 2 3 4 0 0. 6 354 0 0. 0 2 4 0 0 0. 62 9 2 0 0. 0 2 4 9 0 0.62 07 0 0. 0 255 0 0. 6 15 1 0 0. 02 6 3 0 0. 6 0 8 9 0 0. 0 275 0 0. 6 0 2 2 0 0. 0 3 0 8 0 0.5 95 4 0 0. 0 3 35 0 0.5 8 8 4 0 0. 0 3 8 1 0 0.5 8 15 0 0. 0 4 37 0 0.57 4 2 0 0. 052 1 0 0.5 67 8 0 0. 0 6570 0.5 6 0 4 0 0. 0 8 07 0 0.551 4 0 0. 1 255 0 0.5 45 4 0 0. 17 4 0 0 0.5 4 0 9 0 0.2 3 4 0 0 0.53550 0.2 8 01 0 0.524 6 0 0 . 341 9 0 0. 5 1 3 4 0 0. 37 12 0 0 . 5 017 0 0. 3 9 0 2 0 0.4 92 8 0 0. 4 1 2 0 0 0. 4 831 0 0. 4 2 0 1 0 0. 475 2 0 0. 4 253 0 0 . 4 6 5 8 0 0 . 4 2 9 1 0 0. 4575 0 0. 4 32 4 0 0. 45 0 3 0 0. 4 37 2 0 0. 4 42 6 0 0. 4 4 1 8 0 0. 4 352 0 0. 4 455 0 0. 4 2 87 0 0. 4 47 8 0 0.421 0 0 0.45 1 9 0

0. 4 1 6 0 0. 45 6 8

PO LAR.W2 1 1_30_9;6

FFA TN 1990-15 5 POLAR.W211_30_9; 6

1. 0 0 0 0. 4 42 2 0. 0 0 6 5 5 0.0 0 0 0 0 - 0. 0 7 52 0. 4 0 9 0 0. 4 6 0 6 1. 5 0 0 0. 5 0 31 0. 0 0 6 6 7 0. 0 0 000 - 0. 0 7 61 0. 4 0 3 0 0. 4 6 3 6 2. 0 0 0 0. 5 6 41 0. 0 0 6 7 8 0. 0 0 000 - 0. 0 7 7 0 0. 3 9 8 0 0. 4 6 5 9 2. 5 0 0 0. 6 2 4 7 0. 0 0 6 8 6 0. 0 0 0 0 0 - 0. 0 7 8 0 0. 3 9 0 5 0. 4 7 0 8 3. 0 0 0 0. 6 8 5 7 0. 0 0 6 8 9 0. 0 0 00 0 - 0. 0 7 9 0 0.3 8 5 7 0.4 7 51 3. 5 0 0 0. 7 4 6 3 0. 0 0 6 9 8 0. 0 0 0 00 - 0. 0 8 0 0 0. 37 9 7 0. 4 7 8 9 4. 0 0 0 0. 8 0 5 7 0. 0 0 7 23 0. 0 0 0 0 0 - 0. 0 8 0 7 0. 3 7 2 3 0. 4 81 8 4. 5 0 0 0. 8 6 6 3 0.0 0 732 0. 0 0 0 0 0 - 0. 0 81 5 0.3 6 7 6 0. 4 8 4 5 5.0 0 0 0. 9 2 6 4 0. 0 0 7 3 8 0. 0 0 0 0 0 - 0. 0 8 2 4 0 . 3 611 0.4 8 9 5 5. 5 0 0 0. 9 8 4 7 0. 0 0 7 63 0. 00 0 0 0 - 0. 0 8 32 0. 3 5 2 8 0. 4 9 4 0 6.0 0 0 1.0 4 4 8 0. 0 0 7 71 0. 0 0 0 0 0 - 0. 0 8 40 0. 3 4 4 7 0. 4 9 7 9 6. 5 0 0 1.1 0 2 9 0. 0 0 7 9 8 0. 0 0 0 00 - 0. 0 8 4 6 0. 3 3 4 2 0. 5 01 0 7.0 0 0 1.1 5 9 9 0. 0 0 8 31 0. 0 0 0 0 0 - 0. 0 8 51 0. 32 01 0. 5 0 4 7 7.5 0 0 1.21 7 6 0. 0 0 8 5 7 0. 0 0 0 0 0 - 0. 0 8 5 7 0. 3 0 5 7 0.5 0 9 8 7.7 5 0 1.2 4 51 0. 0 0 8 73 0. 0 0 0 0 0 - 0. 0 8 5 8 0.2 9 63 0.5121 8.0 0 0 1.2 7 23 0. 0 0 8 9 7 0. 0 0 0 00 - 0. 0 8 6 0 0.2 8 73 0.51 4 3 8.2 5 0 1.2 993 0. 0 0 9 21 0. 0 0 0 00 - 0. 0 8 60 0.2 7 6 6 0.51 6 4 8.5 0 0 1. 3 2 5 7 0. 0 0950 0. 0 0 0 00 - 0. 0 8 60 0.2 64 5 0.51 8 4 8.7 5 0 1. 3 5 0 8 0. 0 0 9 8 7 0. 0 0 0 0 0 - 0. 0 8 5 9 0.2 5 0 0 0. 51 9 9 9.0 0 0 1. 3 7 4 7 0. 01 032 0.00 000 - 0. 0 8 5 6 0.2 3 3 7 0.5 21 4 9.2 5 0 1. 39 6 6 0. 01 0 8 5 0. 00 0 00 - 0. 0 8 51 0.21 49 0. 5 2 30 9.3 2 4 1 . 4 03 8 0. 01 0 9 7 0. 0 0 0 0 0 - 0. 0 8 51 0.2 0 9 7 0. 523 8 9.39 8 1. 4 09 8 0. 0111 4 0. 00 000 - 0. 0 84 8 0.2 03 6 0.52 4 6 9.4 7 2 1 . 41 6 2 0. 011 3 0 0. 0 0 0 00 - 0. 0 8 4 7 0.1 9 83 0.52 5 4 9.5 83 1. 4 2 51 0. 011 5 6 0. 00 0 00 -0. 0 8 4 4 0.1 89 7 0. 52 6 5 9.7 5 0 1 . 43 8 3 0 . 01195 0. 0 0 0 00 -0. 0 839 0.1 7 71 0.52 8 2 9.91 7 1. 4 5 0 7 0. 012 3 7 0.00 0 00 - 0. 0 833 0.1 6 4 6 0.52 9 8

1 0.0 8 3 1. 4 6 2 4 0. 012 83 0. 00 0 00 - 0. 0 8 2 8 0.1 5 2 5 0. 5 313 1 0.2 5 0 1. 4 72 5 0. 01 330 0. 0 0 0 0 0 - 0. 0 81 8 0.1 4 0 6 0. 5 3 2 7 1 0.5 0 0 1. 4 8 6 4 0. 01 403 0. 0 000 0 - 0. 0 8 0 4 0.1 2 5 2 0. 5 3 4 8 1 0.6 6 7 1. 4 933 0. 01 4 5 5 0. 000 00 - 0. 0 7 92 0.11 6 6 0. 5 3 61 1 0.7 41 1. 4 9 43 0. 01 4 7 6 0. 0 00 00 - 0. 0 7 8 2 0.112 9 0. 5 3 6 6 1 0.81 5 1.4 920 0. 01 501 0. 00 00 0 - 0. 0 7 6 4 0.11 0 4 0. 5371 1 0.9 8 9 1.490 8 0. 01 530 0. 00 000 - 0. 0 7 53 0.1 0 8 2 0.53 7 5 11. 0 0 0 1. 4 91 6 0. 01 5 71 0.00000 -0. 0 7 4 6 0.1 0 40 0. 5 3 80 11.2 5 0 1. 4 8 7 5 0. 01 691 0. 00 00 0 - 0. 0 71 5 0. 0 9 6 6 0. 5 3 92 11. 5 0 0 1. 4 8 4 7 0. 01 8 3 6 0. 00 00 0 - 0. 0 6 9 5 0. 0 8 99 0. 5 4 03 11. 6 6 7 1. 4 8. 0 4 0. 01 9 6 0 0. 00 000 - 0. 0 6 8 9 0. 0 8 6 4 0. 5 41 7 11. 8 3 3 1. 4 71 4 0. 0 21 0 6 0. 0 0 0 0 0 - 0. 0 6 7 2 0. 0 8 31 0. 5 4 3 5 1 2 . 0 0 0 1. 4 6 52 0. 0 2 2 5 2 0. 0 0 0 0 0 - 0. 0 6 61 0. 0 8 03 0. 5 4 4 8 12.2 5 0 1. 4 5 43 0. 0 2 5 0 2 0. 0 0 000 - 0. 0 6 5 0 0. 0 7 6 6 0. 5 4 6 6 1 2. 5 0 0 1. 4 3 4 4 0. 0 2 8 01 0. 0 0 0 00 - 0. 0 6 0 6 0. 0 7 3 2 0.5 4 81 1 2. 7 5 0 1. 4 2 0 4 0. 0 31 4 8 0. 0 00 0 0 ·- 0. 0 6 3 5 0. 0 7 0 9 0. 5 4 93 1 3. 0 0 0 1.4 0 8 8 0. 0 3 4 63 0. 0 0 00 0 - 0. 0 6 2 4 0. 0 6 8 0 0. 5 5 0 7

FFA TN 1990-1 5 6 POLAR.W2 11_3 0_TU1; 1

ISES polar driver Version 1.3

Calculated polar for: AIRFOIL FFA-W1-21 1

Vortex + doublet far field Ent ropy conserved

Mach • 0. 1 5 0 Re = 3. 0 0 0 e 6 Acrit = 9. 0 0 0

alpha CL CD CDi CM S xtr P xtr ------- -------- --------- --------- -------- ------- -------

0. 0 0 0 0.2 9 81 0. 01 1 07 0. 00 0 0 0 - 0. 0 6 8 8 0. 01 00 0. 1 0 0 0 0. 5 0 0 0. 35 67 0. 0 11 17 0. 0 0 0 0 0 - 0. 0 6 9 6 0. 0 1 0 0 0. 1 0 00 1. 0 0 0 0.41 6 8 0. 0112 9 0. 0 0 0 0 0 - 0. 07 07 0. 01 0 0 0. 10 0 0 1. 5 0 0 0. 47 64 0. 01142 0. 0 0 0 0 0 -o. on 5 0. 01 0 0 0.1 0 0 0 2. 0 0 0 0. 5342 0. 0 11 5 8 0. 0 0 0 0 0 - 0. 0724 0. 01 0 0 0. 1 0 0 0 2. 5 0 0 0. 5 9 2 6 0. 01 177 0. 0 0 0 00 - 0. 0732 0.0 1 0 0 0. 1 0 0 0 3. 0 0 0 0. 6 517 0. 011 97 0. 0 0 0 0 0 - 0. 073 8 0. 01 0 0 0. 1 0 00 3. 5 0 0 0. 7 0 93 0. 0 1 2 2 0 0.0 0 0 0 0 - 0. 074 5 0. 0 1 0 0 0. 1 0 0 0 4. 0 0 0 0. 7 6 62 0. 0 1 24 6 0. 0 0 0 0 0 - 0. 07 51 0. 0 1 0 0 0. 1 0 0 0 4. 5 0 0 0. 8 2 2 6 0. 0 1 274 0. 0 0 0 0 0 - 0. 07 5 6 0. 0 1 0 0 0. 1 0 0 0 5. 0 0 0 0.87 8 0 0. 0 13 05 0. 0 0 0 0 0 - 0. 07 6 0 0. 0 1 0 0 0. 1 0 0 0 5. 5 0 0 0. 93 2 8 0. 0 134 0 0. 0 0 0 0 0 - 0. 07 63 0. 0 1 0 0 0. 10 0 0 6. 0 0 0 0. 9 8 62 0. 0 137 8 0. 0 00 0 0 - 0. 07 6 5 0. 0 1 0 0 0. 1 0 0 0 6. 5 0 0 1. 03 8 8 0. 0142 1 0.0 0 0 0 0 - 0. 07 6 5 0. 0 1 0 0 0. 1 0 00 7. 0 0 0 1. 0 893 0. 0 14 67 0. 0 0 0 0 0 - 0. 076 4 0. 01 0 0 0. 1 0 0 0 7. 5 0 0 1. 13 8 5 0. 01 52 0 0. 0 0 0 0 0 - 0. 07 6 0 0. 0 1 0 0 0. 1 0 0 0 7. 7 5 0 1. 1 6 1 6 0. 0 1 54 9 0. 0 0 0 0 0 -0.0757 0. 010 0 0. 1 0 0 0 8. 0 0 0 1.1 8 24 0. 015 8 0 0. 0 0 0 0 0 - 0. 07 5 2 0. 01 0 0 0. 1 0 00 8.2 5 0 1. 2 0 6 1 0. 01 613 0. 0 0 0 0 0 - 0. 074 8 0. 0 1 0 0 0.1 0 0 0 8.5 0 0 1. 2 257 0. 0 164 9 0. 0 0 0 0 0 - 0. 074 1 0. 0 1 0 0 0. 1 0 0 0 8.7 5 0 1. 236 9 0. 0 1 6 93 0. 0 0 0 0 0 - 0. 07 1 9 0. 0 1 0 0 0. 1 0 0 0 9. 0 0 0 1. 24 5 8 0. 0 17 53 0. 0 0 0 0 0 - 0. 07 0 0 0. 01 0 0 0. 1 0 0 0 9.2 50 1. 2 54 0 0. 0 1 831 0.0 0 0 0 0 - 0. 0 6 8 5 0. 0 1 0 0 0.1 0 0 0 9. 5 0 0 1.2 613 0. 0 1 9 2 9 0.0 0 0 0 0 - 0. 0 677 0. 0 1 0 0 0. 1 0 0 0 9. 7 5 0 1. 2 632 0. 02 0 5 0 0. 0 0 00 0 - 0. 0 6 5 9 0. 0 1 0 0 0. 1 0 0 0

1 0. 0 0 0 1. 2 6 53 0. 0 2 1 9 8 0. 0 0 0 0 0 - 0. 0 647 0. 0 1 0 0 0. 1 0 0 0 1 0.2 5 0 1. 27 2 2 0. 0 23 6 5 0. 0 0 0 0 0 - 0. 0 676 0. 0 1 0 0 0. 1 0 0 0 1 0. 5 0 0 1. 2 6 0 8 0. 0 2 57 4 0. 0 00 0 0 - 0. 0 62 2 0. 01 0 0 0.1 0 0 0 1 0. 6 67 1. 2 5 1 6 0. 0 2727 0. 0 0 0 0 0 - 0. 05 9 6 0.0 1 0 0 0. 1 0 0 0 1 0. 833 1.2 577 0. 0 2 8 9 0 0. 0 0 0 0 0 - 0.0 647 0.01 0 0 0. 1 0 0 0 1 1. 0 0 0 1.2443 0. 03 05 9 0. 0 0 0 0 0 - 0. 0 5 8 5 0. 01 0 0 0.1 0 00 11. 2 5 0 1. 2431 0. 0334 1 0. 0 0 0 0 0 - 0. 0 633 0. 0 1 0 0 0. 1 0 0 0 11. 5 0 0 1.233 6 0. 03 6 2 5 0. 0 0 0 0 0 - 0. 0 60 9 0. 01 0 0 0. 1 0 0 0 11. 6 67 1.23 04 0. 03 8 2 8 0. 0 0 0 0 0 - 0.0 61 6 0. 01 0 0 0. 1 0 0 0 11. 77 8 1. 2 2 03 0. 03 9 8 1 0. 0 0 0 0 0 - 0. 0 607 0. 0 1 0 0 0. 1 0 00 11. 8 8 9 1. 2 21 5 0. 0412 8 0. 0 0 0 0 0 - 0.0 6 3 6 0. 0 1 0 0 0.1 0 0 0 12. 0 0 0 1.21 1 5 0. 042 53 0. 0 0 0 0 0 - 0. 0 5 93 0. 0 1 0 0 0.1 0 0 0 12. 2 5 0 1. 204 8 0. 04 5 83 0. 0 0 0 0 0 - 0. 0 6 0 2 0. 0 1 0 0 0.1 00 0

FFA TN 1990-1 5 7

ISES polar driver Version 1. 3

Calculated polar for: A IRFOIL FFA-W1-2 4 2

Vortex + doublet Ent ropy conserved

Mach •

alpha -------

0.5 0 0 1.0 0 0 1.5 0 0 2.0 0 0 2.5 0 0 3.0 0 0 3.5 0 0 4.0 00 4.5 0 0 5.0 0 0 5.50 0 6.0 0 0 6.5 00 7.00 0 7.50 0 7.7 5 0 8.000 8.2 5 0 8.5 00 8. 7 5 0 9.00 0 9.2 5 0 9. 5 0 0 9. 7 5 0

10.0 0 0 1 0. 2 5 0 10. 5 0 0 10.7 5 0 11. 0 0 0 11. 2 5 0 11. 5 0 0 11. 7 5 0 12. 0 0 0 12. 2 5 0 12. 50 0 12.7 5 0 13.00 0 13.25 0 13. 5 0 0 13.75 0 1 4. 00 0 1 4. 25 0 1 4. 50 0 14.6l.1 1 4.722 1 4. 8 33 1 4. 94 4 15.083 15.250

0.15 0

C L --------

0. 3 4 7 8 0. 4 0 9 8 0. 4 7 2 5 0. 5 3 5 7 0. 5 9 7 7 0. 6 5 9 5 0. 7 2 0 3 0. 7 8 2 3 0. 8 4 3 6 0. 90 3 4 0. 9 6 40 1. 0 2 2 7 1. 0 81 9 1.1 40 9 1.1 9 80 1.2 2 62 1.2 5 3 6 1.2 81 5 1. 3 0 8 2 1. 3 3 4 8 1. 3 61 6 1.3 8 7 4 1. 41 4 2 1 . 4 3 91 1. 4 63 5 1. 4 8 8 0 1. 51 00 1. 5 3 2 9 1.5 5 3 4 1. 5 7 21 1. 5 8 7 6 1. 5 9 7 3 1. 6 0 4 2 1. 6 0 70 1. 6 0 5 5 1. 6 0 8 7 1. 6 0 3 4 1. 5 9 3 2 1. 5 8 8 8 1.57 3 0 1. 5 62 3 1.5 3 6 9 1. 5 1 6 9 1.5 0 5 0 1. 4 9 6 8 1. 4 9 4 7 1. 4 82 3 1. 47 5 0 1.4643

far field

Re •

CD ---------

0. 0 0 6 9 7 0. 0 0 71 4 0. 0 0 72 2 0. 0 0 7 2 6 0. 00 7 4 2 0. 0 0 7 5 4 0. 0 0 7 7 7 0. 0 0 7 8 8 0. 0 0 7 9 9 0. 0 0 82 8 0. 0 0 8 4 4 0. 00 8 7 6 0. 00 8 9 8 0. 00 9 2 2 0.00 9 5 8 0.00 9 7 6 0. 01 000 0.01 01 8 0.01 0 50 0.01 0 71 0. 010 92 0. 01121 0. 011 3 9 0. 011 6 9 0. 01201 0. 012 2 8 0. 012 6 8 0.01 300 0. 0 1 3 4 2 0. 01 3 8 8 0. 01 4 3 2 0. 01 4 8 7 0 . 01 5 3 6 0. 01 60 6 0. 01 7 0 5 0. 01 8 0 6 0 . 01 9 51 0. 0 21 4 9 0. 0 2 3 5 5 0. 0 2 61 7 0. 0 2 9 2 6 0. 0 32 8 6 0. 0 3 6 8 3 0.0 3 8 3 3 0. 0 4 0 0 4 0. 0 41 7 5 0. 0 4 3 4 3 0.0 4 5 8 8 0. 0 4 8 7 3

3. 0 00 e 6 Acrit • 9.0 0 0

CDi CM S xtr P xtr -------- - -------- ------ - -------

0. 0 0 000 - 0. 0 7 7 4 0.3 9 0 8 0.4 4 7 0 0. 0 0 00 0 - 0. 0 7 8 5 0. 3 7 9 9 0. 4 4 9 9 0. 00 0 00 - 0. 0 7 9 8 0. 3 7 0 8 0. 4 5 3 9 0. 0 0 0 00 - 0. 0 81 2 0. 3 6 0 4 0. 4 5 91 0. 0 00 00 - 0. 0 8 2 4 0. 3 5 0 2 0. 4 6 3 8 0. 00 000 -0. 0 8 3 4 0. 3 4 0 7 0. 4 6 7 2 0. 0 0 000 - 0. 0 8 4 3 0. 3311 0. 4 6 9 6 0. 00000 - 0. 0 8 5 5 0. 3 2 01 0. 4 7 4 4 0. 00 0 00 - 0.0 8 6 7 0.3117 0. 4 7 9 7 0. 0 0 000 - 0. 0 8 7 5 0. 3001 0. 4 8 3 9 0. 0 0000 - 0. 0 8 8 2 0.2 91 6 0. 4 8 6 8 0. 00000 - 0. 0 8 8 7 0.2 8 0 9 0. 4 8 9 3 0. 00 000 - 0. 0 8 9 5 0.2 6 9 6 0. 4 93 9 0. 0 0000 - 0. 0 9 01 0.2 5 8 7 0. 4 9 8 5 0. 00000 - 0. 0 9 0 5 0.2 4 6 7 0. 5 0 2 7 0. 00000 - 0. 0 90 7 0. 2 3 9 6 0. 5 0 4 7 0. 00000 - 0. 0 9 0 7 0.2 3 3 5 0. 5 0 6 5 0.00000 -0.0 90 7 0.2 2 6 6 0. 5 0 7 9 0. 00000 -0.0 90 6 0.21 7 9 0.5 0 9 4 0.00000 - 0. 0 90 5 0.212 8 0. 51 0 8 0.00000 - 0.0 90 5 0.20 6 2 0. 51 2 9 0.00000 - 0.0 903 0.1 9 9 6 0. 51 5 4 0.00000 - 0. 0 902 0.1 9 3 9 0.51 7 8 0. 00000 - 0. 0 900 0.1 8 7 2 0.52 0 0 0. 00000 - 0. 0 8 9 6 0.1 81 0 0. 5222 0.00000 - 0. 0 8 92 0.1 7 4 7 0. 52 4 4 0. 0 0000 - 0. 0 8 8 5 0.1 6 7 5 0. 5 2 6 3 0. 0 0 000 - 0. 0 8 7 8 0.1 613 0. 5 2 8 2 0. 00 0 00 - 0. 0 8 6 9 0.1 5 4 4 0. 52 9 6 0. 0 00 00 - 0. 0 8 5 8 0.1 4 8 0 0. 5 31 0 0. 0 0 0 00 - 0. 0 8 4 0 0.1 41 6 0. 5 3 2 4 0. 00 0 00 - 0. 0 81 4 0.1 3 4 9 0. 5 3 4 6 0.0 00 00 - 0. 0 7 8 6 0.1 2 9 6 0. 5 3 7 4 0. 0 000 0 - 0. 0 7 5 3 0.1 2 4 2 0.5 3 9 5 0. 0 0 0 0 0 - 0. 0 721 0.11 91 0. 5 41 4 0. 00 0 00 - 0. 0 702 0.11 40 0. 5 4 32 0. 0 0 0 00 - 0. 0 6 81 0.1 0 9 4 0.5 4 4 8 0. 00 0 0 0 - 0. 0 6 5 6 0.1 0 5 4 0. 5 4 62 0. 0 0 0 0 0 - 0. 0 67 0 0.1 01 9 0. 5 4 7 2 0. 0 0 0 00 - 0. 0 62 3 0. 0 9 8 4 0. 5 4 81 0.0 0 0 0 0 - 0. 0 6 6 0 0. 0 9 5 6 0. 5 4 8 8 0. 0 0 0 0 0 - 0. 0 620 0. 0 9 31 0. 5 4 9 7 0.00 0 00 - 0. 0 62 0 0. 0 9 0 7 0. 5 51 2 0. 0 0 00 0 - 0. 0 5 9 6 0. 0 8 9 9 0. 5 51 8 0. 0 00 0 0 - 0. 0 5 92 0. 0 8 8 9 0. 5 5 2 4 0. 0 00 0 0 -0. 0 62 0 0. 0 8 7 8 0. 5 5 31 0. 0 0 0 0 0 - 0. 0 5 8 6 0. 0 8 6 6 0. 5 5 3 7 0. 0 0 0 0 0 - 0. 0 6 0 8 0. 0 8 5 3 0. 5 5 4 4 0. 0 00 0 0 - 0. 0 6 3 3 0. 0 8 4 0 0.5 5 5 6

POLAR.W 2 4 2_30_ 9; 1

FFA TN 1990-15 8 POLAR.W 2 4 2_ 3 0_TU1; 1

ISES polar driver Version 1. 3

Calculated polar for: A IRFOIL FFA-W1-2 4 2

Vortex + doublet far field Entropy conserved

Mach • 0.1 5 0 Re = 3. 0 0 0 e 6 Acrit = 9. 0 0 0

alpha C L CD CDi CM S xtr P xtr ------- -------- --------- --------- -------- ------- -------

0. 5 0 0 0.2 9 62 0. 012 6 7 0. 0 0 0 0 0 - 0. 0 6 4 0 0. 01 0 0 0.1 0 0 0 1. 0 0 0 0. 35 9 8 0. 01 2 6 6 0. 0 0 0 0 0 - 0. 0 6 6 0 0. 01 0 0 0.1 0 0 0 1. 5 0 0 0.4 2 2 6 0.012 6 9 0. 0 0 0 0 0 - 0. 0 67 8 0. 01 0 0 0.1 0 0 0 2.0 0 0 0.4 8 3 9 0. 012 7 6 0. 0 0 0 0 0 - 0. 0 6 9 7 0.01 0 0 0.1 0 0 0 2.5 0 0 0. 5 4 6 4 0. 012 8 6 0. 0 0 0 0 0 -0. 0 711 0. 01 0 0 0.1 0 0 0 3. 0 0 0 0. 6 0 6 0 0. 013 0 0 0. 0 0 00 0 - 0. 07 2 7 0. 01 0 0 0.1 0 0 0 3. 5 0 0 0. 6 661 0. 01 317 0. 0 0 0 0 0 - 0. 0 7 3 9 0. 01 0 0 0.1 0 0 0 4. 0 0 0 0. 7 2 6 8 0. 013 3 7 0. 0 0 0 0 0 - 0. 0 7 4 8 0.01 0 0 0.1 0 0 0 4. 5 0 0 0. 7 8 5 6 0. 01 3 60 0. 0 0 0 0 0 - 0. 0 7 5 7 0. 01 0 0 0.1 0 0 0 5. 0 0 0 0. 8 4 3 3 0. 01 3 8 6 0. 0 0 0 0 0 - 0.0 7 6 5 0. 01 0 0 0.1 0 0 0 5. 5 0 0 0. 8 9 9 7 0. 0141 6 0. 0 0 0 0 0 - 0. 0 7 7 2 0. 01 0 0 0.1 0 0 0 6. 0 0 0 0. 9 5 5 8 0. 01 4 4 9 0. 0 0 0 0 0 - 0. 0 7 7 5 0. 01 0 0 0.1 0 0 0 6. 5 0 0 1. 0 0 9 8 0. 014 8 6 0. 00 0 0 0 - 0. 0 7 7 8 0. 01 0 0 0.1 0 0 0 7. 0 0 0 1. 0 6 2 9 0. 01 5 2 8 0. 0 0 0 0 0 - 0. 0 7 7 8 0. 01 0 0 0.1 0 0 0 7. 5 0 0 1.11 3 4 0. 01 5 7 4 0. 0 0 0 0 0 - 0. 0 7 7 6 0.01 0 0 0.1 0 0 0 7.7 5 0 1.1 3 6 8 0. 01 5 9 9 0. 0 0 0 0 0 - 0. 0 7 7 3 0. 01 0 0 0.1 0 0 0 8. 0 0 0 1.1 6 0 5 0. 01 6 2 5 0. 0 0 0 0 0 - 0. 0 7 71 0. 01 0 0 0.1 0 0 0 8.25 0 1.1 8 3 7 0. 01 6 5 4 0. 0 0 0 0 0 - 0. 0 7 6 6 0. 01 0 0 0.1 0 0 0 8. 5 0 0 1.2 0 6 9 0. 01 6 8 4 0. 0 0 0 0 0 - 0. 0 7 5 9 0. 01 0 0 0.1 0 0 0 8. 7 5 0 1. 2 2 5 3 0. 0171 8 0. 0 0 0 0 0 - 0. 0 7 4 8 0. 01 0 0 0.1 0 0 0 9. 0 0 0 l. 2 4 2 0 0. 01 7 5 4 0. 0 0 0 0 0 - 0. 0 7 32 0. 01 0 0 0.1 0 0 0 9.2 5 0 1. 2 51 9 0. 01 7 9 5 0. 000 0 0 - 0. 0 7 0 7 0. 01 0 0 0.1 0 0 0 9. 5 0 0 1. 2 61 7 0. 01 845 0. 0 0 0 0 0 - 0. 0 6 8 6 0. 010 0 0.1 0 0 0 9.7 5 0 1.27 0 9 0. 01 9 0 8 0. 0 0 0 0 0 - 0. 0 6 6 9 0. 01 0 0 0.1 0 0 0

1 0.0 0 0 1. 2 7 6 7 0. 01 9 87 0. 0 0 0 00 - 0. 0 64 7 0. 01 0 0 0.1 0 0 0 1 0. 2 50 1. 2 8 3 5 0. 02 0 8 7 0. 0 0 0 0 0 - 0. 0 6 3 5 0. 01 0 0 0.1 0 0 0 1 0. 5 0 0 1.2 8 4 2 0. 0 2 213 0. 0 0 0 0 0 - 0. 0 61 9 0. 01 0 0 0.1 0 00 1 0.75 0 1. 2 8 8 4 0. 0 2 3 6 3 0. 0 0 00 0 - 0.0 622 0. 01 0 0 0.1 0 0 0 11. 0 0 0 1.2 8 0 9 0. 0 2 5 51 0. 0 0 0 0 0 - 0. 0 5 9 3 0. 01 0 0 0.1 0 0 0 11.2 5 0 1. 2 7 8 4 0. 0 2 7 6 0 0. 0 0 0 0 0 - 0. 0 5 8 6 0. 0 1 0 0 0.1 0 0 0 11.5 0 0 1. 2731 0. 0 3 011 0. 0 0 0 0 0 - 0. 0 5 8 6 0. 01 0 0 0.1 0 0 0 11. 7 5 0 1.2 6 2 6 0. 0 329 0 0. 0 0 0 0 0 - 0. 0 5 8 0 0. 01 0 0 0.1 0 0 0 12.0 0 0 1.2 55 5 0. 0 3 5 8 8 0.0 0 0 0 0 - 0. 0 5 8 6 0. 01 0 0 0.1 0 0 0 1 2. 2 5 0 1.2 5 62 0. 0 3 9 0 8 0. 0 0 0 0 0 - 0. 0 6 3 9 0. 01 0 0 0.10 0 0 12.417 1.232 9 0. 0 4132 0. 0 0 0 0 0 - 0. 0 5 6 5 0. 01 0 0 0.1 0 0 0 12. 5 8 3 1. 2 3 0 0 0. 0 4 3 5 6 0. 0 0 0 0 0 - 0. 0 5 8 3 0. 01 0 0 0.1 0 0 0 12. 7 5 0 1.22 2 3 0. 0 4 6 02 0. 0 0 0 00 - 0. 0 5 8 3 0. 01 0 0 0.1 0 0 0 1 2. 917 1.21 0 9 0. 04 8 4 8 0. 0 0 0 0 0 - 0. 0 5 5 8 0. 01 0 0 0.1 0 0 0 1 3. 0 8 3 1. 2 0 8 8 0. 0 5 0 8 5 0. 0 0 0 0 0 - 0. 0 5 9 8 0. 01 0 0 0.1 0 0 0 1 3. 2 5 0 1. 2 01 3 0. 0 5 31 9 0. 0 0 0 0 0 - 0. 0 5 92 0. 01 0 0 0.1 0 0 0

FFA TN 1990-15 9

ISES polar driver Version 1. 3

Cal culated polar for: A IRFOIL FFA-W1-2 71

Vortex + doublet Entropy conserved

Mach •

alpha -------

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1.5 0 0 2.0 0 0 2.5 0 0 3.0 0 0 3.5 0 0 4.0 0 0 4.5 0 0 5.0 0 0 5.5 0 0 6.0 0 0 6.5 0 0 7.0 0 0 7.5 0 0 7.7 5 0 8.0 0 0 8.2 5 0 8. 5 0 0 8.7 5 0 9. 0 0 0 9. 2 5 0 9. 5 0 0 9. 7 5 0

1 0. 0 0 0 1 0.2 5 0 1 0. 5 0 0 1 0. 7 5 0 1 1. 0 0 0 11.2 5 0 1 1. 5 0 0 11.7 5 0 1 2. 0 0 0 1 2.25 0 12. 50 0 1 2.75 0 1 3. 00 0 1 3.250 1 3. 50 0 1 3. 75 0 14.00 0 1 4 . 25 0 1 4. 41 7 1 4. 45 0 1 4 . 464 1 4. 47 9 1 4. 48 9 1 4. 494

0. 1 5 0

C L --------

0.2 5 6 7 0.3244 0.3 9 0 8 0.4 5 5 6 0. 5 2 0 3 0. 5 8 31 0. 64 5 8 0.7 0 9 3 0.7 74 2 0. 8 3 6 8 0. 8 9 9 9 0. 9 6 0 2 1 . 0 2 14 1. 0 8 1 3 1.14 2 7 1.2 011 1.2 3 0 6 1.2 5 9 7 1.2 8 7 6 1.3 14 3 1. 34 2 7 1. 3 7 0 0 1. 3 9 51 1. 4 2 31 1. 44 9 5 1.4 7 3 9 1. 4 9 84 1. 5224 1. 5431 1. 5 6 0 2 1.57 9 7 1. 5 912 1. 5 9 3 3 1. 5 9 8 9 1. 6 0 3 3 1. 6 0 3 6 1. 5 9 91 1. 6 0 0 2 1. 5 9 6 5 1. 5 8 6 0 1. 5 7 3 5 1. 5 6 9 9 1. 5 5 3 0 1.54 3 5 1. 5 5 8 2 1.552 9 1. 54 84 1. 5 51 1 1 . 54 9 7

far field

Re =

CD ---------

0. 0 0 7 91 0. 0 0 7 82 0. 0 0 7 7 6 0. 0 0 7 84 0. 0 0 7 8 9 0. 0 0 81 2 0. 0 0 8 2 8 0. 0 0 84 8 0. 0 0 84 6 0. 0 0 8 6 8 0. 0 0 8 7 8 0. 0 0 91 0 0. 0 0 9 31 0. 0 0 9 6 2 0. 0 0 9 7 9 0. 01 01 6 0. 0 1 02 8 0. 01 044 0. 01 0 7 0 0. 01 0 9 5 0. 011 1 3 0. 011 3 9 0. 011 6 9 0. 011 84 0. 01 2 0 6 0. 012 3 6 0. 01 2 6 7 0. 01 2 92 0. 01 3 3 0 0 . 01 3 7 7 0. 014 0 9 0. 014 5 7 0. 01 51 5 0. 01 5 7 0 0. 01 64 0 0. 01 7 3 5 0. 01 8 5 9 0. 01 9 8 0 0. 0 214 3 0. 0 2 34 5 0. 0 2 5 9 5 0. 0 2 81 8 0. 0 3 0 8 5 0. 0 3 2 94 0. 0 3 2 84 0. 0 3 3 0 0 0. 0 3 3 1 6 0. 0 3 3 2 7 0. 0 3 3 34

3. 0 0 0 e 6 Acrit .. 9. 0 0 0

CDi CM S xtr P xtr --------- -------- ------- -------

0. 0 0 0 0 0 - 0. 0 7 8 8 0. 3 8 74 0.41 8 5 0. 0 0 0 0 0 - 0. 0 8 1 5 0. 3 7 7 2 0.4 2 2 5 0. 0 0 0 0 0 - 0. 0 8 3 7 0.3 6 7 5 0.4 2 7 2 0. 0 0 0 0 0 - 0. 0 8 5 6 0. 3 5 74 0.4 31 6 0. 0 0 0 0 0 - 0. 0 8 7 2 0. 34 9 5 0.4 3 5 5 0. 0 0 0 0 0 - 0. 0 8 8 5 0. 3 3 84 0.4 3 84 0. 0 0 0 0 0 - 0. 0 8 94 0. 3 312 0.44 0 6 0. 0 0 0 0 0 - 0. 0 91 0 0. 3 2 04 0.444 0 0. 0 0 0 0 0 - 0. 0 92 8 0.3132 0.44 8 9 0.0 0 0 0 0 - 0. 0 94 1 0. 3 0 2 5 0.4 5 3 6 0. 0 0 0 0 0 - 0. 0 9 54 0.2 9 5 3 0.4 5 7 9 0. 0 0 0 0 0 - 0. 0 9 62 0.2 84 8 0.4 614 0. 0 0 00 0 - 0. 0 9 7 0 0.2 7 7 5 0.4 6 3 7 0. 0 0 0 0 0 - 0. 0 9 7 9 0.2 6 6 8 0.4 6 7 3 0. 0 0 0 0 0 - 0. 0 9 8 9 0. 2 5 7 8 0.4 7 24 0. 0 0 0 0 0 - 0. 0 9 9 6 0.24 6 8 0.4 7 7 9 0. 0 0 0 0 0 - 0. 0 9 9 8 0.241 9 0.4 8 0 0 0. 0 0 0 0 0 - 0.1 0 0 0 0.2 3 6 9 0.4 8 2 2 0. 0 0 0 0 0 - 0.1 0 01 0.2 3 0 2 0.4 84 1 0. 0 0 0 0 0 - 0. 0 9 9 9 0.2 2 5 8 0.4 8 54 0. 0 0 0 0 0 - 0.1 0 0 0 0.21 9 6 0.4 8 6 8 0. 0 0 0 0 0 - 0. 0 9 9 9 0.214 1 0.4 8 8 2 0. 0 0 0 0 0 - 0. 0 9 9 6 0.2 0 91 0. 4 8 9 8 0. 0 0 0 0 0 - 0. 0 9 9 6 0.2 04 6 0.4 924 0. 0 0 0 0 0 - 0. 0 9 9 5 0.1 9 9 0 0.4 9 5 0 0. 0 0 0 0 0 - 0. 0 9 92 0.1 9 3 3 0.4 9 74 0. 0 0 0 0 0 - 0. 0 9 8 7 0.1 8 8 3 0.4 9 9 9 0. 0 0 0 0 0 - 0. 0 9 81 0.1 8 2 8 0. 5 0 2 2 0. 0 0 0 0 0 - 0. 0 9 71 0.1 7 6 9 0.5044 0. 0 0 0 0 0 - 0. 0 9 5 5 0.1 715 0.5 0 64 0. 0 0 0 0 0 - 0. 0 94 3 0.1 6 63 0. 5 0 8 3 0. 0 0 0 0 0 - 0. 0 91 7 0.1 61 0 0.5 0 9 5 0. 0 0 0 0 0 - 0. 0 8 7 6 0.15 64 0.51 0 5 0. 0 0 0 0 0 - 0. 0 84 6 0. 1 521 0. 511 6 0 . 0 0 0 0 0 - 0. 0 81 5 0. 147 3 0.51 3 7 0. 0 0 0 0 0 - 0. 0 7 8 5 0.142 8 0.51 5 8 0. 0 0 0 0 0 - 0. 0 7 6 0 0.1 3 8 8 0. 51 7 8 0. 0 0 0 0 0 - 0. 0 7 34 0.1 34 8 0. 51 9 8 0. 0 0 0 0 0 - o. on1 0.1 3 0 7 0. 521 7 0. 0 0 0 0 0 - 0. 0 6 9 6 0 . 1 2 7 2 0.5 2 3 2 0. 0 0 0 0 0 - 0. 0 6 7 8 0.1 2 3 9 0.5247 0. 0 0 0 0 0 - 0. 0 6 7 8 0.12 0 8 0. 5 2 62 0. 0 0 0 0 0 - 0. 0 64 3 0.11 7 5 0. 5 2 7 3 0. 0 0 0 0 0 - 0. 0 6 3 6 0. 1 1 5 5 0. 5 2 7 8 0. 0 0 0 0 0 - 0. 0 7 0 5 0. 11 7 0 0. 5 2 8 0 0. 0 0 0 0 0 - 0. 0 6 6 8 0. 11 6 9 0. 5 2 8 0 0. 0 0 0 0 0 - 0. 0 64 0 0.1 1 65 0.5 2 8 1 0. 0 0 0 0 0 - 0. 0 6 61 0.11 6 5 0. 5 2 8 1 0. 0 0 0 0 0 - 0. 0 6 5 5 0.11 64 0. 5 2 8 2

POLAR.W2 7 1_3 0_ 9; 1

FFA TN 1990- 1 5 1 0 POLAR.W2 71_3 0_TU1;1

ISES polar driver Version 1. 3

Calculated polar for: AIRFOIL FFA-W1- 2 71

Vortex + doublet far field Entropy conserved

Mach - 0. 1 5 0 Re = 3. 0 0 0 e 6 Acrit = 9. 0 0 0

a lpha CL CD CDi CM S xtr P xtr ------- -------- --------- --------- -------- ------- -------

0. 0 0 0 0. 1 546 0. 01645 0. 0 0 0 0 0 - 0. 046 5 0. 01 0 0 0.1 00 0 0. 5 00 0. 2 2 8 0 0. 01 5 8 0 0. 0 0 0 0 0 - 0. 05 2 5 0. 01 0 0 0. 1 0 0 0 1. 0 0 0 0. 3 0 0 3 0. 01 5 31 0. 0 0 0 0 0 - 0. 0 5 7 7 0. 01 0 0 0.1 0 0 0 1.5 0 0 0.371 8 0. 014 92 0.0 0 0 0 0 - 0.0625 0. 01 0 0 0.1 0 0 0 2. 0 0 0 0.442 2 0. 01462 0. 0 0 0 0 0 - 0. 066 9 0. 0 1 0 0 0.1 0 0 0 2. 5 0 0 0. 5114 0. 0 1441 0. 0 0 0 0 0 - 0. 0 7 0 7 0. 0 1 0 0 0.1 0 0 0 3. 0 0 0 0. 5 7 8 7 0. 01431 0. 0 0 0 0 0 - 0. 0 741 0. 0 1 0 0 0.1 0 0 0 3.5 0 0 0.64 3 2 0. 014 3 7 0. 0 00 0 0 - 0. 0 76 5 0. 01 0 0 0.1 0 0 0 4. 0 0 0 0. 7 0 5 5 0. 01451 0. 0 0 0 0 0 - 0. 0 7 8 3 0. 01 0 0 0. 1 0 00 4. 5 0 0 0. 7664 0. 01471 0.0 0 0 0 0 - 0. 0 7 9 9 0. 01 0 0 0.1 0 0 0 5. 0 0 0 0. 8 26 5 0 . 014 94 0. 0 0 0 0 0 - 0. 0 812 0. 01 00 0.1 0 00 5. 5 0 0 0. 8 8 52 0. 01 5 2 3 0. 0 0 0 0 0 - 0. 0 8 2 3 0. 01 0 0 0.1 0 0 0 6. 0 0 0 0. 9417 0. 01 5 5 5 0. 0 0 0 0 0 - 0. 0 8 2 9 0. 01 0 0 0.1 0 0 0 6. 5 0 0 0. 9 96 3 0. 01 5 9 2 0. 0 0 0 0 0 - 0. 0 8 34 0. 01 0 0 0.1 0 0 0 7. 0 0 0 1. 04 91 0. 01636 0. 0 0 0 0 0 - 0. 0 8 3 3 0. 01 0 0 0. 1 0 0 0 7. 5 0 0 1. 0 9 7 9 0. 016 8 5 0. 0 0 0 0 0 - 0. 0 8 2 9 0. 01 0 0 0.1 0 00 7. 7 5 0 1.1202 0. 01 714 0. 0 0 0 0 0 - 0. 0 8 2 2 0. 01 0 0 0.1 0 0 0 8.0 0 0 1.14 0 5 0. 01746 0. 0 0 0 0 0 - 0. 0 814 0. 01 0 0 0.1 0 0 0 8.2 5 0 1.1 5 81 0. 01 7 80 0. 0 0 0 0 0 - 0. 0 7 9 8 0. 01 0 0 0.1 0 0 0 8.5 0 0 1.16 8 7 0. 01 81 8 0. 0 0 0 0 0 - 0. 0774 0.01 0 0 0.1 0 0 0 8. 7 5 0 1.1 7 7 5 0. 01 864 0. 0 0 0 0 0 - 0. 0 74 7 0. 01 0 0 0.1 0 0 0 9. 0 0 0 1.1 842 0. 01 9 2 0 0. 00 0 0 0 - 0. 0 7 21 0. 01 0 0 0.1 0 0 0 9.2 5 0 1.1 9 3 0 0. 01 9 9 0 0. 0 0 0 0 0 - 0. 0 7 0 3 0. 010 0 0.1 0 0 0 9. 5 0 0 1.1 9 92 0. 0 2 0 76 0. 0 0 0 0 0 - 0. 06 84 0. 01 0 0 0.1 0 0 0 9.7 5 0 1.2 0 31 0. 0 21 7 9 0. 0 0 0 0 0 - 0. 0671 0. 01 0 0 0.1 0 0 0

1 0. 0 0 0 1. 2 0 5 9 0. 0 2 3 0 5 0. 0 0 0 0 0 - 0. 06 54 0. 01 0 0 0.1 0 0 0 1 0.2 5 0 1.2 0 7 8 0. 0245 3 0. 0 0 0 00 - 0. 0640 0. 010 0 0.1 0 0 0 1 0. 5 00 1.2 0 5 0 0. 02622 0. 0 0 0 0 0 -0.0626 0. 01 0 0 0.1 0 0 0 1 0.7 5 0 1.2 0 2 5 0. 0 2 8 2 3 0. 0 0 0 0 0 - 0. 06 16 0. 01 0 0 0.1 0 0 0 1 1. 0 0 0 1. 2 01 9 0. 0 3 02 8 0. 0 0 0 0 0 - 0. 0614 0. 0 1 0 0 0.1 0 0 0 11. 2 5 0 1.1 9 1 2 0. 0 3 2 7 5 0. 0 0 0 0 0 - 0. 0 5 95 0. 01 0 0 0.1 0 0 0 11. 5 0 0 1.1 91 0 0. 0 3 5 34 0. 0 0 0 0 0 - 0. 0622 0. 01 0 0 0.1 0 0 0

FFA TN 1990-15 11 POL.W1 2 8_10_ 9;1

XFOIL Version 5.0

Cal culated polar for: FFA-vU-12 8

1 Reynolds number fixed

xtr f .. 1. 00 0 (suction) 1. 0 0 0 (pre ssure) Ma ch .. 0.150 Re .. 1.000 e 6 Ncr it 9. 000

alpha CL CD Re(CL) CM S xtr P xtr ------ - -------- --------- --------- -------- ------- -------

0 . 0 0 0 0.334 8 0.00701 1. 00 0 00 - 0. 0 52 2 0. 53 54 0. 5314 0 .5 0 0 0.3 9 0 2 0.0063 5 1.0 0 000 -0. 0 5 23 0. 5 2 5 7 0.7 8 80 1. 0 00 0.4417 0. 006 0 7 1. 00 000 -0. 0 50 7 0. 5215 0. 9 0 93 1 . 50 0 0.4 931 0. 00603 1. 00000 - 0. 04 91 0. 51 5 8 0. 9643 2 . 5 00 0.6 2 9 9 0 . 006 2 7 1.000 00 - 0. 0 543 0. 5000 1.0000 3.0 0 0 0.6 8 80 0. 0063 9 1. 00 000 - 0. 0 54 8 0.4 94 5 1. 0 0 00 3.500 0. 746 5 0. 00656 1.00000 -0.05 54 0.4 8 5 9 1.0000 4 .000 0. 804 9 0. 00676 1.000 00 -0.0560 0.4 7 81 1.0000 4. 500 0. 8636 0. 006 92 1. 0 0 000 - 0. 0 56 7 0 . 4 7 2 2 1. 0000 5. 000 0. 9221 0.00713 1. 00000 -0. 0 5 73 0.462 7 1 . 0000 5.5 00 0. 9 804 0.00734 1. 00000 -0. 0 5 80 0.4 5 0 2 1. 0000 6 .000 1.03 84 0. 0 0 764 1.00000 -0.0 5 86 0.430 9 1.0000 6. 500 1.0 9 5 9 0. 0 0 7 9 9 1.0 0000 - 0. 0 5 9 2 0. 4111 1.0 000 7.000 1.1530 0. 0 0 83 8 1.00000 -0.0 5 9 8 0.3 926 1.0000 7.500 1. 20 74 0. 00 914 1. 00000 -0.0601 0.3 527 1. 0000 8.000 1. 2 5 71 0.010 42 1.00000 -0.0602 0. 2 8 96 1. 0000 8. 5 00 1. 2 966 0. 01269 1.00000 - 0. 0 5 96 0.1 9 5 7 1.0 000 9.0 00 1. 3 2 56 0. 01 5 5 7 1.0 0000 -0.0 5 8 2 0.1 0 8 7 1. 0000 9.500 1.3 5 2 2 0.01 7 96 1.00000 -0.0566 0. 0 7 2 7 1. 00 00

1 0.000 1.3 71 7 0.020 8 5 1.00000 -0.0 5 51 0. 0 544 1. 0 0 0 0 1 0. 500 1. 3 901 0. 0 2423 1.00000 -0.0 542 0. 0440 1. 0000 11.000 1.403 8 0.02 831 1.00000 -0. 0 536 0.034 7 1.0000 11. 500 1.41 8 9 0.032 51 1.00000 -0.0531 0. 0 2 9 5 1. 0 0 00 12.000 1. 4310 0. 0371 9 1.000 00 -0.0 5 2 7 0.0 236 1.0 000 12. 5 00 1. 443 7 0. 041 94 1.00000 -0. 0 5 26 0. 0 21 5 1. 0000 13.000 1.4 53 8 0. 04711 1. 0 0000 -0.0 526 0. 01 9 7 1.0000 13. 5 00 1. 4612 0.0 5 2 80 1.00000 -0.0 5 2 8 0. 016 9 1. 0 0 00 14.0 00 1. 460 5 0. 0 5 9 86 1.000 00 - 0. 0 531 0. 0131 1.00 00 14. 5 00 1. 4636 0. 06656 1. 0 0000 -0.0 53 8 0. 011 7 1. 0 000 1 5. 0 00 1.4746 0. 0 7 242 1.00000 -0. 0 54 7 0. 0112 1. 0 0 0 0 1 5. 5 00 1. 4 813 0. 0 7 90 7 1.000 00 - 0.0 5 5 9 0. 0104 1. 0 0 00 16.0 00 1. 4 84 2 0. 0 8651 1.00 000 - 0.0 5 73 0. 00 93 1. 0 0 00 16. 5 00 1.4 7 8 0 0. 0 95 7 5 1. 0 00 0 0 -0. 0 5 92 0.0 0 7 8 1. 0 0 0 0 17.000 1. 4215 0.11 503 1. 0 0 0 0 0 -0.0642 0. 0 060 1.0 00 0 - 0. 5 00 0. 2 7 76 0. 0 0 7 7 5 1. 00 000 - 0. 0 516 0.5422 0.2 846 -1. 0 00 0.21 93 0. 0 0 81 8 1. 00 0 0 0 - 0.0510 0. 546 8 0.16 7 7 -1. 50 0 0.1606 0.00844 1. 0 00 00 - 0. 0 5 04 0. 5 5 55 0.1 0 04 - 2. 0 00 0.1 016 0.00 86 7 1. 0 00 0 0 - 0. 0 5 0 0 0.56 2 8 0. 064 7 -2. 5 00 0. 0426 0. 0 0 8 9 0 1.00 0 00 - 0.04 96 0.56 8 7 0. 0 5 2 0 -3.0 0 0 - 0.0163 0. 0 0 931 1. 00000 - 0. 04 94 0. 5 7 7 0 0. 03 8 2 -3.50 0 - 0. 0 7 52 0. 00 94 8 1. 0 000 0 - 0. 04 9 0 0. 5 8 51 0. 034 8 - 4.0 00 - 0.132 2 0.010 9 5 1. 0 000 0 -0. 04 94 0.5 9 0 7 0. 0 2 2 7 - 4.5 0 0 - 0.1 90 9 0. 01 0 9 7 1.00 000 - 0.04 9 0 0.6 00 7 0. 0 21 7 - 5.0 0 0 - 0. 24 91 0. 011 2 7 1. 000 0 0 -0. 04 8 8 0.6 0 8 8 0. 01 9 7 - 5 . 5 0 0 - 0.3 0 5 7 0. 0123 0 1. 0 000 0 - 0. 04 9 0 0.614 7 0. 01 5 8

FFA TN 1990-15 12 POL.W 1 2 8_ 1 0_TU1;2

XFOIL Version 5. 0

Ca lculated polar for: FFA-W 1-12 8

1 Reyno lds number fixed

xtrf ... 0. 0 1 0 (suction) 0.1 0 0 (pressure) Mach ... 0.1 5 0 Re = 1. 0 0 0 e 6 Ncrit = 9. 0 0 0

alpha C L CD Re (CL) CM S xtr P xtr ------- -------- --------- --------- -------- ------- -------

0. 0 0 0 0.32 8 5 0. 011 5 3 1. 0 0 0 0 0 - 0. 0 5 2 5 0. 01 0 0 0.1 00 0 0.5 0 0 0.3 8 6 5 0. 011 6 9 1. 0 0 0 0 0 - 0. 0 5 3 0 0. 01 0 0 0.1 0 0 0 1. 0 0 0 0.444 3 0. 011 8 8 1. 0 0 0 0 0 - 0. 0 5 3 5 0. 01 0 0 0.1 0 0 0 1. 5 0 0 0. 5 01 9 0. 01 2 0 9 1. 0 0 0 0 0 - 0. 0 5 3 9 0. 01 0 0 0.1 0 0 0 2. 0 0 0 0.5 5 92 0.01 2 3 3 1. 00 0 0 0 - 0. 0544 0. 01 0 0 0.1 0 0 0 2. 5 0 0 0. 61 6 2 0. 01 2 6 0 1. 0 0 0 0 0 - 0. 0 54 9 0. 01 0 0 0.1 0 0 0 3. 0 0 0 0. 6 7 2 8 0.012 8 9 1. 0 0 0 0 0 - 0. 0 5 5 3 0. 01 0 0 0.1 0 0 0 3. 5 0 0 0. 7 2 91 0. 013 2 3 1. 00 0 0 0 - 0. 0 5 5 7 0. 0 1 0 0 0.1 0 0 0 4. 0 0 0 0. 7 84 8 0. 01 3 5 9 1. 0 0 0 0 0 - 0.0 5 6 1 0. 0 1 0 0 0.1 0 0 0 4. 5 0 0 0. 84 0 0 0. 014 0 0 1. 0 0 0 0 0 - 0. 0 5 65 0. 01 0 0 0.1 0 0 0 5. 0 0 0 0. 8 94 5 0. 0144 5 1.0 0 0 0 0 - 0. 0 5 6 7 0.0 1 0 0 0.1 0 0 0 5.50 0 0. 94 8 2 0. 0 14 9 5 1. 0 0 0 0 0 - 0. 0 5 7 0 0. 0 1 0 0 0.1 0 0 0 6. 00 0 1. 0 0 09 0.0 1 5 5 2 1. 0 0 0 0 0 - 0. 0 5 7 1 0. 01 0 0 0.1 0 0 0 6. 5 0 0 1. 0 5 24 0. 01 615 1. 0 0 0 0 0 - 0. 0 5 7 2 0. 0 1 0 0 0. 1 0 0 0 7. 0 0 0 1.1 0 24 0. 01 6 8 6 1. 0 0 0 0 0 - 0. 0 5 7 1 0. 01 0 0 0. 1 0 0 0 7. 5 0 0 1.15 04 0. 01 7 6 8 1. 0 00 0 0 - 0. 0 5 6 8 0. 01 0 0 0. 1 0 0 0 8. 0 0 0 1.1 9 5 7 0. 0 1 8 64 1. 0 0 0 0 0 - 0. 0 5 64 0. 01 0 0 0.1 0 0 0 8. 5 0 0 1. 2 2 92 0. 02 0 0 2 1. 00 0 0 0 - 0. 0 5 5 0 0. 0 1 0 0 0.1 0 0 0 9. 0 0 0 1.26 0 8 0. 0 2 194 1. 0 0 0 00 - 0. 0 542 0.0 1 0 0 0.1 0 0 0 9. 5 0 0 1.2 89 3 0. 0 24 2 8 1. 0 0 0 0 0 - 0. 0 5 3 5 0. 01 0 0 0.1 0 0 0

1 0. 0 0 0 1. 3 1 5 2 0. 0 2 7 0 2 1. 0 0 0 0 0 - 0. 0 529 0. 01 0 0 0.1 0 0 0 1 0. 5 0 0 1. 3 3 8 5 0. 0 3 014 1. 0 0 0 0 0 - 0. 0525 0. 01 0 0 0. 1 00 0 11. 0 0 0 1. 3 6 0 0 0. 0 33 61 1. 0 0 00 0 - 0. 0 521 0. 01 0 0 0.1 0 0 0 11. 5 0 0 1. 3 7 9 0 0. 0 3 744 1. 00 00 0 - 0. 0 5 19 0. 0 1 0 0 0. 1 0 0 0 12. 0 0 0 1. 3 9 69 0. 041 5 6 1. 0 0 0 0 0 - 0. 0 5 1 7 0. 0 1 0 0 0.1 0 0 0 12. 50 0 1.412 7 0. 04 5 9 9 1. 0 0 0 0 0 - 0. 0 5 17 0. 0 1 0 0 0. 1 0 0 0 13. 0 0 0 1. 42 7 1 0. 0 5 0 71 1. 0 0 0 0 0 - 0. 0 51 8 0.010 0 0.1 0 0 0 1 3. 5 0 0 1.44 0 8 0. 0 5 5 6 8 1. 0 0 00 0 - 0. 0 5 2 0 0. 0 1 0 0 0.1 0 0 0 14. 0 0 0 1. 4 5 3 1 0. 0 6 09 9 1. 0 0 0 0 0 - 0. 0 524 0. 01 0 0 0.1 0 0 0 14. 5 0 0 1.4 632 0. 0 6 6 74 1. 0 0 0 0 0 - 0. 05 3 0 0. 01 0 0 0.1 0 0 0 15. 0 0 0 1. 4 7 1 9 0. 0 7 2 92 1.0 0 0 0 0 - 0. 0 5 3 8 0. 01 0 0 0.1 0 0 0 1 5. 5 0 0 1. 4 7 7 0 0. 0 7 9 84 1. 0 00 0 0 - 0. 054 8 0. 01 0 0 0.1 0 0 0 1 6. 0 0 0 1.4 7 7 6 0. 0 8 7 6 0 1. 0 0 0 0 0 - 0. 0 5 62 0. 0 0 94 0.1 0 0 0 1 6. 5 0 0 1.4 7 2 9 0. 0 9 6 6 3 1. 0 0 0 0 0 - 0. 0 5 81 0. 0 0 8 0 0.1 0 0 0 17. 0 0 0 1.414 7 0.11 62 6 1. 0 0 0 0 0 - 0. 0 632 0. 0 0 6 0 0.1 0 0 0 - 0. 5 0 0 0.2 7 0 3 0. 0114 0 1. 0 0 0 0 0 - 0. 0 521 0. 01 0 0 0.1 0 0 0 -1. 0 0 0 0.212 0 0. 011 2 8 1. 0 0 0 0 0 -0.0 51 7 0. 01 0 0 0.1 0 0 0 -1. 5 0 0 0.1 5 3 6 0. 01121 1. 0 0 0 0 0 - 0. 0 51 3 0. 01 0 0 0. 09 7 9 - 2. 0 0 0 0. 0 95 5 0. 0 11 31 1. 0 0 0 0 0 - 0. 0 5 0 9 0. 01 0 0 0. 0 62 6 - 2. 5 0 0 0. 0 3 73 0. 01142 1. 0 0 0 0 0 - 0. 0 5 0 6 0. 01 0 0 0. 0 51 2 - 3. 5 0 0 - 0. 0 7 9 0 0. 011 8 2 1. 0 0 0 0 0 - 0. 05 01 0. 01 0 0 0. 0 34 5

FFA TN 1 9 9 0 - 1 5 1 3

XFOIL Version 5. 0

Calculated polar for: FFA-W 1-12 8

1 Reynolds number fixed

xtr f - 1. 0 0 0 (suction) 1. 0 0 0 (pressure) Mach -

a lpha -- -----

2 . 0 0 0 2 . 5 0 0 3. 5 0 0 4. 0 0 0 4. 5 0 0 5. 0 0 0 5. 5 0 0 6. 0 0 0 6. 5 0 0 7. 0 0 0 7. 5 0 0 8. 0 0 0 8. 5 0 0 9. 0 0 0 9. 5 0 0

1 0. 0 0 0 1 0. 5 0 0 11. 0 0 0 1 1. 5 0 0 12. 0 0 0 1 2. 5 0 0 13. 0 0 0 13.5 0 0 14.0 0 0 14.5 0 0 1 5.0 0 0 1 5.5 0 0 1 6.0 0 0 1 6.5 0 0 1 7.0 0 0

1.5 0 0 1. 0 0 0 0.5 0 0 0.0 0 0

- 0.5 0 0 -1.0 0 0 -1.5 0 0 - 2.0 0 0 - 2.5 0 0 - 3.0 0 0 - 3.5 0 0 -4.0 0 0 -4.5 0 0 - 5.0 0 0 -6.0 0 0 -6.5 0 0 -7 . 0 0 0 -7 . 5 0 0

0.1 5 0

CL --------

0. 5 65 8 0. 6 2 0 7 0. 74 81 0. 8 0 73 0. 8 6 6 5 0. 9 2 5 5 0. 9 842 1. 0424 1. 0 9 9 7 1.1541 1.2 0 54 1.2 523 1.2 942 1. 33 93 1. 3 813 1. 4114 1.43 8 7 1 . 4 623 1.4 7 93 1.4 94 6 1. 5 0 9 8 1. 5 2 1 2 1.532 9 1. 53 93 1. 54 6 7 1 . 54 9 0 1.5 521 1. 5 5 9 6 1.5 642 1. 5 6 7 0 0. 5 0 9 7 0.4 54 0 0.3 9 5 6 0.33 7 0 0.2 7 7 9 0.21 8 8 0.1 5 9 5 0.1 0 0 0 0. 04 04

- 0. 01 8 9 - 0. 0 7 8 2 - 0.13 7 0 - 0.1 9 63 -0. 2 5 5 2 -0.3 6 7 6 - 0.42 61 - 0.4 8 3 9 - 0. 54 03

Re = 2. 0 0 0 e 6 Ncr it

CD Re CCL) CM --------- --------- --------

0. 0 0 5 0 1 2. 0 0 0 0 0 - 0. 0 5 2 9 0. 0 0 5 03 2. 0 0 0 0 0 - 0. 0 5 23 0. 0 0 523 2. 0 0 0 0 0 - 0. 0 5 5 5 0. 0 0 53 7 2. 0 0 0 0 0 - 0. 0 5 62 0. 0 0 5 54 2. 0 0 0 0 0 - 0. 0 5 6 9 0. 0 0 5 7 5 2. 0 0 0 0 0 - 0. 0 5 7 7 0. 0 0 6 0 1 2. 0 0 0 0 0 - 0. 0 5 84 0. 0 0 633 2. 0 0 0 0 0 - 0. 0 5 9 1 0. 0 0 6 8 0 2. 0 0 0 0 0 - 0. 0 5 9 8 0. 0 0 7 71 2. 0 0 0 0 0 - 0. 0 6 03 0. 0 0 8 9 8 2. 0 0 0 0 0 - 0. 0 6 0 6 0. 0 1 0 6 6 2.0 0 0 0 0 - 0. 0 6 0 5 0. 012 62 2. 0 0 0 0 0 - 0. 0 6 0 1 0. 0 13 9 6 2. 0 0 0 0 0 - 0. 0 5 9 7 0. 0 1 53 9 2. 0 0 0 0 0 - 0. 0 5 9 0 0. 0 1 73 1 2. 0 0 0 0 0 - 0. 0 5 7 5 0. 01 9 5 2 2. 0 0 0 0 0 - 0. 0 5 64 0. 0 2 233 2. 0 0 0 0 0 - 0. 0 5 5 5 0.02 5 9 7 2. 0 0 0 0 0 - 0. 0 54 8 0. 03 0 0 2 2. 0 0 0 0 0 - 0. 0 542 0. 03424 2. 0 0 0 0 0 - 0. 0 53 7 0.03 9 0 0 2. 0 0 0 0 0 - 0. 0 534 0. 043 92 2.0 0 0 0 0 -0. 0 534 0. 04 9 5 7 2. 0 0 0 0 0 - 0. 0 534 0. 0 5 534 2. 0 0 0 0 0 - 0. 0 53 7 0. 0 6202 2. 0 0 0 0 0 - 0. 0 54 1 0. 0 6 8 7 2 2. 0 0 0 0 0 - 0. 0 54 8 0. 0 7 5 13 2. 0 0 0 0 0 - 0. 0 5 5 8 0. 0 8 2 1 5 2. 0 0 0 0 0 - 0. 0 5 71 0.0 8 9 54 2. 0 0 0 0 0 - 0. 0 5 8 5 0. 0 0 5 0 6 2. 0 0 0 0 0 - 0. 0 531 0. 0 0 5 6 1 2. 0 0 0 0 0 - 0. 0 532 0. 0 0 6 0 8 2. 0 0 0 0 0 - 0. 0 5 2 5 0. 0 0 6 53 2.0 0 0 0 0 - 0. 0 51 8 0. 0 0 6 8 0 2. 0 0 0 0 0 - 0. 0 51 1 0. 0 0 7 0 8 2. 0 0 0 0 0 - 0. 0 5 0 5 0. 0 0 7 2 7 2. 0 0 0 0 0 - 0. 04 9 9 0. 0 0 74 2 2.0 0 0 0 0 - 0 . 04 94 0. 0 0 7 6 1 2. 0 0 0 0 0 - 0. 04 9 0 0. 0 0 7 7 5 2. 0 0 0 0 0 - 0. 04 8 6 0. 0 0 8 03 2. 0 0 0 0 0 - 0. 04 83 0. 0 0 8 52 2.0 0 0 0 0 - 0. 04 81 0. 0 0 8 53 2. 0 0 0 0 0 - 0. 04 7 7 0. 0 0 8 83 2. 0 0 0 0 0 - 0. 04 7 5 0. 011 5 7 2. 0 0 0 0 0 - 0. 04 8 2 0. 011 7 0 2. 0 0 0 0 0 - 0. 04 7 9 0. 01 2 0 8 2. 0 0 0 0 0 - 0. 04 7 9 0. 012 8 7 2. 0 0 0 0 0 - 0. 04 81

POL.W 1 2 8_ 2 0_ 9; 1

9. 0 0 0

S xtr P xtr ------ - -------0.4 83 6 0. 92 0 0 0.4 7 7 5 0. 9 5 5 0 0.4 6 1 0 1. 0 0 0 0 0.4 543 1. 0 0 0 0 0.44 6 8 1. 0 0 0 0 0.431 8 1.0 0 0 0 0.4 13 1 1. 0 0 0 0 0.3 9 5 8 1. 0 0 0 0 0.3 6 5 0 1. 0 0 0 0 0.311 0 1. 0 0 0 0 0.2422 1. 0 0 0 0 0.1 612 1. 0 0 0 0 0. 0 92 7 1. 0 0 0 0 0. 0 5 9 5 1. 0 0 0 0 0. 04 0 6 1. 0 0 0 0 0. 032 8 1. 0 0 0 0 0. 0 2 6 2 1. 0 0 0 0 0. 0 2 2 0 1. 0 0 0 0 0. 0 2 0 1 1 . 0 0 0 0 0. 0 1 7 2 1. 0 0 0 0 0. 0 13 9 1. 0 0 0 0 0. 011 9 1. 0 0 0 0 0. 01 13 1. 0 0 0 0 0. 01 01 1.0 0 0 0 0. 0 0 84 1. 0 0 0 0 0. 0 0 6 5 1. 0 0 0 0 0. 0 0 5 9 1. 0 0 0 0 0. 0 0 5 8 1. 0 0 0 0 0. 0 0 5 5 1. 0 0 0 0 0. 0 0 5 2 1. 0 0 0 0 0.4 9 24 0. 8 61 7 0.4 9 8 6 0. 631 6 0. 5 023 0.44 5 0 0.51 2 0 0. 2 7 2 1 0. 51 8 8 0.1 7 63 0. 5233 0.1 0 2 7 0. 53 03 0. 0 6 8 9 0.53 8 9 0. 0 524 0. 5443 0. 03 9 0 0. 54 81 0. 03 63 0. 5 5 9 7 0. 0 2 7 0 0.5 6 6 0 0 . 02 2 6 0. 5 7 03 0. 0 2 1 6 0. 5 8 2 2 0. 01 83 0. 5 933 0. 012 2 0. 6 0 5 0 0. 011 9 0. 6121 0. 0112 0. 6 21 5 0. 01 0 2

FFA TN 1 9 9 0 - 1 5 1 4 POL.W 1 2 8_30_9;2

XFOIL Version 5.0

Calculated polar for: FFA-W1-12 8

1 Reynolds number fixed

xtr f = 1.000 ( suction) 1. 000 (pressure) Mach • 0.1 50 Re = 3.000 e 6 Ncr it 9.000

a lpha CL CD Re(CL) CM s xtr P xtr ------- -------- --------- --------- -------- ------- -------- 2.000 0.09 8 5 0.00 6 89 3.00000 -0.0490 0. 5229 0.04 6 3 - 1. 500 0.15 8 2 0.00 6 7 5 3.00000 -0.049 6 0. 51 50 0.0 604 - 1. 000 0.2179 0.00 6 59 3.00000 -0.0 502 0. 5110 0.0 8 69 -0. 500 0. 2 7 74 0.00 6 3 8 3.00000 - 0.050 8 0. 50 3 2 0.14 2 5

0.000 0. 3 3 70 0.00 6 1 7 3.00000 -0.0 51 5 0.49 60 0.2120 0. 500 0.39 63 0.00 5 8 7 3.00000 -0.0 523 0.4913 0. 3 30 1 1.000 0.4 5 5 7 0.00 5 60 3.00000 -0.0 53 1 0.4 84 1 0.4494 1. 500 0. 5140 0.00497 3.00000 -0.0 539 0.47 6 6 0. 71 59 2.000 0. 5723 0.004 73 3.00000 -0.0 543 0. 4 713 0. 84 6 6 2. 500 0. 630 1 0.004 69 3.00000 -0.0 54 6 0.4 6 13 0.9024 3.000 0. 6 8 59 0.004 6 8 3.00000 -0.0 543 0.45. 59 0.94 63 3. 500 0. 7404 0.004 73 3.00000 -0.0 53 7 0.44 8 1 0.9799 4.000 0. 80 8 1 0.00485 3.00000 -0.0 5 63 0.4 3 8 8 1. 0000 4.500 0. 8 6 7 6 0.00 504 3. 00000 -0.0 5 7 1 0.42 6 1 1.0000 5.000 0.9 2 6 7 0.00 52 8 3.00000 -0.0 579 0.4 100 1.0000 5.500 0.9 8 5 5 0.00 5 59 3.00000 -0.0 5 8 7 0. 3 8 59 1.0000 6.000 1. 0435 0.00 60 1 3.00000 -0.0594 0. 3 603 1.0000 6.500 1.0999 0.00 67 1 3.00000 -0.0 60 1 0. 3090 1. 0000 7.000 1.1 545 0. 00 7 65 3.00000 -0.0 60 7 0.2 5 2 7 1.0000 7. 500 1. 203 6 0.00929 3.0000 0 -0.0 609 0.1 6 5 7 1.0000 8.000 1.2 5 3 1 0.010 62 3.00000 -0.0 6 10 0.10 6 6 1.0000 8.500 1. 3003 0.01200 3.00000 -0.0 60 8 0.0 6 70 1.0000 9.000 1. 34 8 2 0.0 1 3 1 2 3.00000 -0.0 60 7 0.04 74 1.0000 9. 500 1. 394 6 0.0 1425 3.00000 -0. 0 603 0.0344 1.0000

10.000 1 . 4395 0.01 53 7 3.00000 -0.059 8 0. 0245 1.0000 10. 500 1.4 693 0.0 1 722 3.00000 -0.0 5 84 0.0218 1.0000 11.000 1. 49 5 5 0.019 5 6 3.00000 -0.0573 0.0179 1.0000 12.000 1. 5 342 0.0 2 6 2 7 3.00000 -0. 0 5 5 8 0.0133 1.0000 1 2. 500 1. 549 6 0.0 3035 3.00000 -0.0 5 53 0. 0 11 2 1.0000

FFA TN 1 9 9 0 - 1 5 1 5 POL.W12 8_30_TU1;3

XFOIL Version 5.0

Calculated polar for: FFA-W1-12 8

1 Reynolds number fixed

xtrf • 0.010 ( su ction) 0.100 (pressure) Mach • 0.150 Re = 3.000 e 6 Ncr it 9.000

alpha C L C D Re (CL) CM S xtr P xtr ------- -------- --------- ----- --- - -------- ------- -- ------3 . 00000 -0.02300 0.00 942 3.00000 -0.04 940 0.01000 0.032 50 - 2. 50000 0.03600 0.00 934 3.00000 -0.04 9 80 0.01000 0.03810 - 2. 00000 0.0 94 90 0.00 932 3.00000 -0.0 5020 0.01000 0.044 50 - 1. 50000 0.153 90 0.00 930 3.00000 -0.05070 0.01000 0.0 5 7 50 - 1.00000 0.21 2 60 0.00 9 2 7 3.00000 -0.0 5120 0.01000 0.0 80 50 -0. 50000 0.2 71 50 0.00 93 2 3.00000 -0.05170 0.01000 0.10000

0.00000 0.33040 0.00 944 3.00000 -0.0 5220 0.01000 0.10000 0. 50000 0.3 8 910 0.00 9 5 8 3.00000 -0.0 5270 0.01000 0.10000 1.00000 0.44 7 70 0.00 9 73 3.00000 -0.0 5330 0.01000 0.10000 1. 50000 0.50 610 0.00 9 91 3.00000 -0.0 53 90 0.01000 0.10000 2.00000 0. 5 6440 0.01010 3.00000 -0.05440 0.01000 0.10000 2. 500 0. 6234 0.01032 3.00000 -0.0 5 52 0.0100 0.1000 3.000 0. 6 813 0.010 5 5 3.00000 -0.0 5 5 8 0.0100 0.1000 3. 500 0. 73 8 9 0.010 80 3.00000 -0.0 5 63 0.0100 0.1000 4.000 0.7 9 61 0.0110 8 3.00000 -0.0 5 6 9 0.0100 0.1000 4. 500 0. 8 531 0.0113 9 3.00000 -0.0 574 0.0100 0.1000 5.000 0. 90 9 6 0.011 7 2 3.00000 -0.0 5 7 9 0.0100 0.1000 5. 500 0. 9 6 5 6 0.0120 9 3.00000 -0.0 5 83 0.0100 0.1000 6.000 1.0211 0.0124 9 3.00000 -0.0 5 8 7 0.0100 0.1000 6. 500 1.0 7 5 9 0.012 93 3.00000 -0.0 5 90 0.0100 0.1000 7.000 1.12 9 9 0.01341 3.00000 -0.0 5 93 0.0100 0.1000 7. 500 1.1830 0.013 94 3.00000 -0.0 5 9 5 0.0100 0.1000 8 .000 1.23 50 0.014 53 3.00000 -0.0 5 9 5 0.0100 0.1000 8 . 500 1. 2 8 5 6 0.01 51 9 3.00000 -0.0 5 94 0.0100 0.1000 9.000 1. 3343 0.01 5 94 3.00000 -0.0 5 9 2 0.0100 0.1000 9 . 500 1.3804 0.01 6 81 3.00000 -0.0 5 8 7 0.0100 0.1000

10.000 1. 413 6 0.01 810 3.00000 -0.0 5 71 0.0100 0.1000 10. 500 1. 4445 0.01 9 9 8 3.00000 -0.0 5 61 0.0100 0.1000 11.000 1. 4 7 20 0.02 23 2 3.00000 -0.05 53 0.0100 0.1000 11. 500 1. 4 9 6 5 0.0 2 51 2 3.00000 -0.0 54 6 0.0100 0.1000 1 2.000 1. 51 83 0.02 834 3.00000 -0.0541 0.0100 0.1000 1 2 . 500 1. 53 81 0.031 91 3.00000 -0.053 6 0.0100 0.1000 13.000 1. 5 541 0.03 60 5 3.00000 -0.0 532 0.00 9 2 0.1000

FFA TN 1 9 9 0 - 1 5 1 6 POL.W152_ 1 0_9; 3

XFOIL Version 5. 0

Ca lculated polar for: FFA-Wl- 152

1 Reynolds number fixed

xtr f • 1. 0 0 0 (suction) 1. 0 0 0 (pre ssure) Mach • 0. 15 0 Re c 1. 0 0 0 e 6 Ncrit = 9. 0 0 0

alpha CL CD Re (CL ) CM S xtr P xtr ------- -------- --------- --------- -------- ------- -------

- 1 0 . 0 0 0 0 0 - 0. 4 3 3 1 0 0. 1 0 0 7 8 1. 0 0 0 0 0 - 0. 0 0 8 0 0 0. 652 8 0 0. 0 0 82 0 -9 . 5 0 0 0 0 - 0. 4 4 1 6 0 0. 0 8 65 6 1. 0 0 0 0 0 - 0. 0 1 7 0 0 0. 6 4 6 8 0 0. 0 0 85 0 -9.0 0 0 0 0 - 0. 4 62 1 0 0. 0 655 0 1. 0 0 0 0 0 - 0. 0 3 4 3 0 0. 6 425 0 0. 0 0 8 8 0 - 8 . 5 0 0 0 0 - 0.5 0 3 4 0 0. 0 42 3 3 1. 0 0 0 0 0 - 0. 0 499 0 0. 6 37 3 0 0. 0 092 0 - 8. 0 0 0 0 0 - 0.5 09 4 0 0. 0 29 2 8 1. 0 0 0 0 0 - 0. 052 4 0 0. 6 297 0 0. 0 099 0 - 7. 5 0 0 0 0 - 0. 4 795 0 0. 0 2 2 8 8 1. 00 0 0 0 - 0. 052 1 0 0. 6 2 250 0. 0 1 0 7 0 -5. 0 0 0 0 0 - 0. 22 6 0 0 0. 0 1 1 3 8 1. 0 0 0 0 0 - 0. 05 0 2 0 0.5 85 1 0 0. 0 1920 - 4.5 0 0 00 - 0 . 1 6 7 6 0 0. 0 1 0 8 6 1. 0 0 0 0 0 - 0. 05 05 0 0.5 7 6 0 0 0. 0 2 2 0 0 - 4. 0 0 0 0 0 - 0. 1 0 8 6 0 0. 0 1 055 1. 0 0 0 0 0 - 0. 05 1 0 0 0.5 7 0 8 0 0. 0 2 3 8 0 - 3.5 0 0 0 0 - 0. 0 49 8 0 0. 0 099 1 1. 0 0 00 0 - 0. 05 1 3 0 0.5 6 49 0 0. 0 3 1 2 0 - 3. 0 0 0 0 0 0. 0 09 7 0 0. 0 09 65 1.0 0 0 0 0 - 0. 05 1 8 0 0.55 6 4 0 0. 0 3 8 4 0 - 2.5 0 0 0 0 0. 0 69 4 0 0. 0 0937 1. 0 0 0 0 0 - 0. 052 4 0 0.55 2 00 0. 05 4 8 0 - 1.5 0 0 0 0 0. 1 8 8 6 0 0. 0 0 8 89 1. 0 0 0 0 0 - 0. 05 3 8 0 0.5 3 8 2 0 0. 129 0 0 - 1. 0 0 0 0 0 0.2 4 7 3 0 0. 0 0 8 3 0 1. 0 0 0 0 0 - 0. 05 4 7 0 0.53 4 1 0 0.2 7 3 8 0 - 0.5 0 0 0 0 0. 3 0 45 0 0. 0 0 7 1 1 1. 0 0 0 0 0 - 0. 055 8 0 0.52 8 7 0 0. 6 157 0

0. 0 0 0 0 0 0. 3 6 35 0 0. 0 0 6 8 8 1. 0 0 0 0 0 - 0. 05 6 4 0 0.5 2 1 0 0 0. 7 3 1 0 0 0.5 0 0 0 0 0. 4 2 2 2 0 0. 0 0 6 8 2 1. 0 0 0 0 0 - 0. 05 6 8 0 0.5 1 6 80 0. 79 0 6 0 1. 0 0 0 0.4 8 1 1 0.0 0 6 8 3 1.0 0 0 0 0 - 0. 05 7 2 0.5 1 19 0. 8 2 4 1 1.5 0 0 0.5 3 8 7 0. 0 0 6 89 1. 0 0 0 0 0 - 0. 05 7 4 0.5 05 4 0. 85 69 2. 0 0 0 0.595 6 0. 0 0 69 8 1. 0 0 0 0 0 - 0. 05 7 4 0. 499 1 0. 8 8 2 1 2.5 0 0 0. 65 3 6 0. 0 0 7 05 1. 0 0 0 0 0 - 0. 05 7 7 0. 49 4 8 0. 89 8 3 3. 0 0 0 0.7 1 09 0. 0 07 1 6 1. 0 0 0 0 0 - 0. 05 79 0. 4 8 8 8 0.9 1 4 3 3.5 0 0 0.7 6 69 0. 0 0 7 3 0 1. 0 0 0 0 0 - 0. 0579 0. 4 8 1 2 0.9 3 10 4. 0 0 0 0. 8 2 2 1 0. 0 0 7 3 8 1. 0 0 0 0 0 - 0. 05 7 7 0 . 47 6'7 0.9 4 89 4.5 0 0 0. 8 7 6 3 0. 0 0 7 49 1. 0 0 0 0 0 - 0.05 7 3 0. 4 69 6 0. 9 7 1 3 5.5 0 0 1. 0 0 75 0. 0 0 7 8 7 1. 0 0 0 0 0 - 0. 0 62 0 0. 45 4 2 1. 0 0 0 0 6 . 0 0 0 1. 0 6 7 0 0. 0 0 8 1 4 1. 0 0 0 0 0 - 0. 0 632 0. 4 4 3 4 1 . 0 0 0 0 6.5 0 0 1. 1 2 6 0 0. 0 0 8 4 0 1. 0 0 0 0 0 - 0. 0 6 4 2 0. 4 3 34 1. 0 0 0 0 7. 0 0 0 1. 1 8 39 0. 0 0 875 1. 0 0 0 0 0 - 0. 0 65 1 0. 4 1 8 1 1 . 0 0 0 0 7.5 0 0 1.2 4 0 8 0. 0 09 1 7 1.0 0 0 0 0 - 0. 0 659 0. 4 0 2 4 1. 0 0 0 0 8. 0 0 0 1.29 6 3 0. 0 09 7 0 1 . 0 0 0 0 0 - 0. 0 6 6 4 0. 3 8 2 8 1 . 0 0 0 0 8.5 0 0 1. 3 4 9 3 0. 0 1 0 4 0 1.0 0 0 0 0 - 0. 0 6 6 8 0. 35 7 2 1 . 0 0 0 0 9. 0 0 0 1. 3999 0. 0 11 25 1. 0 0 0 0 0 - 0. 0 6 6 8 0.33 0 4 1. 0 0 0 0 9.5 0 0 1. 4 4 4 3 0. 0 1 25 0 1. 0 0 0 0 0 - 0. 0 6 62 0.29 32 1. 0 0 0 0

1 0. 0 0 0 1 . 4 6 4 8 0.015 1 3 1. 0 0 0 0 0 - 0. 0 6 3 4 0.23 0 4 1. 0 0 0 0 1 0.5 0 0 1. 4 6 35 0. 0 1917 1. 0 0 0 0 0 - 0. 0 6 0 0 0.1 8 25 1. 0 0 0 0 1 1 . 5 0 0 1. 4 459 0. 0 3 095 1. 0 0 0 00 - 0. 05 6 4 0. 1 1 35 1. 0 0 0 0 1 2. 0 0 0 1. 4 4 19 0. 0 3 7 0 1 1. 0 0 0 0 0 - 0. 055 4 0. 092 0 1. 0 0 0 0 1 2. 5 0 0 1. 4 3 7 0 0. 043 4 1 1. 0 0 0 0 0 - 0. 05 4 7 0.07 39 1. 0 0 0 0 1 3. 0 0 0 1. 4 4 0 8 0. 0 49 09 1 . 0 0 0 0 0 - 0. 05 4 3 0. 0 6 0 3 1. 0 0 0 0 1 3.5 0 0 1. 4 4 15 0. 055 2 4 1 . 0 0 0 0 0 - 0. 054 1 0. 05 4 2 1. 0 0 0 0 1 4. 0 0 0 1. 4 49 0 0. 0 6 0 8 3 1. 0 0 0 0 0 - 0. 05 4 1 0. 0 4 39 1 . 0 0 0 0 1 4.5 0 0 1. 4515 0. 0 6 7 2 0 1. 0 0 0 0 0 - 0. 05 4 4 0. 0 40 4 1 . 0 0 0 0 1 5 . 0 0 0 1. 455 4 0. 0 7 35 8 1. 0 0 0 0 0 - 0. 05 4 8 0. 0 35 0 1 . 0 0 0 0

FFA TN 1 9 9 0 - 1 5 1 7

XFOI L Version 5 . 0

Cal culated polar for: FFA-W1 - 1 52

1 Reynolds number fixed

xtrf • 0 . 0 1 0 (su ction) 0 . 1 0 0 (pressure) Mach •

a lpha - - - - - - -

1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0 1 5 . 5 0 0 1 6 . 0 0 0 1 6 . 5 0 0 1 7 . 0 0 0 1 7 . 5 0 0 1 8 . 0 0 0

0 . 1 5 0 Re c

CL CD -------- ---------

0 . 4 6 9 0 0 . 0 1 2 7 5 0 . 52 6 3 0 . 0 1 2 9 9 0 . 5 8 3 1 0 . 0 1 3 2 6 0 . 6 3 9 4 0 . 0 1 3 5 7 0 . 6 9 5 1 0 . 0 1 3 9 1 0 . 7 5 0 1 0 . 0 1 4 2 9 0 . 8 0 4 3 0 . 0 1 4 7 2 0 . 8 5 7 5 0 . 0 1 5 2 0 0 . 9 0 9 5 0 . 0 1 5 7 3 0 . 9 5 9 9 0 . 0 1 6 3 4 1 . 0 0 8 4 0 . 0 1 7 0 4 1 . 0 5 4 0 0 . 0 1 7 8 6 1 . 0 8 6 6 0 . 0 1 9 0 8 1 . 1 2 0 9 0 . 0 2 0 7 3 1 . 1 5 1 9 0 . 0 2 2 7 6 1 . 1 8 0 2 0 . 0 2 5 1 6 1 . 2 0 6 0 0 . 0 2 7 9 0 1 . 2 3 0 1 0 . 0 3 0 9 4 1 . 2 5 1 7 0 . 0 3 4 3 1 1 . 2 7 1 8 0 . 0 3 7 9 3 1 . 2 9 0 6 0 . 0 4 1 7 6 1 . 3 0 8 1 0 . 0 4 5 8 2 1 . 32 4 8 0 . 0 5 0 1 0 1 . 3 4 0 2 0 . 0 5 4 6 0 1 . 3 5 4 9 0 . 0 5 9 3 1 1 . 3 6 8 6 0 . 0 6 4 2 5 1 . 3 8 1 4 0 . 0 6 9 3 5 1 . 3 9 3 6 0 . 0 7 4 6 5 1 . 4 0 4 8 0 . 0 8 0 3 4 1 . 4 1 5 4 0 . 0 8 62 0 1 . 4 2 5 7 0 . 0 92 1 3 1 . 4 3 4 4 0 . 0 9 8 62 1 . 4 4 2 7 0 . 1 0 5 3 3 1 . 4 5 0 4 0 . 1 12 2 2 1 . 4 5 5 7 0 . 1 1 9 7 5

1 . 0 0 0 e 6 Ncrit = 9 . 0 0 0

Re (CL) CM S xtr P xtr --------- -------- ------- - - -----

1 . 0 0 0 0 0 - 0 . 0 5 6 9 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 7 4 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 8 0 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 8 4 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 8 9 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 9 3 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 9 6 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 9 8 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 9 9 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 9 8 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 9 6 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 9 1 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 7 3 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 6 5 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 5 8 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 5 2 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 4 6 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 4 1 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 3 7 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 3 3 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 52 9 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 2 7 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 2 5 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 2 5 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 2 5 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 2 7 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 3 0 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 3 4 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 4 1 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 4 9 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 5 7 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 6 9 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 8 2 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 5 9 7 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 0 - 0 . 0 6 1 5 0 . 0 1 0 0 0 . 1 0 0 0

POL . W1 52_1 0_TU1 ; 2

FFA TN 1 9 9 0 - 1 5 1 8

XFOI L Ve rs ion 5 . 0

Calculated polar for : FFA-W1 - 1 52

1 Reynolds number fixed

xt rf • 1 . 0 0 0 ( suction ) 1 . 0 0 0 (pres sure ) Mach -= 0 . 1 5 0 Re ... 2 . 0 0 0 e 6 Ncr it

alpha CL CD Re (CL) CM ------- -------- --------- --------- ------ --- 9 . 5 0 0 0 0 - 0 . 4 3 3 1 0 0 . 0 9 0 0 5 2 . 0 0 0 0 0 - 0 . 0 1 3 6 0 - 9 . 0 0 0 0 0 - 0 . 4 4 6 1 0 0 . 0 7 3 7 0 2 . 0 0 0 0 0 - 0 . 0 2 5 6 0 - 8 . 5 0 0 0 0 - 0 . 4 7 5 3 0 0 . 0 4 8 6 3 2 . 0 0 0 0 0 - 0 . 0 4 6 6 0 -8 . 0 0 0 0 0 - 0 . 5 1 1 0 0 0 . 0 2 92 3 2 . 0 0 0 0 0 - 0 . 0 5 1 8 0 - 7 . 5 0 0 0 0 - o . 5 1 6 o o 0 . 0 1 37 8 2 . 0 0 0 0 0 - 0 . 0 4 9 1 0 - 7 . 0 0 0 0 0 - 0 . 4 6 3 1 0 0 . 0 1 2 0 1 2 . 0 0 0 0 0 - 0 . 0 4 8 6 0 - 6 . 5 0 0 0 0 - 0 . 4 0 5 3 0 0 . 0 1 1 4 6 2 . 0 0 0 0 0 - 0 . 0 4 8 8 0 - 6 . 0 0 0 0 0 - 0 . 3 4 6 8 0 0 . 0 1 1 0 4 2 . 0 0 0 0 0 - 0 . 0 4 9 1 0 - 5 . 5 0 0 0 0 - 0 . 2 8 7 6 0 0 . 0 1 0 8 0 2 . 0 0 0 0 0 - 0 . 0 4 95 0 - 4 . 5 0 0 0 0 - 0 . 1 7 1 8 0 0 . 0 0 8 9 8 2 . 0 0 0 0 0 - 0 . 0 4 9 7 0 - 4 . 0 0 0 0 0 - 0 . 1 1 2 0 0 0 . 0 0 8 6 4 2 . 0 0 0 0 0 - 0 . 0 5 0 1 0 -3 . 0 0 0 0 0 0 . 0 0 8 3 0 0 . 0 0 8 2 0 2 . 0 0 0 0 0 - 0 . 0 5 1 3 0 - 2 . 5 0 0 0 0 0 . 0 6 8 4 0 0 . 0 0 8 0 1 2 . 0 0 0 0 0 - 0 . 0 5 2 0 0 -2 . 0 0 0 0 0 0 . 1 2 8 7 0 0 . 0 0 7 8 4 2 . 0 0 0 0 0 - 0 . 0 5 2 8 0 - 1 . 5 0 0 0 0 0 . 1 8 8 9 0 0 . 0 0 7 6 4 2 . 0 0 0 0 0 - 0 . 0 5 3 5 0 - 1 . 0 0 0 0 0 0 . 2 4 9 0 0 0 . 0 0 7 3 8 2 . 0 0 0 0 0 - 0 . 0 5 4 4 0 - 0 . 5 0 0 0 0 0 . 3 0 8 8 0 0 . 0 0 6 9 5 2 . 0 0 0 0 0 - 0 . 0 5 5 4 0

0 . 0 0 0 0 0 0 . 3 6 7 7 0 0 . 0 0 6 1 1 2 . 0 0 0 0 0 - 0 . 0 5 6 6 0 0 . 5 0 0 0 0 0 . 4 2 7 8 0 0 . 0 0 5 7 9 2 . 0 0 0 0 0 - 0 . 0 5 7 6 0 1 . 0 0 0 0 . 4 8 8 1 0 . 0 0 5 6 4 2 . 0 0 0 0 0 - 0 . 0 5 8 5 1 . 5 0 0 0 . 5 4 8 2 0 . 0 0 5 6 6 2 . 0 0 0 0 0 - 0 . 0 5 9 3 2 . 0 0 0 0 . 6 0 7 8 0 . 0 0 5 6 5 2 . 0 0 0 0 0 - 0 . 0 6 0 0 2 . 50 0 0 . 6 6 7 5 0 . 0 0 5 7 1 2 . 0 0 0 0 0 - 0 . 0 6 0 7 3 . 0 0 0 0 . 7 2 7 2 0 . 0 0 5 8 1 2 . 0 0 0 0 0 - 0 . 0 6 1 5 3 . 5 0 0 0 . 7 8 6 8 0 . 0 0 5 9 0 2 . 0 0 0 0 0 - 0 . 0 62 2 4 . 0 0 0 0 . 8 4 6 0 0 . 0 0 6 0 1 2 . 0 0 0 0 0 - 0 . 0 62 9 4 . 5 0 0 0 . 9 0 4 8 0 . 0 0 6 1 6 2 . 0 0 0 0 0 - 0 . 0 6 3 6 5 . 0 0 0 0 . 9 6 3 0 0 . 0 0 6 2 8 2 . 0 0 0 0 0 - 0 . 0 6 4 2 5 . 5 0 0 l. 0 2 0 2 0 . 0 0 6 4 7 2 . 0 0 0 0 0 - 0 . 0 6 4 6 6 . 0 0 0 l. 0 7 5 6 0 . 0 0 6 6 5 2 . 0 0 0 0 0 - 0 . 0 6 4 6 7 . 0 0 0 1 . 1 9 3 7 0 . 0 0 7 3 1 2 . 0 0 0 0 0 - 0 . 0 6 6 6 7 . 5 0 0 1 . 2 5 0 8 0 . 0 0 7 8 1 2 . 0 0 0 0 0 - 0 . 0 67 5 8 . 0 0 0 1 . 3 0 5 4 0 . 0 0 8 5 1 2 . 0 0 0 0 0 - 0 . 0 6 8 0 8 . 5 0 0 l . 3 5 8 0 0 . 0 0 932 2 . 0 0 0 0 0 - 0 . 0 6 8 4 9 . 0 0 0 l . 4 0 4 2 0 . 0 1 0 6 4 2 . 0 0 0 0 0 - 0 . 0 6 8 1 9 . 5 0 0 l . 4 3 6 6 0 . 0 1 2 8 9 2 . 0 0 0 0 0 - 0 . 0 6 6 4

1 0 . 0 0 0 l. 4 5 8 8 0 . 0 1 5 1 9 2 . 0 0 0 0 0 - 0 . 0 6 3 7 1 0 . 5 0 0 l. 4 5 7 6 0 . 0 1 9 4 2 2 . 0 0 0 0 0 - 0 . 0 6 0 8 1 1 . 0 0 0 l . 4 6 5 2 0 . 02 3 6 6 2 . 0 0 0 0 0 - 0 . 0 5 9 3 1 1 . 5 0 0 l. 4 7 3 0 0 . 0 2 8 2 1 2 . 0 0 0 0 0 - 0 . 0 5 8 3 1 2 . 0 0 0 1 . 4 7 8 4 0 . 0 3 3 2 1 2 . 0 0 0 0 0 - 0 . 0 5 7 3 1 2 . 5 0 0 l . 4 9 0 7 0 . 0 3 7 6 6 2 . 0 0 0 0 0 - 0 . 0 5 6 7 1 3 . 0 0 0 1 . 4 9 3 4 0 . 0 4 3 2 6 2 . 0 0 0 0 0 - 0 . 0 5 6 1 1 3 . 5 0 0 l. 5 0 1 1 0 . 0 4 8 5 1 2 . 0 0 0 0 0 - 0 . 0 5 5 8 1 4 . 0 0 0 1 . 5 1 02 0 . 0 5 3 6 9 2 . 0 0 0 0 0 - 0 . 0 5 55 1 4 . 5 0 0 l. 5 1 3 6 0 . 0 5 9 6 7 2 . 0 0 0 0 0 - 0 . 0 55 5 1 5 . 0 0 0 1 . 5 1 7 9 0 . 0 6 5 7 9 2 . 0 0 0 0 0 - 0 . 0 5 5 7

9 . 0 0 0

S xtr ----- - -0 . 6 1 1 5 0 0 . 6 0 8 0 0 0 . 6 0 4 5 0 0 . 5 9 8 9 0 0 . 5 9 3 2 0 0 . 5 8 7 7 0 0 . 5 7 7 2 0 0 . 57 2 2 0 0 . 5 6 6 1 0 0 . 5 5 2 8 0 0 . 5 4 7 1 0 0 . 5 3 4 8 0 0 . 5 2 9 1 0 0 . 52 1 3 0 0 . 5 1 7 1 0 0 . 5 1 2 9 0 0 . 5 0 6 6 0 0 . 5 0 0 2 0 0 . 4 9 6 7 0 0 . 4 9 1 6 0 . 4 8 2 9 0 . 4 7 9 7 0 . 4 7 4 3 0 . 4 6 6 5 0 . 4 6 1 1 0 . 4 5 4 8 0 . 4 4 4 9 0 . 4 3 9 2 0 . 42 5 3 0 . 4 1 6 0 0 . 3 7 9 4 0 . 3 5 4 8 0 . 32 6 5 0 . 2 9 3 0 0 . 2 4 6 9 0 . 1 7 7 8 0 . 1 3 7 3 0 . 0 9 4 2 0 . 0 7 5 6 0 . 0 6 3 1 0 . 0 5 4 7 0 . 0 4 4 1 0 . 0 4 0 3 0 . 0 3 4 5 0 . 02 8 7 0 . 0 2 6 8 0 . 0 2 3 4

P xt r -------

0 . 0 0 7 6 0 0 . 0 0 7 7 0 0 . 0 0 7 8 0 0 . 0 0 8 0 0 0 . 0 0 9 6 0 0 . 0 1 1 2 0 0 . 0 1 2 2 0 0 . 0 1 3 0 0 0 . 0 1 3 4 0 0 . 0 1 8 5 0 0 . 0 2 2 5 0 0 . 0 3 1 4 0 0 . 0 3 9 1 0 0 . 0 5 5 9 0 0 . 0 8 8 2 0 0 . 1 4 4 0 0 0 . 2 6 3 3 0 0 . 5 3 5 4 0 0 . 6 5 8 8 0

0 . 7 4 6 5 0 . 7 8 7 8 0 . 8 2 7 5 0 . 8 4 9 8 0 . 8 6 6 0 0 . 8 8 1 3 0 . 8 9 5 7 0 . 9 0 7 8 0 . 9 2 3 7 0 . 9 4 0 2 0 . 9 5 9 8 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 l . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 l . 0 0 0 0 1 . 0 0 0 0 l . 0 0 0 0

POL . W1 52_20_9 ; 3

FFA TN 1 9 9 0 - 1 5 1 9

XFOI L Ve rsion 5 . 0

Calcu lated pola r for : FFA-W1 - 1 52

1 Reynolds numbe r fixed

xtrf • 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pre s sure ) Mach • 0 . 1 5 0

alpha CL ------- --------- 9 . 5 0 0 0 0 - 0 . 4 2 8 5 0 - 9 . 2 5 0 0 0 - 0 . 4 3 4 1 0 - 9 . 0 0 0 0 0 -o . 4 4 0 1 0 - 8 . 7 5 0 0 0 - 0 . 4 4 5 7 0 - 8 . 5 0 0 0 0 - 0 . 4 5 6 8 0 - 8 . 2 5 0 0 0 - 0 . 4 7 1 8 0 - 8 . 0 0 0 0 0 - 0 . 4 8 2 4 0 - 7 . 7 5 0 0 0 - 0 . 4 8 8 7 0 - 7 . 5 0 0 0 0 - 0 . 4 8 9 8 0 - 7 . 2 5 0 0 0 - 0 . 4 9 0 0 0 - 7 . 0 0 0 0 0 - 0 . 4 7 0 2 0 - 6 . 5 0 0 0 0 - 0 . 4 1 1 4 0 - 6 . 0 0 0 0 0 - 0 . 3 52 0 0 - 5 . 5 0 0 0 0 - 0 . 2 92 2 0 -4 . 5 0 0 0 0 - 0 . 1 7 3 1 0 - 4 . 0 0 0 0 0 - 0 . 1 1 3 5 0 - 3 . 5 0 0 -2 . 5 0 0 -2 . 0 0 0 - 1 . 5 0 0 - 1 . 0 0 0 - 0 . 5 0 0

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 50 0

- 0 . 0 5 2 5 0 . 0 6 8 3 0 . 1 2 8 5 0 . 1 8 9 0 0 . 2 4 92 0 . 3 0 9 5 0 . 3 6 8 6 0 . 4 2 8 4 0 . 4 8 8 6 0 . 5 4 8 8 0 . 6 0 8 9 0 . 6 6 8 9 0 . 7 2 8 8 0 . 7 8 8 7 0 . 8 4 8 5 0 . 9 0 7 7 0 . 9 6 6 7 1 . 0 2 5 1 1 . 0 8 2 8 1 . 1 3 8 8 1 . 1 9 1 9 1 . 2 4 8 5 1 . 3 0 2 4 1 . 3 5 2 1 1 . 3 9 6 6 1 . 4 3 0 3 1 . 4 4 5 4 1 . 4 6 1 6 1 . 4 8 2 1 1 . 4 9 0 9

Re ==

CD ---------

0 . 0 9 1 9 3 0 . 0 8 4 3 4 0 . 0 7 6 2 8 0 . 0 6 4 5 0 0 . 0 5 2 2 0 0 . 0 4 4 0 7 0 . 0 3 5 9 7 0 . 0 2 8 2 6 0 . 02 0 9 1 0 . 0 1 3 0 7 0 . 0 1 0 2 4 0 . 0 0 9 7 8 0 . 0 0 9 4 9 0 . 0 0 9 3 3 0 . 0 0 8 6 3 0 . 0 0 7 9 4

0 . 0 0 7 7 8 0 . 0 0 7 3 7 0 . 0 0 7 1 9 0 . 0 0 7 0 7 0 . 0 0 6 9 0 0 . 0 0 67 1 0 . 0 0 5 9 8 0 . 0 0 5 6 0 0 . 0 0 5 3 6 0 . 0 0 5 1 9 0 . 0 0 5 1 6 0 . 0 0 52 0 0 . 0 0 52 7 0 . 0 0 5 3 6 0 . 0 0 5 4 7 0 . 0 0 5 62 0 . 0 0 5 7 8 0 . 0 0 5 9 7 0 . 0 0 62 5 0 . 0 0 6 5 8 0 . 0 0 6 9 9 0 . 0 0 7 6 5 0 . 0 0 8 4 0 0 . 0 0 9 4 8 0 . 0 1 0 8 7 0 . 0 12 8 9 0 . 0 1 5 4 4 0 . 0 1 8 3 4 0 . 0 2 1 2 6 0 . 0 2 5 4 7

3 . 0 0 0 e 6 Ncrit = 9 . 0 0 0

Re (CL) CM S xt r P xt r - -------- -------- ------- - -- - ---

3 . 0 0 0 0 0 - 0 . 0 1 2 0 0 0 . 5 9 3 5 0 0 . 0 0 7 5 0 3 . 0 0 0 0 0 - 0 . 0 1 7 0 0 0 . 5 92 2 0 0 . 0 0 7 5 0 3 . 0 0 0 0 0 - 0 . 0 2 3 0 0 0 . 5 9 0 7 0 0 . 0 0 7 5 0 3 . 0 0 0 0 0 - 0 . 0 3 4 2 0 0 . 5 8 9 3 0 0 . 0 0 7 5 0 3 . 0 0 0 0 0 - 0 . 0 4 4 8 0 0 . 5 8 7 7 0 0 . 0 0 7 6 0 3 . 0 0 0 0 0 - 0 . 0 4 8 4 0 0 . 5 8 5 4 0 0 . 0 0 7 6 0 3 . 0 0 0 0 0 - 0 . 0 5 0 8 0 0 . 5 8 2 5 0 0 . 0 0 7 6 0 3 . 0 0 0 0 0 - 0 . 0 5 1 6 0 0 . 5 7 8 9 0 0 . 0 0 7 6 0 3 . 0 0 0 0 0 - 0 . 0 5 1 0 0 0 . 57 5 7 0 0 . 0 0 7 7 0 3 . 0 0 0 0 0 - 0 . 0 4 8 9 0 0 . 57 4 6 0 0 . 0 0 8 2 0 3 . 0 0 0 0 0 - 0 . 0 4 7 6 0 0 . 5 7 1 9 0 0 . 0 1 0 6 0 3 . 0 0 0 0 0 - 0 . 0 4 7 9 0 0 . 5 6 5 0 0 0 . 0 1 2 3 0 3 . 0 0 0 0 0 - 0 . 0 4 8 2 0 0 . 5 5 6 7 0 0 . 0 1 3 2 0 3 . 0 0 0 0 0 - 0 . 0 4 8 7 0 0 . 5 52 0 0 0 . 0 1 3 5 0 3 . 0 0 0 0 0 - 0 . 0 4 9 6 0 0 . 53 8 1 0 0 . 0 1 4 9 0 3 . 0 0 0 0 0 - 0 . 0 4 9 8 0 0 . 5 3 3 9 0 0 . 02 0 3 0 3 . 0 0 0 0 0 - 0 . 0 5 0 9 0 . 52 37 0 . 0 2 3 1 3 . 0 0 0 0 0 - 0 . 0 5 2 0 0 . 5 1 4 4 0 . 0 3 5 6 3 . 0 0 0 0 0 - 0 . 0 5 2 7 0 . 5 0 8 5 0 . 0 4 53 3 . 0 0 0 0 0 - 0 . 0 5 3 5 0 . 5 0 2 3 0 . 0 6 6 7 3 . 0 0 0 0 0 - 0 . 0 5 4 3 0 . 4 9 8 3 0 . 0 9 4 3 3 . 0 0 0 0 0 - 0 . 0 5 5 2 0 . 4 92 2 0 . 1 5 7 7 3 . 0 0 0 0 0 - 0 . 0 5 6 3 0 . 4 8 7 9 0 . 3 9 2 7 3 . 0 0 0 0 0 - 0 . 0 5 7 4 0 . 4 8 2 5 0 . 5 3 1 0 3 . 0 0 0 0 0 - 0 . 0 5 8 3 0 . 4 7 7 1 0 . 6 3 7 4 3 . 0 0 0 0 0 - 0 . 0 5 9 3 0 . 4 7 1 4 0 . 7 3 6 0 3 . 0 0 0 0 0 - 0 . 0 6 0 1 0 . 4 6 5 8 0 . 7 8 7 3 3 . 0 0 0 0 0 - 0 . 0 6 0 9 0 . 4 6 0 0 0 . 8 2 0 5 3 . 0 0 0 0 0 -o . 0 6 1 8 0 . 4 5 3 7 0 . 8 4 0 7 3 . 0 0 0 0 0 - 0 . 0 62 6 0 . 4 4 6 5 0 . 8 5 8 9 3 . 0 0 0 0 0 - 0 . 0 6 35 0 . 4 4 0 4 0 . 8 7 0 3 3 . 0 0 0 0 0 - 0 . 0 6 4 3 0 . 42 9 6 0 . 8 8 6 4 3 . 0 0 0 0 0 - 0 . 0 6 5 0 0 . 4 1 8 8 0 . 8 9 9 1 3 . 0 0 0 0 0 - 0 . 0 6 5 7 0 . 4 0 6 9 0 . 9 1 3 3 3 . 0 0 0 0 0 - 0 . 0 6 6 4 0 . 3 9 0 4 0 . 92 6 3 3 . 0 0 0 0 0 - 0 . 0 6 6 7 0 . 37 0 3 0 . 9 4 2 0 3 . 0 0 0 0 0 - 0 . 0 6 6 5 0 . 3 4 6 0 0 . 9 6 5 5 3 . 0 0 0 0 0 - 0 . 0 6 7 4 0 . 3 1 0 1 1 . 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 6 7 9 0 . 2 7 8 7 1 . 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 6 8 0 0 . 22 9 9 l. 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 6 7 5 0 . 1 7 8 7 l . 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 6 5 9 0 . 1 2 2 5 l. 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 62 5 0 . 0 8 7 6 1 . 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 6 0 5 0 . 0 7 1 2 l . 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 5 92 0 . 0 5 6 3 l. 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 5 7 9 0 . 0 4 9 8 1 . 0 0 0 0

POL . W1 52_30_9 ; 5

FFA TN 1 9 9 0 - 1 5 2 0 POL . W152_30_TU1 ; 3

XFOIL Vers ion 5 . 0

Calculated polar for : FFA-W1 - 1 5 2

1 Reynolds number fixed

xt rf • 0 . 0 1 0 ( suction ) 0 . 1 0 0 (pre s sure ) Mach • 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re ( CL ) CM S xt r P xt r ------- -------- --------- --- - - --- - -------- ------- --- - ---- 3 . 5 0 0 - 0 . 0 5 7 7 0 . 0 1 0 0 6 3 . 0 0 0 0 0 - 0 . 0 5 1 3 0 . 0 1 0 0 0 . 0 2 3 9 - 3 . 0 0 0 0 . 0 0 1 7 0 . 0 0 9 9 9 3 . 0 0 0 0 0 - 0 . 0 5 1 9 0 . 0 1 0 0 0 . 0 2 6 0 -2 . 5 0 0 0 . 0 6 1 4 0 . 0 0 9 9 4 3 . 0 0 0 0 0 - 0 . 0 5 2 5 0 . 0 1 0 0 0 . 0 3 6 0 - 2 . 0 0 0 0 . 1 2 0 7 0 . 0 0 9 8 8 3 . 0 0 0 0 0 - 0 . 0 5 3 1 0 . 0 1 0 0 0 . 0 4 6 3 - 1 . 5 0 0 0 . 1 8 0 0 0 . 0 0 9 8 4 3 . 0 0 0 0 0 - 0 . 0 5 3 8 0 . 0 1 0 0 0 . 0 6 62 - 1 . 0 0 0 0 . 2 3 9 3 0 . 0 0 9 8 4 3 . 0 0 0 0 0 - 0 . 0 5 4 5 0 . 0 1 0 0 0 . 0 9 8 9 - 0 . 5 0 0 0 . 2 9 8 7 0 . 0 0 9 9 6 3 . 0 0 0 0 0 - 0 . 0 5 5 2 0 . 0 1 0 0 0 . 1 0 0 0

0 . 0 0 0 0 . 3 5 7 9 0 . 0 1 0 1 0 3 . 0 0 0 0 0 - 0 . 0 5 5 9 0 . 0 1 0 0 0 . 1 0 0 0 0 . 5 0 0 0 . 4 1 6 8 0 . 0 1 0 2 6 3 . 0 0 0 0 0 - 0 . 0 5 6 6 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 . 4 7 5 5 0 . 0 1 0 4 4 3 . 0 0 0 0 0 - 0 . 0 5 7 3 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 5 3 4 0 0 . 0 1 0 6 4 3 . 0 0 0 0 0 - 0 . 0 5 7 9 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 5 9 2 1 0 . 0 1 0 8 6 3 . 0 0 0 0 0 - 0 . 0 5 8 6 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 6 4 9 9 0 . 0 1 1 1 0 3 . 0 0 0 0 0 - 0 . 0 5 9 3 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 7 0 7 3 0 . 0 1 1 3 6 3 . 0 0 0 0 0 - 0 . 0 5 9 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 7 6 4 2 0 . 0 1 1 6 6 3 . 0 0 0 0 0 - 0 . 0 6 0 4 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 8 2 0 5 0 . 0 1 1 9 8 3 . 0 0 0 0 0 - 0 . 0 6 1 0 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 8 7 6 3 0 . 0 1 2 3 3 3 . 0 0 0 0 0 - 0 . 0 6 1 4 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 9 3 1 3 0 . 0 1 2 7 2 3 . 0 0 0 0 0 - 0 . 0 6 1 8 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 9 8 5 4 0 . 0 1 3 1 5 3 . 0 0 0 0 0 - 0 . 0 62 1 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 1 . 0 3 8 5 0 . 0 1 3 6 2 3 . 0 0 0 0 0 - 0 . 0 62 3 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 0 9 0 3 0 . 0 1 4 1 5 3 . 0 0 0 0 0 - 0 . 0 62 4 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 1 4 0 5 0 . 0 1 4 7 5 3 . 0 0 0 0 0 - 0 . 0 622 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1 8 8 5 0 . 0 1 5 4 2 3 . 0 0 0 0 0 - 0 . 0 6 1 9 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 2 3 0 0 0 . 0 1 62 5 3 . 0 0 0 0 0 - 0 . 0 6 0 7 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 2 6 0 4 0 . 0 1 7 6 3 3 . 0 0 0 0 0 - 0 . 0 5 8 8 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 2 9 1 7 0 . 0 1 9 4 0 3 . 0 0 0 0 0 - 0 . 0 57 7 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 3 1 9 4 0 . 0 2 1 5 8 3 . 0 0 0 0 0 - 0 . 0 5 6 7 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 3 4 4 8 0 . 0 2 4 1 5 3 . 0 0 0 0 0 - 0 . 0 5 5 9 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 3 6 7 5 0 . 0 2 7 1 0 3 . 0 0 0 0 0 - 0 . 0 5 5 1 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 3 8 8 9 0 . 0 3 0 3 4 3 . 0 0 0 0 0 - 0 . 0 5 4 4 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 4 0 8 0 0 . 0 3 3 8 3 3 . 0 0 0 0 0 - 0 . 0 5 3 7 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 21 POL . W1 52_8 0_9 ; 2

XFOIL Ve rs ion 5 . 0

Calculated polar for : FFA-W1 - 1 52

1 Reynolds number fixed

xtrf • 1 . 0 0 0 ( suction) 1 . 0 0 0 (pressure ) Mach .. 0 . 1 5 0 Re ... 8 . 0 0 0 e 6 Ncrit = 9 . 0 0 0

al.pha CL CD Re ( CL ) CM S xt r P xtr - - - - - - - -------- --------- --------- -------- ------- -------

2 . 0 0 0 0 . 6 1 2 6 0 . 0 0 4 8 3 8 . 0 0 0 0 0 - 0 . 0 6 0 3 0 . 4 3 8 5 0 . 5 1 4 9 2 . 50 0 0 . 6 7 2 7 0 . 0 0 4 4 8 8 . 0 0 0 0 0 - 0 . 0 6 1 4 0 . 4 2 9 7 0 . 6 9 7 1 3 . 0 0 0 0 . 7 3 3 1 0 . 0 0 4 4 8 8 . 0 0 0 0 0 - 0 . 0 62 5 0 . 4 1 92 0 . 7 5 3 3 3 . 5 0 0 0 . 7 9 3 5 0 . 0 0 4 5 5 8 . 0 0 0 0 0 - 0 . 0 6 35 0 . 4 0 9 0 0 . 7 8 4 6 4 . 0 0 0 0 . 8 5 3 7 0 . 0 0 4 6 7 8 . 0 0 0 0 0 - 0 . 0 6 4 5 0 . 3 9 6 9 0 . 8 1 0 1 4 . 5 0 0 0 . 9 1 3 6 0 . 0 0 4 8 5 8 . 0 0 0 0 0 - 0 . 0 6 5 5 0 . 3 8 2 8 0 . 8 2 5 8 5 . 0 0 0 0 . 9 7 2 7 0 . 0 0 5 1 4 8 . 0 0 0 0 0 - 0 . 0 6 6 4 0 . 3 5 8 9 0 . 8 3 9 6 5 . 5 0 0 1 . 0 3 1 5 0 . 0 0 5 4 5 8 . 0 0 0 0 0 - 0 . 0 6 7 3 0 . 3 3 7 8 0 . 8 5 3 6 6 . 0 0 0 1 . 0 9 0 4 0 . 0 0 5 7 0 8 . 0 0 0 0 0 - 0 . 0 6 8 2 0 . 32 2 5 0 . 8 6 5 6 6 . 5 0 0 1 . 1 4 7 0 0 . 0 0 6 2 5 8 . 0 0 0 0 0 - 0 . 0 6 8 9 0 . 2 8 6 1 0 . 8 8 2 9 7 . 0 0 0 1 . 1 9 9 5 0 . 0 0 7 2 7 8 . 0 0 0 0 0 - 0 . 0 6 92 0 . 2 1 9 8 0 . 8 9 1 6 7 . 5 0 0 1 . 2 5 3 0 0 . 0 0 8 0 0 8 . 0 0 0 0 0 - 0 . 0 6 9 5 0 . 1 8 0 2 0 . 9 1 0 3 8 . 0 0 0 1 . 3 0 4 6 0 . 0 0 8 8 2 8 . 0 0 0 0 0 - 0 . 0 6 9 6 0 . 1 4 6 3 0 . 92 6 5 8 . 5 0 0 1 . 3 5 1 2 0 . 0 0 9 9 0 8 . 0 0 0 0 0 - 0 . 0 6 9 0 0 . 0 9 9 7 0 . 9 5 2 5 9 . 0 0 0 1 . 3 9 8 8 0 . 0 1 0 6 5 8 . 0 0 0 0 0 - 0 . 0 6 8 3 0 . 0 7 7 6 1 . 0 0 0 0 9 . 5 0 0 1 . 4 4 3 6 0 . 0 1 1 8 1 8 . 0 0 0 0 0 - 0 . 0 6 7 7 0 . 0 5 3 7 1 . 0 0 0 0

1 0 . 0 0 0 1 . 4 8 6 0 0 . 0 1 2 9 6 8 . 0 0 0 0 0 - 0 . 0 6 6 8 0 . 0 4 52 1 . 0 0 0 0 1 0 . 5 0 0 1 . 5 2 1 7 0 . 0 1 4 0 4 8 . 0 0 0 0 0 - 0 . 0 6 5 1 0 . 0 3 7 2 1 . 0 0 0 0 1 1 . 0 0 0 1 . 5 4 52 0 . 0 1 6 0 7 8 . 0 0 0 0 0 - 0 . 0 6 2 9 0 . 0 3 2 2 1 . 0 0 0 0 1 1 . 5 0 0 1 . 5 6 1 2 0 . 0 1 9 0 4 8 . 0 0 0 0 0 - 0 . 0 6 1 0 0 . 02 8 1 1 . 0 0 0 0 1 2 . 0 0 0 1 . 5 8 1 9 0 . 0 2 1 9 8 8 . 0 0 0 0 0 - 0 . 0 5 9 8 0 . 02 3 9 1 . 0 0 0 0 1 2 . 5 0 0 1 . 6 0 1 4 0 . 0 2 5 1 5 8 . 0 0 0 0 0 - 0 . 0 5 8 8 0 . 0 2 0 3 1 . 0 0 0 0 1 3 . 0 0 0 1 . 6 1 9 7 0 . 0 2 8 6 4 8 . 0 0 0 0 0 - 0 . 0 5 7 9 0 . 0 1 7 3 1 . 0 0 0 0 1 3 . 5 0 0 1 . 622 4 0 . 0 3 3 6 8 8 . 0 0 0 0 0 - 0 . 0 5 6 7 0 . 0 1 6 0 1 . 0 0 0 0

FFA TN 1 9 9 0 - 1 5 2 2

XFOI L Vers ion 5 . 0

Calculated polar fo r : FFA-W1 - 1 5 2

1 Reynolds numbe r fixed

xt rf- '"' 0 . 0 1 0 ( suction ) 0 . 1 0 0 (pressure ) Mach ""

alpha - - - -- --

2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 2 5 0 1 2 . 5 0 0 1 2 . 7 5 0 1 3 . 0 0 0

0 . 1 5 0

CL --------

0 . 5 9 8 6 0 . 6 5 7 4 0 . 7 1 5 9 0 . 7 7 4 1 0 . 8 3 1 8 0 . 8 8 92 0 . 9 4 6 1 1 . 0 0 2 4 1 . 0 5 8 1 1 . 1 1 3 0 1 . 1 6 7 0 1 . 2 1 9 9 1 . 2 7 1 5 1 . 32 1 5 1 . 3 6 9 0 1 . 4 0 2 7 1 . 4 3 4 3 1 . 4 62 8 1 . 4 8 9 0 1 . 5 11 6 1. 5 3 3 0 1 . 5 4 2 8 1 . 5 5 0 8 1 . 5 6 0 1 1 . 5 6 7 5

Re = 8 . 0 0 0 e 6 Ncr it

CD Re (CL) CM --------- --------- --------

0 . 0 0 9 1 8 8 . 0 0 0 0 0 - 0 . 0 5 9 2 0 . 0 0 9 3 8 8 . 0 0 0 0 0 - 0 . 0 6 0 0 0 . 0 0 9 5 9 8 . 0 0 0 0 0 - 0 . 0 6 0 7 0 . 0 0 9 8 2 8 . 0 0 0 0 0 - 0 . 0 6 1 4 0 . 0 1 0 0 8 8 . 0 0 0 0 0 - 0 . 0 62 1 0 . 0 1 0 3 6 8 . 0 0 0 0 0 - 0 . 0 62 8 0 . 0 1 0 6 6 8 . 0 0 0 0 0 - 0 . 0 6 3 4 0 . 0 1 0 9 8 8 . 0 0 0 0 0 - 0 . 0 6 3 9 0 . 0 1 1 3 4 8 . 0 0 0 0 0 - 0 . 0 6 4 4 0 . 0 1 1 7 3 8 . 0 0 0 0 0 - 0 . 0 6 4 8 0 . 0 12 1 5 8 . 0 0 0 0 0 - 0 . 0 6 5 1 0 . 0 1 2 6 2 8 . 0 0 0 0 0 - 0 . 0 6 52 0 . 0 1 3 1 4 8 . 0 0 0 0 0 - 0 . 0 6 53 0 . 0 1 372 8 . 0 0 0 0 0 - 0 . 0 6 5 1 0 . 0 1 4 3 8 8 . 0 0 0 0 0 - 0 . 0 6 4 6 0 . 0 1 52 9 8 . 0 0 0 0 0 - 0 . 0 62 3 0 . 0 1 6 7 4 8 . 0 0 0 0 0 - 0 . 0 6 0 7 0 . 0 1 8 6 1 8 . 0 0 0 0 0 - 0 . 0 5 9 3 0 . 0 2 0 8 6 8 . 0 0 0 0 0 - 0 . 0 5 8 1 0 . 0 2 3 5 8 8 . 0 0 0 0 0 - 0 . 0 5 7 0 0 . 0 2 6 5 9 8 . 0 0 0 0 0 - 0 . 0 5 6 1 0 . 0 2 8 2 4 8 . 0 0 0 0 0 - 0 . 0557 0 . 0 3 0 0 8 8 . 0 0 0 0 0 - 0 . 0 5 53 0 . 0 3 1 7 5 8 . 0 0 0 0 0 - 0 . 0 5 4 8 0 . 0 3 3 7 5 8 . 0 0 0 0 0 - 0 . 0 5 4 4

POL . W1 52_8 0_TU1 ; 2

9 . 0 0 0

s xt r P xt r ------- - ------0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 · 2 3 POL . W182_1 0_9 ; 5

XFOI L Version 5 . 0

Ca l culated polar for : FFA-W1 - 1 8 2

1 Reynolds number fixed

xt rf - 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pre s sure ) Mach - 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncrit = 9 . 0 0 0

alpha CL CD Re (CL) CM s xtr P xtr --- - --- -------- --------- --------- -------- ------- --- ----- 7 . 5 0 0 0 0 - 0 . 5 1 7 9 0 0 . 0 2 1 2 3 1 . 0 0 0 0 0 - 0 . 0 4 6 8 0 0 . 6 0 8 7 0 0 . 0 1 0 5 0 -7 . 0 0 0 0 0 - 0 . 5 0 0 2 0 0 . 0 1 4 8 1 1 . 0 0 0 0 0 - 0 . 0 4 5 8 0 0 . 5 9 9 0 0 0 . 0 1 3 1 0 - 6 . 5 0 0 0 0 - o . 4.4 5 3 0 0 . 0 1 3 6 8 1 . 0 0 0 0 0 - 0 . 0 4 6 4 0 0 . 5 8 9 5 0 0 . 0 1 4 5 0 - 6 . 0 0 0 0 0 - 0 . 3 8 8 0 0 0 . 0 1 2 9 3 1 . 0 0 0 0 0 - 0 . 0 4 7 2 0 0 . 57 9 6 0 0 . 0 1 5 7 0 - 5 . 5 0 0 0 0 - 0 . 32 95 0 0 . 0 1 2 3 7 1 . 0 0 0 0 0 - 0 . 0 4 8 0 0 0 . 5 7 2 0 0 0 . 0 1 6 7 0 - 5 . 0 0 0 0 0 - 0 . 2 7 0 2 0 0 . 0 1 1 9 7 1 . 0 0 0 0 0 - 0 . 0 4 8 9 0 0 . 5 6 2 1 0 0 . 0 1 7 4 0 - 4 . 5 0 0 0 0 - 0 . 2 1 0 7 0 0 . 0 1 1 0 3 1 . 0 0 0 0 0 - 0 . 0 4 9 7 0 0 . 5 5 6 1 0 0 . 02 5 4 0 - 4 . 0 0 0 0 0 - 0 . 1 5 0 3 0 0 . 0 1 0 6 6 1 . 0 0 0 0 0 - 0 . 0 5 0 7 0 0 . 5 4 7 6 0 0 . 0 3 3 5 0 - 3 . 5 0 0 0 0 - 0 . 0 8 9 8 0 0 . 0 1 0 3 0 1 . 0 0 0 0 0 - 0 . 0 5 1 7 0 0 . 5 4 0 4 0 0 . 0 5 5 8 0 - 3 . 0 0 0 0 0 - 0 . 0 3 0 9 0 0 . 0 0 8 4 9 1 . 0 0 0 0 0 - 0 . 0 5 4 0 0 0 . 5 3 4 6 0 0 . 32 4 0 0 -2 . 5 0 0 0 0 0 . 0 2 9 5 0 0 . 0 0 7 7 4 1. 0 0 0 0 0 - 0 . 0 5 5 5 0 0 . 52 5 6 0 0 . 4 6 1 4 0 -2 . 0 0 0 0 0 0 . 0 9 0 7 0 0 . 0 0 7 5 0 1 . 0 0 0 0 0 - 0 . 0 5 6 6 0 0 . 52 0 7 0 0 . 52 6 6 0 - 1 . 5 0 0 0 0 0 . 1 5 1 8 0 0 . 0 0 7 4 7 1 . 0 0 0 0 0 - 0 . 0 5 7 5 0 0 . 5 1 5 4 0 0 . 5 7 1 4 0 - 1 . 0 0 0 0 0 0 . 2 1 3 0 0 0 . 0 0 7 5 4 1 . 0 0 0 0 0 - 0 . 0 5 8 5 0 0 . 5 0 7 3 0 0 . 5 8 1 8 0 - 0 . 5 0 0 0 0 0 . 2 7 4 3 0 0 . 0 0 7 6 0 1 . 0 0 0 0 0 - 0 . 0 5 9 4 0 0 . 5 0 2 4 0 0 . 5 9 2 7 0

0 . 0 0 0 0 0 0 . 3 3 5 4 0 0 . 0 0 7 6 6 1 . 0 0 0 0 0 - 0 . 0 6 0 4 0 0 . 4 9 7 9 0 0 . 6 0 3 0 0 0 . 5 0 0 0 0 0 . 3 9 6 4 0 0 . 0 0 7 7 6 1 . 0 0 0 0 0 - 0 . 0 6 1 4 0 0 . 4 9 0 6 0 0 . 6 1 1 2 0 1 . 0 0 0 0 . 4 5 7 1 0 . 0 0 7 8 8 1 . 0 0 0 0 0 - 0 . 0 62 3 0 . 4 8 4 9 0 . 6 1 9 4 1 . 5 0 0 0 . 5 1 8 0 0 . 0 0 7 9 7 1 . 0 0 0 0 0 - 0 . 0 6 3 3 0 . 4 8 1 0 0 . 62 7 8 2 . 0 0 0 0 . 5 7 8 5 0 . 0 0 8 0 9 1 . 0 0 0 0 0 - 0 . 0 6 4 2 0 . 4 7 5 5 0 . 6 3 4 1 2 . 50 0 0 . 6 3 8 7 0 . 0 0 8 2 5 1 . 0 0 0 0 0 - 0 . 0 6 5 1 0 . 4 6 7 4 0 . 6 4 2 5 3 . 0 0 0 0 . 6 9 9 0 0 . 0 0 8 3 8 1 . 0 0 0 0 0 - 0 . 0 6 6 0 0 . 4 6 3 8 0 . 6 4 9 1 3 . 5 0 0 0 . 7 5 9 1 0 . 0 0 8 5 1 1 . 0 0 0 0 0 - 0 . 0 6 6 9 0 . 4 5 9 0 0 . 6 5 4 2 4 . 0 0 0 0 . 8 1 8 8 0 . 0 0 8 6 8 1 . 0 0 0 0 0 - 0 . 0 6 7 8 0 . 4 5 1 2 0 . 6 62 8 4 . 5 0 0 0 . 8 7 8 3 0 . 0 0 8 8 6 1 . 0 0 0 0 0 - 0 . 0 6 8 6 0 . 4 4 5 6 0 . 6 6 8 7 5 . 0 0 0 0 . 9 3 7 8 0 . 0 0 9 0 2 1 . 0 0 0 0 0 - 0 . 0 6 9 4 0 . 4 4 0 5 0 . 6 7 3 5 5 . 5 0 0 0 . 9 9 6 8 0 . 0 0 9 2 3 1 . 0 0 0 0 0 - 0 . 0 7 0 2 0 . 4 32 0 0 . 6 8 1 9 6 . 0 0 0 1 . 0 5 5 6 0 . 0 0 9 4 3 1 . 0 0 0 0 0 - 0 . 0 7 1 0 0 . 4 2 4 9 0 . 6 8 7 7 6 . 5 0 0 1 . 1 1 4 0 0 . 0 0 9 6 7 1 . 0 0 0 0 0 - 0 . 0 7 1 6 0 . 4 1 6 6 0 . 6 9 2 9 7 . 0 0 0 1 . 1 7 1 9 0 . 0 0 9 9 2 1 . 0 0 0 0 0 - 0 . 0 7 2 3 0 . 4 0 5 5 0 . 7 0 0 9 7 . 5 0 0 1 . 2 2 8 8 0 . 0 1 0 2 7 1 . 0 0 0 0 0 -o . 0 7 2 8 0 . 3 8 9 7 0 . 7 0 6 9 8 . 0 0 0 1 . 2 8 4 5 0 . 0 1 0 7 0 1 . 0 0 0 0 0 - 0 . 0 7 32 0 . 3 7 1 8 0 . 7 1 2 3 8 . 5 0 0 1 . 3 3 8 1 0 . 0 1 1 2 8 1 . 0 0 0 0 0 - 0 . 0 7 3 3 0 . 3 4 9 1 0 . 7 2 0 8 9 . 0 0 0 1 . 3 8 6 3 0 . 0 1 2 2 4 1 . 0 0 0 0 0 - o . 0 7 2 8 0 . 3 1 2 5 0 . 7 2 7 2 9 . 5 0 0 1 . 4 2 8 9 0 . 0 1 35 2 1 . 0 0 0 0 0 - 0 . 0 7 1 7 0 . 2 7 3 5 0 . 7 3 3 8

1 0 . 0 0 0 1 . 4 6 0 5 0 . 0 1 5 3 8 1 . 0 0 0 0 0 - 0 . 0 6 9 5 0 . 2 2 8 4 0 . 7 4 2 8 1 1 . 0 0 0 1 . 4 5 9 7 0 . 0 2 2 9 0 1 . 0 0 0 0 0 - 0 . 0 6 1 5 0 . 1 4 4 9 0 . 7 6 1 1 1 1 . 50 0 1 . 4 5 32 0 . 0 2 8 6 1 1 . 0 0 0 0 0 - 0 . 0 6 0 1 0 . 1 2 1 6 0 . 7 7 0 2 1 2 . 0 0 0 1 . 4 4 5 2 0 . 0 3 5 1 1 1 . 0 0 0 0 0 - 0 . 0 5 9 4 0 . 0 9 9 5 0 . 7 8 3 3 1 2 . 5 0 0 1 . 4 3 8 4 0 . 0 4 1 9 0 1 . 0 0 0 0 0 - 0 . 0 5 92 0 . 0 8 1 7 0 . 7 9 7 0 1 3 . 0 0 0 1 . 4 3 3 7 0 . 0 4 8 6 8 1 . 0 0 0 0 0 - 0 . 0 5 9 1 0 . 0 6 8 6 0 . 8 1 4 4 1 3 . 5 0 0 1 . 4 3 3 7 0 . 0 5 5 1 0 1 . 0 0 0 0 0 - 0 . 0 5 9 3 0 . 0 5 6 6 0 . 8 5 1 9 1 4 . 0 0 0 1 . 4 3 1 2 0 . 0 6 1 3 8 1 . 0 0 0 0 0 - 0 . 0 5 9 0 0 . 0 5 0 0 1 . 0 0 0 0 1 4 . 5 0 0 1 . 4 3 5 1 0 . 0 6 7 7 9 1 . 0 0 0 0 0 - 0 . 0 5 9 5 0 . 0 4 2 0 1 . 0 0 0 0 1 5 . 0 0 0 1 . 4 3 4 5 0 . 0 7 4 8 7 1 . 0 0 0 0 0 - 0 . 0 6 0 3 0 . 0 3 8 5 1 . 0 0 0 0 1 5 . 5 0 0 1 . 4 3 8 2 0 . 0 8 1 6 7 1 . 0 0 0 0 0 - 0 . 0 6 12 0 . 0 3 3 5 1 . 0 0 0 0 1 6 . 0 0 0 1 . 4 4 0 6 0 . 0 8 8 8 5 1 . 0 0 0 0 0 - 0 . 0 62 4 0 . 02 8 8 1 . 0 0 0 0 1 6 . 5 0 0 1 . 4 4 5 9 0 . 0 95 6 3 1 . 0 0 0 0 0 - 0 . 0 6 3 6 0 . 0 2 7 7 1 . 0 0 0 0 1 7 . 0 0 0 1 . 4 4 7 9 0 . 1 0 3 2 6 1 . 0 0 0 0 0 - 0 . 0 6 5 1 0 . 02 62 1 . 0 0 0 0 1 7 . 5 0 0 1 . 4 4 8 5 0 . 1 1 1 3 7 1 . 0 0 0 0 0 - 0 . 0 6 7 0 0 . 0 2 3 8 1 . 0 0 0 0

FFA TN 1 9 9 0 - 1 5 2 4 POL . W 1 8 2_1 0_TU1 ; 2

XFOI L Ve rsion 5 . 0

Ca lculated polar for : FFA-W1- 1 8 2

1 Reynolds number fixed

xt rf • 0 . 0 1 0 ( suct ion ) 0 . 1 0 0 (pressure ) Mach = 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it 9 . 0 0 0

alpha CL CD Re (CL) CM S xt r P xt r - - - - - -- -------- ------ --- --------- -------- ------- -------

1 . 0 0 0 0 . 4 3 4 1 0 . 0 1 32 0 1 . 0 0 0 0 0 - 0 . 0 5 9 0 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 4 92 1 0 . 0 1 3 42 1 . 0 0 0 0 0 - 0 . 0 5 9 8 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 5 4 9 7 0 . 0 1 3 6 7 1 . 0 0 0 0 0 - 0 . 0 6 0 4 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 6 0 6 9 0 . 0 1 3 9 5 1 . 0 0 0 0 0 - 0 . 0 6 1 1 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 6 3 4 0 . 0 1 4 2 7 1 . 0 0 0 0 0 - 0 . 0 6 1 6 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 7 1 9 3 0 . 0 1 4 62 1 . 0 0 0 0 0 - 0 . 0 62 1 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 7 7 4 4 0 . 0 1 5 0 2 1 . 0 0 0 0 0 - 0 . 0 62 5 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 8 2 8 6 0 . 0 1 5 4 6 1 . 0 0 0 0 0 - 0 . 0 62 8 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 8 8 1 7 0 . 0 1 5 9 6 1 . 0 0 0 0 0 - 0 . 0 6 2 9 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 9 3 3 4 0 . 0 1 6 5 2 1 . 0 0 0 0 0 - 0 . 0 6 3 0 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 9 8 3 4 0 . 0 1 7 1 6 1 . 0 0 0 0 0 - 0 . 0 62 8 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 0 3 1 3 0 . 0 1 7 8 9 1 . 0 0 0 0 0 - 0 . 0 62 4 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 0 7 5 0 0 . 0 1 8 7 3 1 . 0 0 0 0 0 - 0 . 0 6 1 5 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1 0 5 4 0 . 0 1 9 9 4 1 . 0 0 0 0 0 - 0 . 0 5 9 1 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 1 3 7 8 0 . 0 2 1 6 5 1 . 0 0 0 0 0 - 0 . 0 5 8 1 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 1 6 6 5 0 . 0 2 3 8 6 1 . 0 0 0 0 0 - 0 . 0 5 7 3 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 1 92 3 0 . 0 2 6 5 5 1 . 0 0 0 0 0 - 0 . 0 5 6 7 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1. 2 1 5 5 0 . 0 2 9 7 0 1 . 0 0 0 0 0 - 0 . 0 5 6 4 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 2 3 6 1 0 . 0 3 32 8 1 . 0 0 0 0 0 - 0 . 0 5 6 3 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 2 5 4 6 0 . 0 3 7 2 5 1 . 0 0 0 0 0 - 0 . 0 5 62 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 2 7 1 5 0 . 0 4 1 4 8 1 . 0 0 0 0 0 - 0 . 0 5 62 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1. 2 8 6 7 0 . 0 4 6 0 2 1 . 0 0 0 0 0 - 0 . 0 5 6 3 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 3 0 1 1 0 . 0 5 0 7 6 1 . 0 0 0 0 0 - 0 . 0 5 6 5 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 3 1 4 2 0 . 0 5 5 6 9 1 . 0 0 0 0 0 - 0 . 0 5 6 7 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 32 6 7 0 . 0 6 0 8 4 1 . 0 0 0 0 0 - 0 . 0 5 71 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 3 3 8 1 0 . 0 6 6 2 2 1 . 0 0 0 0 0 - 0 . 0 5 7 6 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 3 4 8 9 0 . 0 7 1 7 5 1 . 0 0 0 0 0 - 0 . 0 5 8 1 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 3 5 9 7 0 . 0 7 7 4 1 1 . 0 0 0 0 0 - 0 . 0 5 8 8 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 3 6 9 5 0 . 0 8 3 4 5 1 . 0 0 0 0 0 - 0 . 0 5 9 8 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 2 5 POL . W1 82_2 0_9 ; 3

XFOIL Ve rsion 5 . 0

Calculated polar for : FFA-W1 - 1 8 2

1 Reynolds number f ixed

xtrf .. 1 . 0 0 0 ( suction ) 1 . 0 0 0 (pres sure ) Mach • 0 . 1 5 0 Re = 2 . 0 0 0 e 6 Ncr it 9 . 0 0 0

alpha CL CD Re (CL) CM S xtr P xt r - - - ---- -------- --------- --------- -------- ------- -------

- 1 0 . 0 0 0 0 0 - 0 . 7 7 1 2 0 0 . 0 2 3 9 3 2 . 0 0 0 0 0 - 0 . 0 42 4 0 0 . 6 3 02 0 0 . 0 0 8 0 0 - 9 . 5 0 0 0 0 - 0 . 7 4 9 9 0 0 . 0 2 0 5 9 2 . 0 0 0 0 0 - 0 . 0 4 3 3 0 0 . 6 1 7 6 0 0 . 0 0 8 3 0 - 9 . 0 0 0 0 0 - 0 . 7 0 6 5 0 0 . 0 1 8 6 6 2 . 0 0 0 0 0 - 0 . 0 4 4 4 0 0 . 6 0 6 3 0 0 . 0 0 8 7 0 - 6 . 5 0 0 0 0 - 0 . 4 5 0 7 0 0 . 0 1 1 4 3 2 . 0 0 0 0 0 - 0 . 0 4 6 7 0 0 . 55 9 1 0 0 . 0 1 1 8 0 - 6 . 0 0 0 0 0 - 0 . 3 9 1 9 0 0 . 0 1 0 6 3 2 . 0 0 0 0 0 - 0 . 0 4 7 4 0 0 . 5 5 1 1 0 0 . 0 1 3 6 0 - 5 . 5 0 0 0 0 - 0 . 3 3 1 9 0 0 . 0 1 0 1 7 2 . 0 0 0 0 0 - 0 . 0 4 8 3 0 0 . 5 4 2 5 0 0 . 0 1 52 0 - 5 . 0 0 0 0 0 - o . 2 7 1 5 0 0 . 0 0 9 8 3 2 . 0 0 0 0 0 - 0 . 0 4 9 2 0 0 . 5 3 7 2 0 0 . 0 1 6 5 0 - 4 . 0 0 0 0 0 - 0 . 1 4 9 8 0 0 . 0 0 92 0 2 . 0 0 0 0 0 - 0 . 0 5 1 1 0 0 . 52 2 1 0 0 . 0 2 5 1 0 - 3 . 5 0 0 0 0 - 0 . 0 8 8 7 0 0 . 0 0 8 9 6 2 . 0 0 0 0 0 - 0 . 0 52 1 0 0 . 5 1 6 9 0 0 . 0 32 7 0 - 3 . 0 0 0 0 0 - 0 . 0 2 7 7 0 0 . 0 0 8 5 7 2 . 0 0 0 0 0 - 0 . 0 5 3 2 0 0 . 5 0 7 4 0 0 . 0 7 5 6 0 - 2 . 5 0 0 0 0 0 . 0 3 2 7 0 0 . 0 0 7 0 7 2 . 0 0 0 0 0 - 0 . 0 5 5 4 0 0 . 5 0 3 4 0 0 . 32 5 2 0 -2 . 0 0 0 0 0 0 . 0 9 3 9 0 0 . 0 0 6 4 9 2 . 0 0 0 0 0 - 0 . 0 5 6 8 0 0 . 4 9 9 0 0 0 . 4 4 0 7 0 - 1 . 5 0 0 0 0 0 . 1 5 5 3 0 0 . 0 0 62 6 2 . 0 0 0 0 0 - 0 . 0 5 8 0 0 0 . 4 9 1 1 0 0 . 5 0 0 5 0 - 1 . 0 0 0 0 0 0 . 2 1 6 8 0 0 . 0 0 6 1 6 2 . 0 0 0 0 0 - 0 . 0 5 9 1 0 0 . 4 8 5 6 0 0 . 5 4 6 0 0 - 0 . 5 0 0 0 0 0 . 2 7 8 4 0 0 . 0 0 6 1 6 2 . 0 0 0 0 0 - 0 . 0 6 0 1 0 0 . 4 8 2 1 0 0 . 5 6 4 0 0

0 . 0 0 0 0 0 0 . 3 4 0 0 0 0 . 0 0 62 0 2 . 0 0 0 0 0 - 0 . 0 6 1 2 0 0 . 4 7 6 3 0 0 . 5 7 5 0 0 0 . 5 0 0 0 0 0 . 4 0 1 5 0 0 . 0 0 62 7 2 . 0 0 0 0 0 - 0 . 0 62 2 0 0 . 4 6 8 7 0 0 . 5 8 4 9 0 1. 0 0 0 0 . 4 62 9 0 . 0 0 6 3 2 2 . 0 0 0 0 0 - 0 . 0 6 3 3 0 . 4 6 5 1 0 . 5 9 3 9 1 . 5 0 0 0 . 52 4 2 0 . 0 0 6 3 9 2 . 0 0 0 0 0 - 0 . 0 6 4 3 0 . 4 6 1 2 0 . 6 0 1 6 2 . 0 0 0 0 . 5 8 5 4 0 . 0 0 6 4 8 2 . 0 0 0 0 0 - 0 . 0 6 5 4 0 . 4 5 4 5 0 . 6 1 0 8 2 . 5 0 0 0 . 6 4 6 3 0 . 0 0 6 6 0 2 . 0 0 0 0 0 - 0 . 0 6 6 4 0 . 4 4 7 7 0 . 6 1 6 0 3 . 0 0 0 0 . 7 0 7 4 0 . 0 0 6 6 7 2 . 0 0 0 0 0 - 0 . 0 6 7 4 0 . 4 4 4 5 0 . 6 2 5 8 3 . 5 0 0 0 . 7 6 8 1 0 . 0 0 6 7 9 2 . 0 0 0 0 0 - 0 . 0 6 8 4 0 . 4 3 9 0 0 . 6 3 2 3 4 . 0 0 0 0 . 8 2 8 6 0 . 0 0 6 9 5 2 . 0 0 0 0 0 - 0 . 0 6 9 4 0 . 4 2 9 8 0 . 6 3 7 5 4 . 5 0 0 0 . 8 8 9 1 0 . 0 0 7 0 6 2 . 0 0 0 0 0 - 0 . 0 7 0 4 0 . 4 2 5 9 0 . 6 4 6 4 5 . 0 0 0 0 . 9 4 9 3 0 . 0 0 7 2 2 2 . 0 0 0 0 0 - 0 . 0 7 1 3 0 . 4 1 9 6 0 . 6 5 1 5 5 . 5 0 0 1 . 0 0 9 0 0 . 0 0 7 4 1 2 . 0 0 0 0 0 - o . 0 1 2 2 0 . 4 0 9 0 0 . 6 5 7 0 6 . 0 0 0 1 . 0 6 8 5 0 . 0 0 7 6 1 2 . 0 0 0 0 0 - 0 . 0 7 3 1 0 . 4 0 0 0 0 . 6 6 5 4 6 . 50 0 1 . 12 7 5 0 . 0 0 7 8 6 2 . 0 0 0 0 0 - 0 . 0 7 3 8 0 . 3 8 8 4 0 . 6 7 0 7 7 . 0 0 0 1 . 1 8 5 3 0 . 0 0 8 2 1 2 . 0 0 0 0 0 - 0 . 0 7 4 5 0 . 3 7 0 0 0 . 6 7 4 8 7 . 5 0 0 1 . 2 4 1 8 0 . 0 0 8 6 6 2 . 0 0 0 0 0 - 0 . 0 7 5 0 0 . 3 4 8 4 0 . 6 8 3 6 8 . 0 0 0 1 . 2 9 3 7 0 . 0 0 952 2 . 0 0 0 0 0 - 0 . 0 7 5 0 0 . 3 0 7 5 0 . 6 8 92 8 . 5 0 0 1 . 3 4 4 3 0 . 0 1 0 4 3 2 . 0 0 0 0 0 - 0 . 0 7 4 8 0 . 2 71 1 0 . 6 9 3 3 9 . 0 0 0 1 . 3 9 0 0 0 . 0 1 1 6 4 2 . 0 0 0 0 0 - 0 . 0 7 4 1 0 . 2 2 7 7 0 . 7 0 1 7 9 . 5 0 0 1 . 4 2 9 9 0 . 0 1 3 1 7 2 . 0 0 0 0 0 - 0 . 0 7 2 7 0 . 1 8 0 5 0 . 7 0 7 4

1 0 . 0 0 0 1 . 4 5 72 0 . 0 1 5 2 8 2 . 0 0 0 0 0 - 0 . 0 6 9 9 0 . 1 3 1 9 0 . 7 1 2 2 1 0 . 5 0 0 1 . 4 6 7 0 0 . 0 1 7 7 5 2 . 0 0 0 0 0 - 0 . 0 6 55 0 . 1 0 62 0 . 7 2 1 1 1 1 . 0 0 0 1 . 4 7 2 4 0 . 0 2 1 5 1 2 . 0 0 0 0 0 - 0 . 0 62 9 0 . 0 8 5 6 0 . 7 2 7 5 1 1 . 5 0 0 1 . 4 7 6 5 0 . 0 2 6 1 3 2 . 0 0 0 0 0 - 0 . 0 6 1 5 0 . 0 6 9 6 0 . 7 3 3 0 1 2 . 0 0 0 1 . 4 82 0 0 . 0 3 1 1 4 2 . 0 0 0 0 0 - 0 . 0 6 0 9 0 . 0 5 6 5 0 . 7 4 2 6 1 2 . 5 0 0 1 . 4 8 5 1 0 . 0 3 6 6 9 2 . 0 0 0 0 0 - 0 . 0 6 0 5 0 . 0 4 8 2 0 . 7 4 9 6 1 3 . 0 0 0 1 . 4 8 9 6 0 . 0 42 2 7 2 . 0 0 0 0 0 - 0 . 0 6 0 3 0 . 0 4 1 4 0 . 7 5 9 9 1 3 . 5 0 0 1 . 4 8 9 1 0 . 0 4 8 5 8 2 . 0 0 0 0 0 - 0 . 0 6 0 2 0 . 0 3 6 2 0 . 7 6 7 9 1 4 . 0 0 0 1 . 4 97 3 0 . 0 5 4 0 7 2 . 0 0 0 0 0 - 0 . 0 6 0 3 0 . 0 3 0 3 0 . 7 8 1 0 1 4 . 5 0 0 1 . 5 0 0 5 0 . 0 6 0 2 8 2 . 0 0 0 0 0 - 0 . 0 6 0 6 0 . 02 8 1 0 . 7 9 7 8 1 5 . 0 0 0 1 . 5 0 3 0 0 . 0 6 6 7 6 2 . 0 0 0 0 0 - 0 . 0 6 1 2 0 . 0 2 6 4 0 . 8 2 3 4

FFA TN 1 9 9 0 - 1 5 2 6 POL . W1 8 2_3 0_9 ; 5

XFOI L Ve rsion 5 . 0

Calculated polar for : FFA-W1 - 1 8 2

1 Reynolds numbe r fixed

xtrf • 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pres sure ) Mach • 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

alpha CL CD Re ( CL ) CM s xtr P xt r - - - - - - - -------- --------- --------- ------- - ------- -------- 7 . 0 0 0 0 0 - 0 . 4 9 6 3 0 0 . 0 1 4 3 9 3 . 0 0 0 0 0 - 0 . 0 4 7 1 0 0 . 5 52 9 0 0 . 0 1 0 0 0 - 6 . 5 0 0 0 0 - 0 . 4 4 6 5 0 0 . 0 1 2 1 1 3 . 0 0 0 0 0 - 0 . 0 4 7 4 0 0 . 5 4 2 3 0 0 . 0 1 0 2 0 - 6 . 0 0 0 0 0 - 0 . 3 9 0 6 0 0 . 0 1 0 5 8 3 . 0 0 0 0 0 - 0 . 0 4 8 0 0 0 . 537 1 0 0 . 0 1 0 5 0 - 5 . 5 0 0 0 0 - 0 . 3 3 1 7 0 0 . 0 0 9 6 0 3 . 0 0 0 0 0 - 0 . 0 4 8 8 0 0 . 5 3 0 6 0 0 . 0 1 1 2 0 - 5 . 0 0 0 0 0 - 0 . 2 7 1 2 0 0 . 0 0 9 0 5 3 . 0 0 0 0 0 - 0 . 0 4 9 6 0 0 . 52 1 4 0 0 . 0 1 3 1 0 - 3 . 5 0 0 0 0 - 0 . 0 8 8 0 0 0 . 0 0 8 2 8 3 . 0 0 0 0 0 - 0 . 0 52 4 0 0 . 5 0 4 2 0 0 . 0 2 8 2 0 - 3 . 0 0 0 0 0 - 0 . 0 2 6 7 0 0 . 0 0 8 0 5 3 . 0 0 0 0 0 - 0 . 0 5 3 4 0 0 . 4 9 5 6 0 0 . 0 4 4 2 0 - 2 . 5 0 0 0 0 0 . 0 3 4 3 0 0 . 0 0 7 4 8 3 . 0 0 0 0 0 - 0 . 0 5 4 8 0 0 . 4 9 2 0 0 0 . 1 3 3 3 0 -2 . 0 0 0 0 0 0 . 0 9 5 1 0 0 . 0 0 62 5 3 . 0 0 0 0 0 - 0 . 0 5 6 7 0 0 . 4 8 8 6 0 0 . 3 5 4 9 0 - 1. 5 0 0 0 0 0 . 1 5 6 4 0 0 . 0 0 5 8 4 3 . 0 0 0 0 0 - 0 . 0 5 8 0 0 0 . 4 8 2 2 0 0 . 4 52 1 0 - 1 . 0 0 0 0 0 0 . 2 1 7 9 0 0 . 0 0 5 6 3 3 . 0 0 0 0 0 - 0 . 0 5 9 2 0 0 . 4 7 4 6 0 0 . 5 1 0 7 0 - 0 . 5 0 0 0 0 0 . 2 7 9 5 0 0 . 0 0 5 5 6 3 . 0 0 0 0 0 - 0 . 0 6 0 3 0 0 . 4 6 9 9 0 0 . 5 4 8 3 0

0 . 0 0 0 0 0 0 . 3 4 1 1 0 0 . 0 0 5 5 8 3 . 0 0 0 0 0 - 0 . 0 6 1 3 0 0 . 4 6 6 5 0 0 . 557 5 0 0 . 5 0 0 0 . 4 0 2 1 0 . 0 0 5 6 3 3 . 0 0 0 0 0 - 0 . 0 62 3 0 . 4 5 6 7 0 . 5 6 8 1 1 . 0 0 0 0 . 4 6 3 6 0 . 0 0 5 6 8 3 . 0 0 0 0 0 - 0 . 0 6 3 4 0 . 4 5 3 7 0 . 5 7 42 1 . 5 0 0 0 . 5 2 4 9 0 . 0 0 5 7 4 3 . 0 0 0 0 0 - 0 . 0 6 4 4 0 . 4 4 9 0 0 . 5 8 6 9 2 . 0 0 0 0 . 5 8 6 2 0 . 0 0 5 8 2 3 . 0 0 0 0 0 - 0 . 0 6 5 5 0 . 4 4 0 7 0 . 5 9 4 8 2 . 5 0 0 0 . 6 4 7 3 0 . 0 0 5 9 1 3 . 0 0 0 0 0 - 0 . 0 6 6 5 0 . 4333 0 . 6 0 1 5 3 . 0 0 0 0 . 7 0 8 4 0 . 0 0 5 9 8 3 . 0 0 0 0 0 - 0 . 0 6 7 6 0 . 4 3 0 8 0 . 6 1 2 2 3 . 5 0 0 0 . 7 6 92 0 . 0 0 6 0 9 3 . 0 0 0 0 0 - 0 . 0 6 8 6 0 . 4 2 6 0 0 . 6 1 9 8 4 . 0 0 0 0 . 8 2 9 9 0 . 0 0 62 3 3 . 0 0 0 0 0 - 0 . 0 6 9 6 0 . 4 1 67 0 . 62 3 5 4 . 5 0 0 0 . 8 9 0 3 0 . 0 0 6 3 6 3 . 0 0 0 0 0 - 0 . 0 7 0 6 0 . 4 1 0 4 0 . 63 4 4 5 . 0 0 0 0 . 9 5 0 4 0 . 0 0 6 5 3 3 . 0 0 0 0 0 - 0 . 0 7 1 6 0 . 4 0 2 1 0 . 6 4 1 2 5 . 5 0 0 1 . 0 1 0 1 0 . 0 0 6 7 4 3 . 0 0 0 0 0 - 0 . 0 7 2 5 0 . 3 9 3 6 0 . 6 4 5 8 6 . 0 0 0 1 . 0 6 9 3 0 . 0 0 6 9 8 3 . 0 0 0 0 0 - 0 . 0 7 3 3 0 . 3 8 2 4 0 . 6 5 0 8 6 . 5 0 0 1 . 1 2 7 2 0 . 0 0 7 3 5 3 . 0 0 0 0 0 - 0 . 0 7 4 0 0 . 3 6 0 3 0 . 6 6 0 9 7 . 0 0 0 1 . 1 8 5 2 0 . 0 0 7 6 8 3 . 0 0 0 0 0 - 0 . 0 7 4 7 0 . 3 4 34 0 . 6 6 6 5 7 . 5 0 0 1 . 2 3 6 5 0 . 0 0 8 6 8 3 . 0 0 0 0 0 - 0 . 0 7 4 7 0 . 2 8 9 6 0 . 6 7 1 1 8 . 0 0 0 1 . 2 8 8 6 0 . 0 0 9 5 1 3 . 0 0 0 0 0 - 0 . 0 7 4 7 0 . 2 5 3 5 0 . 6 7 6 6 8 . 5 0 0 1 . 3 3 7 6 0 . 0 1 0 52 3 . 0 0 0 0..0 - 0 . 0 7 4 3 0 . 2 1 0 3 0 . 6 8 4 9 9 . 0 0 0 1 . 3 8 2 6 0 . 0 1 1 7 5 3 . 0 0 0 0 0 - 0 . 0 7 3 5 0 . 1 6 7 7 0 . 6 9 0 7 9 . 5 0 0 1. 4 2 3 4 0 . 0 1 3 1 3 3 . 0 0 0 0 0 - 0 . 0 7 2 2 0 . 1 3 0 5 0 . 6 9 5 4

1 0 . 0 0 0 1 . 4 5 7 2 0 . 0 1 4 7 4 3 . 0 0 0 0 0 - 0 . 0 7 0 1 0 . 1 0 0 7 0 . 6 9 9 0 1 0 . 5 0 0 1 . 4 7 1 7 0 . 0 1 6 7 8 3 . 0 0 0 0 0 - 0 . 0 6 5 7 0 . 0 8 0 4 0 . 7 0 8 5 1 1 . 0 0 0 1 . 4 8 7 9 0 . 0 1 9 4 5 3 . 0 0 0 0 0 - 0 . 0 6 32 0 . 0 6 33 0 . 7 1 6 0 1 1 . 5 0 0 1 . 4 9 3 7 0 . 0 2 3 5 4 3 . 0 0 0 0 0 - 0 . 0 6 1 3 0 . 0 4 9 5 0 . 7 2 0 4

FFA TN 1 9 9 0 - 1 5 2 7

XFOI L Vers ion 5 . 0

Calculated pola r for : FFA-W1 - 1 8 2

1 Reynolds number fixed

xt rf • 0 . 0 1 0 ( suct ion) 0 . 1 0 0 ( pres sure ) Mach •

a lpha --------5 . 0 0 0 0 0 - 4 . 5 0 0 0 0 - 4 . 0 0 0 0 0 - 3 . 5 0 0 0 0 - 3 . 0 0 0 0 0 - 2 . 5 0 0 0 0 - 2 . 0 0 0 0 0 - 1 . 5 0 0 0 0 - 1 . 0 0 0 0 0 - 0 . 5 0 0 0 0

0 . 0 0 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0

0 . 1 5 0

CL --------

- 0 . 2 7 7 4 0 - 0 . 2 1 7 2 0 - 0 . 1 5 7 0 0 - 0 . 0 9 6 4 0 - 0 . 0 3 6 0 0

0 . 0 2 4 2 0 0 . 0 8 4 7 0 0 . 1 4 5 0 0 0 . 2 0 5 2 0 0 . 2 6 5 2 0 0 . 32 5 0 0

0 . 3 8 4 5 0 . 4 4 3 9 0 . 5 0 3 0 0 . 5 6 1 9 0 . 62 0 3 0 . 6 7 8 4 0 . 7 3 6 1 0 . 7 9 3 2 0 . 8 4 9 7 0 . 9 0 5 5 0 . 9 6 0 6 1 . 0 1 4 7 1 . 0 6 7 7 1 . 11 92 1 . 1 6 9 1 1 . 2 1 6 5 1 . 2 5 4 2 1 . 2 8 4 6 1 . 3 1 3 5 1 . 3 3 9 0 1 . 3 6 12 1 . 3 8 1 7 1 . 3 9 9 9

Re = 3 . 0 0 0 e 6 Ncr it

CD Re (CL) CM -- - - - - --- --- ------ ------- -

0 . 0 1 1 0 7 3 . 0 0 0 0 0 - 0 . 0 4 9 7 0 0 . 0 1 0 8 0 3 . 0 0 0 0 0 - 0 . 0 5 0 5 0 0 . 0 1 0 6 8 3 . 0 0 0 0 0 - 0 . 0 5 1 4 0 0 . 0 1 0 5 4 3 . 0 0 0 0 0 - 0 . 0 5 2 2 0 0 . 0 1 0 4 1 3 . 0 0 0 0 0 - 0 . 0 5 3 2 0 0 . 0 1 0 0 9 3 . 0 0 0 0 0 - 0 . 0 5 4 3 0 0 . 0 1 0 1 4 3 . 0 0 0 0 0 - 0 . 0 5 5 2 0 0 . 0 1 0 2 1 3 . 0 0 0 0 0 - 0 . 0 5 6 0 0 0 . 0 1 0 3 0 3 . 0 0 0 0 0 - 0 . 0 5 6 9 0 0 . 0 1 0 4 0 3 . 0 0 0 0 0 - 0 . 0 5 7 8 0 0 . 0 1 0 52 3 . 0 0 0 0 0 - 0 . 0 5 8 7 0

0 . 0 1 0 6 8 3 . 0 0 0 0 0 - 0 . 0 5 9 6 0 . 0 1 0 8 3 3 . 0 0 0 0 0 - 0 . 0 6 0 4 0 . 0 1 1 0 1 3 . 0 0 0 0 0 - 0 . 0 6 1 3 0 . 0 1 1 2 2 3 . 0 0 0 0 0 - 0 . 0 62 1 0 . 0 1 1 4 4 3 . 0 0 0 0 0 - 0 . 0 62 8 0 . 0 1 1 6 9 3 . 0 0 0 0 0 - 0 . 0 6 3 5 0 . 0 1 1 9 6 3 . 0 0 0 0 0 - 0 . 0 6 4 2 0 . 0 1 2 2 6 3 . 0 0 0 0 0 - 0 . 0 6 4 8 0 . 0 1 2 5 9 3 . 0 0 0 0 0 - 0 . 0 6 5 3 0 . 0 1 2 9 5 3 . 0 0 0 0 0 - 0 . 0 6 5 8 0 . 0 1 3 3 5 3 . 0 0 0 0 0 - 0 . 0 6 62 0 . 0 1 3 8 0 3 . 0 0 0 0 0 - 0 . 0 6 6 4 0 . 0 1 4 2 8 3 . 0 0 0 0 0 - 0 . 0 6 6 5 0 . 0 1 4 8 3 3 . 0 0 0 0 0 - 0 . 0 6 6 5 0 . 0 1 5 4 4 3 . 0 0 0 0 0 - 0 . 0 6 62 0 . 0 1 6 1 3 3 . 0 0 0 0 0 - 0 . 0 6 5 6 0 . 0 1 6 9 5 3 . 0 0 0 0 0 - 0 . 0 6 3 6 0 . 0 1 8 2 7 3 . 0 0 0 0 0 - 0 . 0 6 1 4 0 . 02 0 0 7 3 . 0 0 0 0 0 - 0 . 0 5 9 9 0 . 0 2 2 4 2 3 . 0 0 0 0 0 - 0 . 0 5 8 7 0 . 0 2 52 9 3 . 0 0 0 0 0 - 0 . 0 5 7 9 0 . 02 8 6 5 3 . 0 0 0 0 0 - 0 . 0 5 7 4 0 . 0 3 2 3 4 3 . 0 0 0 0 0 - 0 . 0 5 6 9

POL . W1 8 2_30_TU1 ; 5

9 . 0 0 0

S xt r P xt r -- ----- -------0 . 0 1 0 0 0 0 . 0 12 8 0 0 . 0 1 0 0 0 0 . 0 1 7 3 0 0 . 0 1 0 0 0 0 . 0 1 8 4 0 0 . 0 1 0 0 0 0 . 02 7 4 0 0 . 0 1 0 0 0 0 . 0 4 1 2 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 2 8

XFOIL Ve rs ion 5 . 0

Calculated polar for : FFA-W1-2 1 1

1 Reynolds number fixed

xtrf • 1 . 0 0 0 ( suct ion ) l . 0 0 0 (pres sure ) Mach -

alpha -------- 6 . 0 0 0 0 0 - 5 . 5 0 0 0 0 - 5 . 0 0 0 0 0 - 4 . 5 0 0 0 0 - 4 . 0 0 0 0 0 - 3 . 5 0 0 0 0 - 3 . 0 0 0 0 0 - 2 . 5 0 0 0 0 -2 . 0 0 0 0 0 - l . 5 0 0 0 0 - 1 . 0 0 0 0 0 - 0 . 5 0 0 0 0

0 . 0 0 0 0 0 0 . 5 0 0 0 0 1 . 0 0 0 0 0 l . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0 1 5 . 5 0 0 1 6 . 0 0 0 1 6 . 5 0 0 1 7 . 0 0 0 1 7 . 50 0 1 8 . 0 0 0

0 . 1 5 0

CL --------

- 0 . 4 2 8 6 0 - 0 . 3 6 5 9 0 - 0 . 3 0 3 4 0 - 0 . 2 4 0 7 0 - 0 . 1 7 8 0 0 - 0 . 1 1 52 0 - 0 . 0 5 2 7 0

0 . 0 0 9 9 0 0 . 0 7 2 2 0 0 . 1 3 4 7 0 0 . 1 9 7 1 0 0 . 2 5 9 3 0 0 . 32 12 0 0 . 3 8 3 1 0 0 . 4 4 5 0 0

0 . 4 4 5 0 0 . 5 0 6 6 0 . 5 6 8 1 0 . 62 92 0 . 6 9 0 2 0 . 7 5 1 2 0 . 8 1 1 7 0 . 8 7 1 9 0 . 9 3 2 0 0 . 9 9 1 5 1 . 0 5 0 7 1 . 1 0 9 9 1 . 1 6 7 9 l . 2 2 5 9 l . 2 8 2 6 l . 3 3 8 0 l . 3 92 0 1 . 4 4 0 9 1 . 4 8 3 8 1 . 5 1 4 6 l . 5 1 3 5 1 . 5 1 0 8 l . 5 0 7 3 1 . 4 9 9 8 l . 4 9 3 2 1 . 4 8 6 8 l. 4 8 3 4 1 . 4 7 4 9 l. 4 7 4 3 1 . 4 7 1 6 l . 4 6 7 8 1 . 4 6 5 2 l . 4 6 4 8 1 . 4 6 3 1 l . 4 6 2 6

Re = 1 . 0 0 0 e 6 Ncr it

CD Re (CL) CM --------- --------- --------

0 . 0 0 8 4 9 1 . 0 0 0 0 0 - 0 . 0 6 0 3 0 0 . 0 0 8 4 1 1 . 0 0 0 0 0 - 0 . 0 6 1 4 0 0 . 0 0 8 5 3 1 . 0 0 0 0 0 - 0 . 0 62 3 0 0 . 0 0 8 5 8 1 . 0 0 0 0 0 - 0 . 0 6 3 3 0 0 . 0 0 8 53 1 . 0 0 0 0 0 - 0 . 0 6 4 5 0 0 . 0 0 8 4 9 1 . 0 0 0 0 0 - 0 . 0 6 5 6 0 0 . 0 0 8 5 1 1 . 0 0 0 0 0 - 0 . 0 6 6 7 0 0 . 0 0 8 5 5 1 . 0 0 0 0 0 - 0 . 0 6 7 8 0 0 . 0 0 8 6 0 1 . 0 0 0 0 0 - 0 . 0 6 8 8 0 0 . 0 0 8 5 8 1 . 0 0 0 0 0 - 0 . 0 7 0 0 0 0 . 0 0 8 6 0 1 . 0 0 0 0 0 - 0 . 0 7 1 1 0 0 . 0 0 8 6 7 1 . 0 0 0 0 0 - 0 . 0 7 2 2 0 0 . 0 0 8 7 6 1 . 0 0 0 0 0 - 0 . 0 7 3 2 0 0 . 0 0 8 8 5 1 . 0 0 0 0 0 - 0 . 0 7 4 1 0 0 . 0 0 8 9 1 1 . 0 0 0 0 0 - 0 . 0 7 5 2 0

0 . 0 0 8 9 1 1 . 0 0 0 0 0 - 0 . 0 7 5 2 0 . 0 0 8 9 9 1 . 0 0 0 0 0 - 0 . 0 7 6 2 0 . 0 0 9 1 0 1 . 0 0 0 0 0 - o . 0 7 7 1 0 . 0 0 9 2 7 1 . 0 0 0 0 0 - o . o 7 8 o 0 . 0 0 9 4 2 1 . 0 0 0 0 0 - 0 . 0 7 8 9 0 . 0 0 9 5 3 1 . 0 0 0 0 0 - 0 . 0 7 9 8 0 . 0 0 9 7 0 1 . 0 0 0 0 0 - 0 . 0 8 0 6 0 . 0 0 9 9 1 1 . 0 0 0 0 0 - 0 . 0 8 1 3 0 . 0 1 0 0 8 1 . 0 0 0 0 0 - 0 . 0 8 2 0 0 . 0 1 0 3 3 1 . 0 0 0 0 0 - 0 . 0 8 2 6 0 . 0 1 0 5 6 1 . 0 0 0 0 0 - 0 . 0 8 32 0 . 0 1 0 7 7 1 . 0 0 0 0 0 - 0 . 0 8 3 8 0 . 0 1 1 1 0 1 . 0 0 0 0 0 - 0 . 0 8 4 2 0 . 0 11 3 9 1 . 0 0 0 0 0 - 0 . 0 8 4 5 0 . 0 1 1 7 8 1 . 0 0 0 0 0 - 0 . 0 8 4 7 0 . 0 1 2 2 3 l. 0 0 0 0 0 - 0 . 0 8 4 8 0 . 0 1 2 7 7 1 . 0 0 0 0 0 - 0 . 0 8 4 7 0 . 0 1 3 6 4 1 . 0 0 0 0 0 - 0 . 0 8 3 9 0 . 0 1 4 8 5 1 . 0 0 0 0 0 - 0 . 0 8 2 5 0 . 0 1 6 6 1 1 . 0 0 0 0 0 - 0 . 0 7 9 8 0 . 0 1 9 6 5 1 . 0 0 0 0 0 - 0 . 0 7 3 9 0 . 0 2 3 9 4 1 . 0 0 0 0 0 - 0 . 0 7 0 6 0 . 0 2 92 9 1 . 0 0 0 0 0 - 0 . 0 6 9 1 0 . 0 3 5 8 2 1 . 0 0 0 0 0 - 0 . 0 6 8 6 0 . 0 4 2 8 2 1 . 0 0 0 0 0 - 0 . 0 6 8 8 0 . 0 5 0 2 5 l . 0 0 0 0 0 - 0 . 0 6 9 4 0 . 0 5 7 5 6 1 . 0 0 0 0 0 - 0 . 0 7 0 2 0 . 0 6 5 7 8 1 . 0 0 0 0 0 - 0 . 0 71 4 0 . 0 7 3 1 9 l . 0 0 0 0 0 - 0 . 0 7 2 5 0 . 0 8 1 1 1 1 . 0 0 0 0 0 - 0 . 0 7 3 9 0 . 0 8 9 3 9 1 . 0 0 0 0 0 - 0 . 0 7 5 6 0 . 0 9 7 6 6 1 . 0 0 0 0 0 - 0 . 07 7 3 0 . 1 0 5 8 8 l . 0 0 0 0 0 - 0 . 0 7 9 1 0 . 1 1 4 5 8 l . 0 0 0 0 0 - 0 . 0 8 1 3 0 . 12 3 2 8 1 . 0 0 0 0 0 - 0 . 0 8 3 6

POL . W2 1 1_1 0_9 ; 4

9 . 0 0 0

5 xt r P xt r --- - --- - ------0 . 5 7 6 5 0 0 . 4 0 0 5 0 0 . 5 6 4 3 0 0 . 4 1 8 2 0 0 . 5 5 1 6 0 0 . 4 3 5 5 0 0 . 5 3 8 6 0 0 . 4 3 9 8 0 0 . 52 9 6 0 0 . 4 4 4 9 0 0 . 5 1 6 5 0 0 . 4 5 0 4 0 0 . 5 0 8 5 0 0 . 4 5 4 2 0 0 . 4 9 7 3 0 0 . 4 5 7 2 0 0 . 4 9 0 4 0 0 . 4 6 0 1 0 0 . 4 7 8 8 0 0 . 4 6 5 5 0 0 . 4 7 3 0 0 0 . 4 7 0 2 0 0 . 4 6 4 9 0 0 . 4 7 3 3 0 0 . 4 5 7 2 0 0 . 4 7 6 4 0 0 . 4 5 0 8 0 0 . 4 7 8 9 0 0 . 4 42 1 0 0 . 4 8 3 8 0 0 . 4 4 2 1 0 . 4 8 3 8 0 . 4 3 6 8 0 . 4 8 8 8 0 . 4 3 0 9 0 . 4 9 2 0 0 . 4 2 2 6 0 . 4 9 4 9 0 . 4 1 7 7 0 . 4 9 7 8 0 . 4 1 2 5 0 . 5 0 2 5 0 . 4 0 4 3 0 . 5 0 7 5 0 . 3 9 8 8 0 . 5 1 1 0 0 . 3 9 4 0 0 . 5 1 4 1 0 . 3 8 62 0 . 5 1 7 2 0 . 3 7 9 3 0 . 52 2 8 0 . 3 7 2 7 0 . 52 7 6 0 . 3 6 1 5 0 . 5 3 1 2 0 . 3 5 2 3 0 . 5 3 4 5 0 . 3 3 9 5 0 . 5 3 7 7 0 . 32 3 0 0 . 5 4 52 0 . 3 0 9 0 0 . 5 4 9 3 0 . 2 8 2 4 0 . 5 52 8 0 . 2 5 1 4 0 . 5 5 6 0 0 . 2 1 2 5 0 . 5 6 2 9 0 . 1 7 0 3 0 . 5 6 7 0 0 . 1 4 3 9 0 . 5 7 0 4 0 . 1 1 6 5 0 . 57 3 7 0 . 0 9 7 6 0 . 5 7 7 7 0 . 0 8 52 0 . 5 8 3 2 0 . 0 7 5 3 0 . 5 8 6 9 0 . 0 6 3 3 0 . 5 9 0 2 0 . 0 5 8 1 0 . 5 9 3 0 0 . 0 5 0 4 0 . 5 9 7 7 0 . 0 4 6 3 0 . 6 0 3 1 0 . 0 4 3 7 0 . 6 0 7 5 0 . 0 3 9 9 0 . 6 1 0 8 0 . 0 3 5 3 0 . 6 1 4 1 0 . 0 3 2 8 0 . 62 0 9 0 . 0 3 1 7 0 . 6 2 5 7

FFA TN 1 9 9 0 - 1 5 2 9 POL . W2 1 1_1 0_TU1 ; 2

XFOI L Version 5 . 0

Calculated polar for : FFA-W1-2 1 1

1 Reynolds number f ixed

xt rf • 0 . 0 1 0 ( suction) 0 . 1 0 0 (pres sure ) Mach • 0 . 1 5 0 Re - 1 . 0 0 0 e 6 Ncrit "" 9 . 0 0 0

alpha CL CD Re (CL) CM S xtr P xt r --- - - -- --- - -- - - -- - ------ --- - - - --- - ----- -- - -- - --- - - -- - - -

1 . 0 0 0 0 . 4 1 6 9 0 . 0 1 4 0 3 1 . 0 0 0 0 0 - 0 . 0 7 0 6 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 4 7 6 4 0 . 0 1 4 2 2 1 . 0 0 0 0 0 - 0 . 0 7 1 4 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 5 3 5 3 0 . 0 1 4 4 3 1 . 0 0 0 0 0 - 0 . 0 7 2 2 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 5 9 3 8 0 . 0 1 4 6 8 1 . 0 0 0 0 0 - 0 . 0 7 2 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 5 1 8 0 . 0 1 4 9 7 1 . 0 0 0 0 0 - o . 0 7 3 5 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 7 0 9 0 0 . 0 1 5 3 0 1 . 0 0 0 0 0 - 0 . 0 7 4 1 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 7 6 5 5 0 . 0 1 5 6 6 1 . 0 0 0 0 0 - 0 . 0 7 4 5 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 8 2 12 0 . 0 1 6 0 7 1 . 0 0 0 0 0 - 0 . 0 7 4 8 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 8 7 5 8 0 . 0 1 6 5 4 1 . 0 0 0 0 0 - 0 . 0 7 5 0 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 92 9 3 0 . 0 1 7 0 6 1 . 0 0 0 0 0 - 0 . 0 7 5 0 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 9 8 1 3 0 . 0 1 7 6 4 1 . 0 0 0 0 0 - 0 . 0 7 4 9 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 0 3 1 5 0 . 0 1 8 3 1 1 . 0 0 0 0 0 - 0 . 0 7 4 6 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 0 7 92 0 . 0 1 9 0 7 1 . 0 0 0 0 0 - 0 . 0 7 4 0 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1 2 1 1 0 . 0 1 9 9 5 1 . 0 0 0 0 0 - 0 . 0 7 2 5 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 1 5 1 2 0 . 02 1 1 6 1 . 0 0 0 0 0 - 0 . 0 6 9 8 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 1 8 3 4 0 . 0 2 2 8 6 1 . 0 0 0 0 0 - 0 . 0 6 8 5 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 2 1 1 3 0 . 0 2 5 1 0 1 . 0 0 0 0 0 - 0 . 0 6 7 5 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 2 3 5 9 0 . 0 2 7 9 0 1 . 0 0 0 0 0 - 0 . 0 6 6 8 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 2 57 8 0 . 0 3 1 2 7 1 . 0 0 0 0 0 - 0 . 0 6 6 6 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 27 6 9 0 . 0 3 5 1 7 1 . 0 0 0 0 0 - 0 . 0 6 6 6 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 2 9 3 8 0 . 0 3 9 5 6 1 . 0 0 0 0 0 - 0 . 0 6 6 9 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 3 0 8 4 0 . 0 4 4 3 8 1 . 0 0 0 0 0 - 0 . 0 6 7 4 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 32 1 3 0 . 0 4 9 6 1 1 . 0 0 0 0 0 - 0 . 0 6 8 0 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 3 3 1 9 0 . 0 5 52 0 1 . 0 0 0 0 0 - 0 . 0 6 8 7 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1. 3 4 1 1 0 . 0 6 1 1 6 1 . 0 0 0 0 0 - 0 . 0 6 9 5 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 3 4 9 5 0 . 0 6 7 3 4 1 . 0 0 0 0 0 - 0 . 0 7 0 5 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 35 6 7 0 . 0 7 3 7 6 1 . 0 0 0 0 0 - 0 . 0 7 1 6 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1. 3 6 3 5 0 . 0 8 0 4 3 1 . 0 0 0 0 0 - 0 . 0 7 2 8 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 3 6 9 9 0 . 0 8 7 3 0 1 . 0 0 0 0 0 - 0 . 0 7 4 2 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 3 0

XFOI L Ve rs ion 5 . 0

Calculated polar for : FFA-W1 -2 1 1

1 Reynolds numbe r fixed

xt rf ... 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pres sure ) Mach •

a lpha -------- 8 . 0 0 0 0 0 - 7 . 5 0 0 0 0 - 7 . 0 0 0 0 0 - 6 . 5 0 0 0 0 - 6 . 0 0 0 0 0 -5 . 5 0 0 0 0 - 5 . 0 0 0 0 0 - 4 . 5 0 0 0 0 - 4 . 0 0 0 0 0 - 3 . 5 0 0 0 0 - 3 . 0 0 0 0 0 -2 . 5 0 0 0 0 -2 . 0 0 0 0 0 - 1 . 5 0 0 0 0 - 1 . 0 0 0 0 0 - 0 . 5 0 0 0 0

0 . 0 0 0 0 0 0 . 5 0 0 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 50 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0

0 . 1 5 0

CL --------

- 0 . 6 8 0 5 0 - 0 . 6 1 7 9 0 - 0 . 5 5 4 2 0 - 0 . 4 8 9 1 0 - 0 . 4 2 5 7 0 - 0 . 3 6 2 7 0 - 0 . 2 9 9 7 0 - 0 . 2 3 7 1 0 - 0 . 1 7 4 0 0 - 0 . 1 1 1 1 0 - 0 . 0 4 8 2 0

0 . 0 1 4 5 0 0 . 0 7 7 5 0 0 . 1 4 0 2 0 0 . 2 0 2 9 0 0 . 2 6 5 3 0 0 . 32 7 7 0 0 . 3 9 0 3 0

0 . 4 5 2 6 0 . 5 1 4 8 0 . 5 7 6 7 0 . 6 3 8 5 0 . 7 0 0 4 0 . 7 62 0 0 . 8 2 3 3 0 . 8 8 4 5 0 . 9 4 5 4 1 . 0 0 5 9 1 . 0 6 6 2 1 . 12 5 9 1 . 1 8 4 5 1 . 2 4 2 4 1 . 2 9 9 7 1 . 3 5 3 3 1 . 4 0 4 2 1 . 4 4 9 5 1 . 4 8 4 0 1 . 5 1 1 2 1 . 5 2 4 0 1 . 5 3 3 2 1 . 53 7 1 1 . 5 3 9 9 1 . 5 4 4 9 1 . 5 4 8 4 1 . 5 4 6 8 1. 5 4 8 5 1 . 5 5 2 8

Re = 2 . 0 0 0 e 6 Ncr it

CD Re (CL) CM --------- --------- --------

0 . 0 1 3 7 0 2 . 0 0 0 0 0 - 0 . 0 4 6 9 0 0 . 0 1 2 4 6 2 . 0 0 0 0 0 - 0 . 0 5 0 1 0 0 . 0 1 0 8 5 2 . 0 0 0 0 0 - 0 . 0 5 3 9 0 0 . 0 0 8 1 6 2 . 0 0 0 0 0 - 0 . 0 5 9 0 0 0 . 0 0 7 3 4 2 . 0 0 0 0 0 - 0 . 0 6 1 1 0 0 . 0 0 7 0 4 2 . 0 0 0 0 0 - 0 . 0 62 5 0 0 . 0 0 6 8 7 2 . 0 0 0 0 0 - 0 . 0 6 3 7 0 0 . 0 0 6 8 3 2 . 0 0 0 0 0 - 0 . 0 6 4 8 0 0 . 0 0 6 7 9 2 . 0 0 0 0 0 - 0 . 0 6 5 9 0 0 . 0 0 6 8 0 2 . 0 0 0 0 0 - 0 . 0 67 0 0 0 . 0 0 6 8 3 2 . 0 0 0 0 0 - 0 . 0 6 8 1 0 0 . 0 0 6 8 7 2 . 0 0 0 0 0 - 0 . 0 6 9 2 0 0 . 0 0 6 8 6 2 . 0 0 0 0 0 - 0 . 0 7 0 4 0 0 . 0 0 6 8 8 2 . 0 0 0 0 0 - 0 . 0 7 1 5 0 0 . 0 0 6 9 3 2 . 0 0 0 0 0 - 0 . 0 7 2 6 0 0 . 0 0 7 0 0 2 . 0 0 0 0 0 - 0 . 0 7 3 6 0 0 . 0 0 7 0 7 2 . 0 0 0 0 0 - 0 . 0 7 4 7 0 0 . 0 0 7 1 0 2 . 0 0 0 0 0 - 0 . 0 7 5 8 0

0 . 0 0 7 1 8 2 . 0 0 0 0 0 - 0 . 0 7 6 8 0 . 0 0 7 2 6 2 . 0 0 0 0 0 - 0 . 0 7 7 8 0 . 0 0 7 3 6 2 . 0 0 0 0 0 - o . 0 78 8 0 . 0 0 7 5 0 2 . 0 0 0 0 0 - 0 . 0 7 9 8 0 . 0 0 7 5 7 2 . 0 0 0 0 0 - 0 . 0 8 0 8 0 . 0 0 7 6 9 2 . 0 0 0 0 0 - 0 . 0 8 1 7 0 . 0 0 7 8 5 2 . 0 0 0 0 0 - 0 . 0 8 2 6 0 . 0 0 7 9 8 2 . 0 0 0 0 0 - 0 . 0 8 3 4 0 . 0 0 8 1 5 2 . 0 0 0 0 0 - 0 . 0 8 4 2 0 . 0 0 8 3 4 2 . 0 0 0 0 0 - 0 . 0 8 5 0 0 . 0 0 8 5 3 2 . 0 0 0 0 0 - 0 . 0 8 5 7 0 . 0 0 8 7 9 2 . 0 0 0 0 0 - 0 . 0 8 6 4 0 . 0 0 9 1 1 2 . 0 0 0 0 0 - 0 . 0 8 6 8 0 . 0 0 9 4 9 2 . 0 0 0 0 0 - 0 . 0 8 7 2 0 . 0 0 9 8 8 2 . 0 0 0 0 0 - 0 . 0 8 7 5 0 . 0 1 0 5 8 2 . 0 0 0 0 0 - 0 . 0 8 7 4 0 . 0 1 1 4 5 2 . 0 0 0 0 0 - 0 . 0 8 6 9 0 . 0 12 6 8 2 . 0 0 0 0 0 - 0 . 0 8 5 8 0 . 0 1 4 5 4 2 . 0 0 0 0 0 - 0 . 0 8 3 5 0 . 0 1 6 3 7 2 . 0 0 0 0 0 - 0 . 0 8 0 1 0 . 0 1 8 6 1 2 . 0 0 0 0 0 - 0 . 0 7 5 5 0 . 02 1 8 7 2 . 0 0 0 0 0 - 0 . 0 7 2 6 0 . 0 2 6 2 9 2 . 0 0 0 0 0 - 0 . 0 7 0 8 0 . 0 3 1 5 0 2 . 0 0 0 0 0 - 0 . 0 7 0 1 0 . 0 3 6 9 9 2 . 0 0 0 0 0 - 0 . 0 6 9 9 0 . 0 4 2 9 2 2 . 0 0 0 0 0 - 0 . 0 7 0 1 0 . 0 4 9 7 9 2 . 0 0 0 0 0 - 0 . 0 7 0 6 0 . 0 5 6 4 1 2 . 0 0 0 0 0 - 0 . 0 7 1 2 0 . 0 62 9 4 2 . 0 0 0 0 0 - 0 . 0 7 1 9

POL . W2 1 1_2 0_9 ; 3

9 . 0 0 0

S xt r P xt r ------- -------0 . 5 9 32 0 0 . 0 4 1 5 0 0 . 5 7 8 5 0 0 . 0 6 0 6 0 0 . 5 6 7 2 0 0 . 12 0 3 0 0 . 5 5 2 2 0 0 . 2 8 5 5 0 0 . 5 3 7 8 0 0 . 3 5 2 4 0 0 . 52 9 5 0 0 . 3 8 1 6 0 0 . 5 1 6 6 0 0 . 4 0 4 1 0 0 . 5 0 6 8 0 0 . 4 2 5 4 0 0 . 4 9 6 1 0 0 . 4 3 2 6 0 0 . 4 8 8 2 0 0 . 4 3 6 9 0 0 . 4 7 7 7 0 0 . 4 3 9 6 0 0 . 4 7 0 4 0 0 . 4 4 1 7 0 0 . 4 5 9 5 0 0 . 4 4 8 6 0 0 . 4 5 4 9 0 0 . 4 5 3 5 0 0 . 4 4 7 5 0 0 . 4 5 6 4 0 0 . 4 3 8 7 0 0 . 4 5 8 9 0 0 . 4 3 4 1 0 0 . 4 6 0 8 0 0 . 4 2 6 7 0 0 . 4 6 7 4 0 0 . 4 1 9 7 0 . 4 7 1 8 0 . 4 1 52 0 . 4 7 4 8 0 . 4 0 9 1 0 . 4 7 7 4 0 . 4 0 0 7 0 . 4 7 9 4 0 . 3 9 7 5 0 . 4 8 4 4 0 . 3 9 1 7 0 . 4 9 0 0 0 . 3 8 2 3 0 . 4 9 3 4 0 . 3 7 8 5 0 . 4 9 6 0 0 . 3 7 3 9 0 . 4 9 8 2 0 . 3 62 7 0 . 5 0 2 9 0 . 3572 0 . 5 0 9 0 0 . 3 4 4 0 0 . 5 1 2 7 0 . 3 3 2 7 0 . 5 1 5 5 0 . 3 1 7 9 0 . 5 1 7 8 0 . 3 0 2 2 0 . 52 4 0 0 . 2 7 6 9 0 . 52 9 1 0 . 2 4 5 0 0 . 5 3 3 1 0 . 2 0 7 0 0 . 5 3 5 8 0 . 1 5 9 3 0 . 5 3 9 7 0 . 1 2 6 4 0 . 5 4 5 8 0 . 1 0 1 2 0 . 5 4 9 8 0 . 0 8 3 7 0 . 5 52 9 0 . 0 7 2 7 0 . 5 5 5 3 0 . 0 6 0 6 0 . 5 5 92 0 . 0 5 2 4 0 . 5 6 5 6 0 . 0 4 6 6 0 . 5 6 9 3 0 . 0 4 3 5 0 . 57 2 1 0 . 0 3 9 0 0 . 5 7 4 5 0 . 0 3 4 3 0 . 5 7 8 8

FFA TN 1 9 9 0 - 1 5 3 1 POL . W2 1 1_30_9 ; 3

XFOIL Vers ion 5 . 0

Calculated polar for : FFA-W1-2 1 1

1 Reynolds number f ixed

xt r f • 1 . 0 0 0 ( s uction) 1 . 0 0 0 (pre s sure ) Mach • 0 . 1 5 0 Re ... 3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

alpha CL CD Re (CL) CM S xt r P xtr - ------ -------- --------- --------- ---- ---- - ------ -------

- 1 0 . 0 0 0 0 0 - 0 . 9 2 3 7 0 0 . 0 1 8 7 0 3 . 0 0 0 0 0 - 0 . 0 3 3 5 0 0 . 63 4 2 0 0 . 0 1 9 6 0 - 9 . 5 0 0 0 0 - 0 . 8 6 5 8 0 0 . 0 1 657 3 . 0 0 0 0 0 - 0 . 0 3 8 3 0 0 . 6 1 6 8 0 0 . 0 1 9 9 0 - 9 . 0 0 0 0 0 - 0 . 8 0 3 1 0 0 . 0 1 4 4 7 3 . 0 0 0 0 0 - 0 . 0 4 3 4 0 0 . 5 9 9 7 0 0 . 02 3 2 0 - 8 . 5 0 0 0 0 - 0 . 7 4 0 3 0 0 . 0 1 3 3 1 3 . 0 0 0 0 0 - 0 . 0 4 6 6 0 0 . 5 8 4 5 0 0 . 0 2 7 8 0 - 8 . 0 0 0 0 0 - 0 . 6 7 8 3 0 0 . 0 1 2 4 0 3 . 0 0 0 0 0 - 0 . 0 4 9 1 0 0 . 5 7 2 7 0 0 . 0 32 7 0 - 7 . 5 0 0 0 0 - 0 . 6 1 5 9 0 0 . 0 1 1 6 5 3 . 0 0 0 0 0 - 0 . 0 5 1 3 0 0 . 5 5 5 8 0 0 . 0 4 4 0 0 - 7 . 0 0 0 0 0 - 0 . 5 5 3 1 0 0 . 0 1 0 7 5 3 . 0 0 0 0 0 - 0 . 0 5 3 8 0 0 . 5 4 5 2 0 0 . 0 6 9 3 0 - 6 . 5 0 0 0 0 - 0 . 4 8 8 9 0 0 . 0 0 9 0 4 3 . 0 0 0 0 0 - 0 . 0 5 7 4 0 0 . 5 3 1 2 0 0 . 1 5 9 8 0 - 6 . 0 0 0 0 0 - 0 . 4 2 4 9 0 0 . 0 0 7 3 3 3 . 0 0 0 0 0 - 0 . 0 6 0 7 0 0 . 52 2 7 0 0 . 2 7 9 5 0 - 5 . 5 0 0 0 0 - 0 . 3 6 1 6 0 0 . 0 0 6 6 7 3 . 0 0 0 0 0 - 0 . 0 62 6 0 0 . 5 0 8 7 0 0 . 3 4 4 0 0 - 5 . 0 0 0 0 0 - 0 . 2 9 8 5 0 0 . 0 0 6 3 6 3 . 0 0 0 0 0 - 0 . 0 6 4 0 0 0 . 5 0 2 3 0 0 . 3 7 3 3 0 - 4 . 5 0 0 0 0 - 0 . 2 3 5 5 0 0 . 0 0 6 1 4 3 . 0 0 0 0 0 - 0 . 0 6 5 2 0 0 . 4 8 7 2 0 0 . 4 1 1 4 0 - 4 . 0 0 0 0 0 - 0 . 1 7 2 7 0 0 . 0 0 6 1 1 3 . 0 0 0 0 0 - 0 . 0 6 6 3 0 0 . 4 8 1 6 0 0 . 42 2 2 0 - 3 . 5 0 0 0 0 - 0 . 1 0 9 7 0 0 . 0 0 6 1 0 3 . 0 0 0 0 0 - 0 . 0 6 7 5 0 0 . 4 7 3 0 0 0 . 4 2 9 9 0 - 3 . 0 0 0 0 0 - 0 . 0 4 6 7 0 0 . 0 0 6 1 1 3 . 0 0 0 0 0 - 0 . 0 6 8 6 0 0 . 4 62 2 0 0 . 4 3 4 3 0 - 2 . 5 0 0 0 0 0 . 0 1 62 0 0 . 0 0 6 1 2 3 . 0 0 0 0 0 - 0 . 0 6 9 7 0 0 . 4 5 7 9 0 0 . 4 3 7 8 0 - 2 . 0 0 0 0 0 0 . 0 7 8 9 0 0 . 0 0 6 1 8 3 . 0 0 0 0 0 - 0 . 0 7 0 7 0 0 . 4 4 8 4 0 0 . 4 3 9 6 0 - 1 . 5 0 0 0 0 0 . 1 4 1 7 0 0 . 0 0 62 1 3 . 0 0 0 0 0 - o . o n 8 o 0 . 4 3 9 0 0 0 . 4 4 2 9 0 - 1 . 0 0 0 0 0 0 . 2 0 4 5 0 0 . 0 0 62 2 3 . 0 0 0 0 0 - 0 . 0 7 3 0 0 0 . 4 3 5 5 0 0 . 4 4 9 0 0 - 0 . 5 0 0 0 0 0 . 2 6 7 2 0 0 . 0 0 62 7 3 . 0 0 0 0 0 - 0 . 0 7 4 0 0 0 . 4 3 0 0 0 0 . 4 5 4 7 0

0 . 0 0 0 0 0 0 . 32 9 8 0 0 . 0 0 6 3 2 3 . 0 0 0 0 0 - 0 . 0 7 5 1 0 0 . 42 1 6 0 0 . 4 5 8 0 0 0 . 5 0 0 0 0 0 . 3 9 2 3 0 0 . 0 0 6 3 8 3 . 0 0 0 0 0 - 0 . 0 7 62 0 0 . 4 1 4 6 0 0 . 4 6 0 4 0 1 . 0 0 0 0 . 4 5 4 1 0 . 0 0 6 4 5 3 . 0 0 0 0 0 - 0 . 0 7 6 6 0 . 4 0 6 7 0 . 4 6 3 4 1 . 5 0 0 0 . 5 1 6 3 0 . 0 0 6 52 3 . 0 0 0 0 0 - 0 . 0 7 7 6 0 . 4 0 4 0 0 . 4 6 7 2 2 . 0 0 0 0 . 5 7 8 3 0 . 0 0 6 6 1 3 . 0 0 0 0 0 - 0 . 0 7 8 6 0 . 3 9 9 3 0 . 4 7 0 5 2 . 5 0 0 0 . 6 4 0 2 0 . 0 0 67 1 3 . 0 0 0 0 0 - 0 . 0 7 9 6 0 . 3 92 7 0 . 4 7 2 4 3 . 0 0 0 0 . 7 0 1 9 0 . 0 0 6 8 4 3 . 0 0 0 0 0 - 0 . 0 8 0 6 0 . 3 8 3 5 0 . 4 7 3 9 3 . 5 0 0 0 . 7 6 3 8 0 . 0 0 6 9 1 3 . 0 0 0 0 0 - 0 . 0 8 1 5 0 . 3 8 1 2 0 . 4 7 9 1 4 . 0 0 0 0 . 82 52 0 . 0 0 7 0 4 3 . 0 0 0 0 0 - 0 . 0 8 2 5 0 . 3 7 62 0 . 4 8 5 5 4 . 50 0 0 . 8 8 6 5 0 . 0 0 7 1 8 3 . 0 0 0 0 0 - 0 . 0 8 3 3 0 . 3 6 7 5 0 . 4 8 9 5 5 . 0 0 0 0 . 9 4 7 5 0 . 0 0 7 3 3 3 . 0 0 0 0 0 - 0 . 0 8 42 0 . 3 6 0 1 0 . 4 92 4 5 . 5 0 0 1 . 0 0 8 2 0 . 0 0 7 5 0 3 . 0 0 0 0 0 - 0 . 0 8 5 0 0 . 3 5 5 1 0 . 4 9 4 6 6 . 0 0 0 1 . 0 6 8 3 0 . 0 0 7 7 3 3 . 0 0 0 0 0 - 0 . 0 8 5 7 0 . 3 4 12 0 . 4 9 62 6 . 5 0 0 1 . 12 8 1 0 . 0 0 7 9 7 3 . 0 0 0 0 0 - 0 . 0 8 6 3 0 . 3 3 3 3 0 . 5 0 33 7 . 0 0 0 1 . 1 8 6 1 0 . 0 0 8 3 7 3 . 0 0 0 0 0 - 0 . 0 8 6 8 0 . 3 1 2 1 0 . 5 0 8 8 7 . 5 0 0 1 . 2 4 4 5 0 . 0 0 8 7 1 3 . 0 0 0 0 0 - 0 . 0 8 7 3 0 . 2 9 4 6 0 . 5 1 2 7 8 . 0 0 0 1 . 3 0 0 7 0 . 0 0 9 2 2 3 . 0 0 0 0 0 - 0 . 0 8 7 5 0 . 2 7 62 0 . 5 1 5 6 8 . 5 0 0 1 . 35 0 7 0 . 0 1 0 2 6 3 . 0 0 0 0 0 - 0 . 0 8 6 9 0 . 2 332 0 . 5 1 7 7 9 . 0 0 0 1 . 3 9 9 0 0 . 0 1 1 3 4 3 . 0 0 0 0 0 - 0 . 0 8 62 0 . 1 9 7 8 0 . 52 1 6 9 . 5 0 0 1 . 4 4 3 8 0 . 0 1 2 5 7 3 . 0 0 0 0 0 - 0 . 0 8 5 0 0 . 1 5 8 3 0 . 52 8 0

1 0 . 0 0 0 1 . 4 8 3 5 0 . 0 1 4 0 2 3 . 0 0 0 0 0 - 0 . 0 8 32 0 . 1 2 4 6 0 . 53 3 7 1 0 . 5 0 0 1 . 5 1 0 5 0 . 0 1 5 8 8 3 . 0 0 0 0 0 - 0 . 0 7 9 8 0 . 0 9 1 7 0 . 5 3 6 8 1 1 . 0 0 0 1 . 52 8 7 0 . 0 1 7 6 5 3 . 0 0 0 0 0 - 0 . 0 7 5 4 0 . 0 7 4 7 0 . 5 3 9 1 1 1 . 5 0 0 1 . 5 4 3 0 0 . 0 2 0 2 9 3 . 0 0 0 0 0 - 0 . 0 7 2 2 0 . 0 6 3 3 0 . 5 4 0 8

FFA TN 1 9 9 0 - 1 5 3 2 POL . W2 1 1_3 0_TU 1 ; 2

XFOIL Ve rs ion 5 . 0

Calculated polar for : FFA-W1 - 2 1 1

1 Reynolds number fixed

xt r f • 0 . 0 1 0 ( suct ion ) 0 . 1 0 0 (pre s sure ) Mach • 0 . 1 5 0 R e = 3 . 0 0 0 e 6 Ncrit = 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xt r ------- -------- --------- --------- -------- ------- -------

1 . 0 0 0 0 . 42 9 6 0 . 0 1 1 4 9 3 . 0 0 0 0 0 - 0 . 0 7 2 2 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 4 8 9 8 0 . 0 1 1 6 4 3 . 0 0 0 0 0 - 0 . 0 7 3 1 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 5 4 9 8 0 . 0 1 1 82 3 . 0 0 0 0 0 - 0 . 0 7 4 0 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 6 0 9 3 0 . 0 1 2 0 2 3 . 0 0 0 0 0 - 0 . 0 7 4 7 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 6 8 5 0 . 0 1 2 2 5 3 . 0 0 0 0 0 - 0 . 0 7 5 5 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 7 2 7 2 0 . 0 1 2 5 0 3 . 0 0 0 0 0 - 0 . 0 7 6 1 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 7 8 5 4 0 . 0 1 2 7 8 3 . 0 0 0 0 0 - 0 . 0 7 67 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 8 4 3 1 0 . 0 1 3 0 9 3 . 0 0 0 0 0 - 0 . 0 7 7 2 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 9 0 0 1 0 . 0 1 3 4 3 3 . 0 0 0 0 0 - 0 . 0 7 7 6 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 9 5 6 4 0 . 0 1 3 8 1 3 . 0 0 0 0 0 - 0 . 0 7 7 9 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 1 . 0 1 1 8 0 . 0 1 4 2 3 3 . 0 0 0 0 0 - 0 . 0 7 8 1 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 0 6 62 0 . 0 1 4 6 9 3 . 0 0 0 0 0 - 0 . 0 7 8 2 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 11 9 3 0 . 0 1 5 2 0 3 . 0 0 0 0 0 - 0 . 0 7 8 1 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1 7 1 1 0 . 0 1 5 7 6 3 . 0 0 0 0 0 - 0 . 0 7 7 8 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 2 2 0 9 0 . 0 1 6 4 0 3 . 0 0 0 0 0 - 0 . 0 7 7 3 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 2 6 82 0 . 0 1 7 1 2 3 . 0 0 0 0 0 - 0 . 0 7 6 5 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 3 0 2 6 0 . 0 1 7 9 6 3 . 0 0 0 0 0 - 0 . 0 7 3 6 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 3 3 4 5 0 . 0 1 92 3 3 . 0 0 0 0 0 - 0 . 0 7 1 2 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 3 6 32 0 . 0 2 0 9 8 3 . 0 0 0 0 0 - 0 . 0 6 9 4 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 3 8 7 5 0 . 0 2 332 3 . 0 0 0 0 0 - 0 . 0 67 9 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 4 0 92 0 . 0 2 6 2 5 3 . 0 0 0 0 0 - 0 . 0 6 6 9 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 4 2 8 1 0 . 0 2 9 7 7 3 . 0 0 0 0 0 - 0 . 0 6 6 4 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 3 3 POL . W2 4 2_1 0_9 ; 3

XFOI L Version 5 . 0

Calculated polar for : FFA-W1 - 2 4 2

1 Reynolds number fixed

xt r f • 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pres sure ) Mach • 0 . 1 5 0 Re - 1 . 0 0 0 e 6 Ncrit '"' 9 . 0 0 0

alpha CL CD Re CCL) CM s xt r P xt r ------- -------- --------- --------- -------- ------- -------- 6 . 5 0 0 0 0 - 0 . 5 7 0 6 0 0 . 0 1 0 6 6 l. 0 0 0 0 0 - 0 . 0 4 9 4 0 0 . 6 0 0 2 0 0 . 4 1 5 0 0 - 6 . 0 0 0 0 0 - 0 . 5 0 3 9 0 0 . 0 1 0 4 8 1 . 0 0 0 0 0 - 0 . 0 5 1 8 0 0 . 5 8 3 2 0 0 . 4 1 9 0 0 - 5 . 5 0 0 0 0 - 0 . 4 3 7 3 0 0 . 0 1 0 2 9 l. 0 0 0 0 0 - 0 . 0 5 4 1 0 0 . 5 7 1 3 0 0 . 42 1 8 0 -5 . 0 0 0 0 0 - 0 . 3 7 0 5 0 0 . 0 1 0 0 8 l. 0 0 0 0 0 - 0 . 0 5 6 6 0 0 . 5 5 7 1 0 0 . 42 5 5 0 - 4 . 5 0 0 0 0 - 0 . 3 0 3 2 0 0 . 0 0 9 8 5 1 . 0 0 0 0 0 - 0 . 0 5 9 1 0 0 . 5 4 3 2 0 0 . 4 3 2 0 0 - 4 . 0 0 0 0 0 - 0 . 2 3 7 2 0 0 . 0 0 9 7 4 1 . 0 0 0 0 0 -o. 0 6 1 1 0 0 . 5 3 1 0 0 0 . 4 3 5 6 0 - 3 . 5 0 0 0 0 - 0 . 17 1 5 0 0 . 0 0 9 6 7 l. 0 0 0 0 0 - 0 . 0 6 3 1 0 0 . 5 1 9 8 0 0 . 4 3 8 5 0 - 3 . 0 0 0 0 0 - 0 . 1 0 6 1 0 0 . 0 0 9 6 4 l. 0 0 0 0 0 - 0 . 0 6 4 9 0 0 . 5 0 5 6 0 0 . 4 4 1 2 0 - 2 . 5 0 0 0 0 - 0 . 0 4 0 1 0 0 . 0 0 9 5 3 1 . 0 0 0 0 0 - 0 . 0 6 7 0 0 0 . 4 9 7 0 0 0 . 4 4 6 5 0 - 2 . 0 0 0 0 0 0 . 02 5 5 0 0 . 0 0 9 4 7 1 . 0 0 0 0 0 - 0 . 0 6 8 9 0 0 . 4 8 4 8 0 0 . 4 5 1 7 0 - 1 . 5 0 0 0 0 0 . 0 9 0 4 0 0 . 0 0 9 4 8 l. 0 0 0 0 0 - 0 . 0 7 0 5 0 0 . 4 7 4 7 0 0 . 4 5 5 1 0 - 1 . 0 0 0 0 0 0 . 1 5 5 1 0 0 . 0 0 95 1 l. 0 0 0 0 0 - 0 . 0 7 2 2 0 0 . 4 6 3 7 0 0 . 4 5 8 1 0 - 0 . 5 0 0 0 0 0 . 2 1 9 5 0 0 . 0 0 9 5 6 1 . 0 0 0 0 0 - 0 . 0 7 3 7 0 0 . 4 5 42 0 0 . 4 6 0 7 0

0 . 0 0 0 0 0 0 . 2 8 4 4 0 0 . 0 0 9 5 5 1 . 0 0 0 0 0 - 0 . 0 7 5 4 0 0 . 4 4 2 9 0 0 . 4 6 6 9 0 0 . 5 0 0 0 0 0 . 3 4 8 7 0 0 . 0 0 9 6 1 1 . 0 0 0 0 0 - 0 . 0 7 6 9 0 0 . 4 3 2 4 0 0 . 4 7 1 5 0 l. 0 0 0 0 . 4 1 1 2 0 . 0 0 9 7 4 1 . 0 0 0 0 0 - 0 . 0 7 8 0 0 . 4 2 2 2 0 . 4 7 3 1 1 . 5 0 0 0 . 4 7 5 2 0 . 0 0 9 8 0 1 . 0 0 0 0 0 - 0 . 0 7 9 5 0 . 4 12 0 0 . 4 7 8 2 2 . 0 0 0 0 . 5 3 8 9 0 . 0 0 9 8 9 1 . 0 0 0 0 0 - 0 . 0 8 0 8 0 . 4 0 1 0 0 . 4 8 3 5 2 . 5 0 0 0 . 6 0 1 8 0 . 0 1 0 0 4 1 . 0 0 0 0 0 - 0 . 0 8 2 0 0 . 3 9 1 4 0 . 4 8 6 9 3 . 0 0 0 0 . 6 6 4 5 0 . 0 1 0 2 2 1 . 0 0 0 0 0 - 0 . 0 8 3 1 0 . 3 7 9 8 0 . 4 8 9 9 3 . 5 0 0 0 . 7 2 6 7 0 . 0 1 0 4 2 1 . 0 0 0 0 0 - 0 . 0 8 4 2 0 . 3 7 0 7 0 . 4 92 6 4 . 0 0 0 0 . 7 8 9 1 0 . 0 1 0 5 9 1 . 0 0 0 0 0 - 0 . 0 8 5 3 0 . 3 5 8 5 0 . 4 9 8 7 4 . 5 0 0 0 . 8 5 0 9 0 . 0 1 0 8 0 1 . 0 0 0 0 0 - 0 . 0 8 6 3 0 . 3 5 0 1 0 . 5 0 3 4 5 . 0 0 0 0 . 9 1 2 0 0 . 0 1 1 0 6 1 . 0 0 0 0 0 - 0 . 0 8 7 1 0 . 3 3 9 3 0 . 5 0 6 8 5 . 5 0 0 0 . 9 7 2 4 0 . 0 1 1 3 6 1 . 0 0 0 0 0 - 0 . 0 8 7 8 0 . 32 9 5 0 . 5 0 9 8 6 . 0 0 0 l. 0 3 2 4 0 . 0 1 1 6 9 l. 0 0 0 0 0 - 0 . 0 8 8 4 0 . 3 1 7 9 0 . 5 12 4 6 . 5 0 0 l. 0 92 1 0 . 0 1 1 9 9 1 . 0 0 0 0 0 - 0 . 0 8 9 0 0 . 3 0 8 6 0 . 5 1 8 7 7 . 0 0 0 1 . 1 5 0 7 0 . 0 1 2 3 8 1 . 0 0 0 0 0 - 0 . 0 8 9 4 0 . 2 95 8 0 . 52 3 5 7 . 5 0 0 1 . 2 0 8 2 0 . 0 1 2 8 1 1 . 0 0 0 0 0 - 0 . 0 8 9 6 0 . 2 8 7 2 0 . 52 6 7 8 . 0 0 0 1 . 2 6 4 4 0 . 0 1 3 3 1 1 . 0 0 0 0 0 - 0 . 0 8 9 6 0 . 2 7 3 3 0 . 52 9 7 8 . 5 0 0 1 . 3 1 92 0 . 0 1 3 8 7 l. 0 0 0 0 0 - 0 . 0 8 9 4 0 . 2 6 1 2 0 . 5 3 2 3 9 . 0 0 0 1 . 37 1 9 0 . 0 1 4 53 1 . 0 0 0 0 0 - 0 . 0 8 9 0 0 . 2 4 5 7 0 . 5 3 9 3 9 . 5 0 0 1 . 4 2 3 1 0 . 0 1 5 2 3 1 . 0 0 0 0 0 - 0 . 0 8 8 3 0 . 2 3 2 6 0 . 5 4 3 5

1 0 . 0 0 0 1 . 4 7 1 6 0 . 0 1 6 0 3 1 . 0 0 0 0 0 - 0 . 0 8 7 2 0 . 2 1 95 0 . 5 4 6 7 1 0 . 5 0 0 l. 5 1 4 0 0 . 0 1 7 0 9 l. 0 0 0 0 0 - 0 . 0 8 5 3 0 . 2 0 5 9 0 . 5 4 9 6 1 1 . 0 0 0 l. 5 4 3 6 0 . 0 1 8 1 8 1 . 0 0 0 0 0 - 0 . 0 8 1 3 0 . 1 9 3 4 0 . 5 5 3 2 1 1 . 5 0 0 1 . 5 6 9 5 0 . 0 1 97 4 1 . 0 0 0 0 0 - 0 . 0 7 7 6 0 . 1 8 0 7 0 . 5 5 9 0 12 . 0 0 0 1 . 5 8 8 2 0 . 0 2 2 0 1 1 . 0 0 0 0 0 - 0 . 0 7 4 0 0 . 1 7 1 1 0 . 5 6 2 8 1 2 . 5 0 0 1 . 6 0 1 2 0 . 0 2 5 1 1 1 . 0 0 0 0 0 - 0 . 0 7 1 2 0 . 1 5 7 3 0 . 5 6 5 7 1 3 . 0 0 0 1 . 6 0 6 4 0 . 02 9 4 8 1 . 0 0 0 0 0 - 0 . 0 6 9 4 0 . 1 4 8 1 0 . 5 6 8 3 1 3 . 5 0 0 1 . 6 0 8 8 0 . 0 3 4 8 1 1 . 0 0 0 0 0 - 0 . 0 6 8 7 0 . 1 3 6 3 0 . 57 0 5 1 4 . 0 0 0 1 . 6 0 2 1 0 . 0 4 1 7 7 1 . 0 0 0 0 0 - 0 . 0 6 9 0 0 . 12 0 5 0 . 5 7 5 8 1 4 . 5 0 0 1 . 5 9 3 3 0 . 0 4 9 3 8 1 . 0 0 0 0 0 - 0 . 0 6 9 7 0 . 1 1 2 4 0 . 5 7 9 7 1 5 . 0 0 0 1 . 5 8 5 9 0 . 0 5 7 2 5 l. 0 0 0 0 0 - 0 . 0 7 0 8 0 . 1 0 0 9 0 . 5 8 2 3 1 5 . 5 0 0 1 . 57 3 6 0 . 0 6 6 0 5 1 . 0 0 0 0 0 - 0 . 0 7 2 4 0 . 0 92 1 0 . 5 8 4 6 1 6 . 0 0 0 1 . 5 6 4 2 0 . 0 7 4 7 4 1 . 0 0 0 0 0 - 0 . 0 7 4 0 0 . 0 8 3 3 0 . 5 8 67 1 6 . 5 0 0 1 . 55 0 9 0 . 0 8 4 4 4 1 . 0 0 0 0 0 - 0 . 0 7 6 3 0 . 0 7 7 0 0 . 5 8 8 6 1 7 . 0 0 0 1 . 5 4 3 1 0 . 0 9 3 5 8 1 . 0 0 0 0 0 - 0 . 0 7 8 5 0 . 0 6 8 3 0 . 5 9 1 1 1 7 . 5 0 0 1 . 53 2 8 0 . 1 0 3�1 1 . 0 0 0 0 0 - 0 . 0 8 1 3 0 . 0 6 5 2 0 . 5 9 5 7 1 8 . 0 0 0 1 . 52 2 5 0 . 1 1 3 8 1 . 0 0 0 0 0 - 0 . 0 8 4 3 0 . 0 6 0 5 0 . 5 9 9 0

FFA TN 1 9 9 0 - 1 5 3 4 POL . W2 4 2_1 0_TU1 ; 3

XFOIL Ver s ion 5 . 0

Calculated polar for : FFA-W1-2 42

1 Reynolds number fixed

xt rf • 0 . 0 1 0 ( suct ion) 0 . 1 0 0 (pre ssure ) Mach - 0 . 1 5 0 Re "" 1 . 0 0 0 e 6 Ncrit .. 9 . 0 0 0

alpha CL CD Re (CL) CM S xt r P xt r - - - - - - - -------- --------- - - ----- - - -------- ------- ------ -

1 . 0 0 0 0 . 3 5 0 2 0 . 0 1 6 1 5 1 . 0 0 0 0 0 - 0 . 0 6 35 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 4 1 4 6 0 . 0 1 6 1 7 1 . 0 0 0 0 0 - 0 . 0 6 5 7 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 4 7 8 2 0 . 0 1 62 4 1 . 0 0 0 0 0 - 0 . 0 67 7 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 5 4 0 9 0 . 0 1 6 37 1 . 0 0 0 0 0 - 0 . 0 6 9 4 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 0 2 7 0 . 0 1 6 5 5 1 . 0 0 0 0 0 - o . 0 1 1 0 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 6 6 3 6 0 . 0 1 6 7 8 1. 0 0 0 0 0 - 0 . 0 7 2 3 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 7 2 3 5 0 . 0 1 7 0 6 1 . 0 0 0 0 0 - 0 . 0 7 3 4 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 7 8 2 3 0 . 0 1 7 3 9 1 . 0 0 0 0 0 - 0 . 0 7 4 4 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 8 3 9 8 0 . 0 1 7 7 8 1 . 0 0 0 0 0 - 0 . 0 7 5 1 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 8 9 6 0 0 . 0 1 8 2 2 1 . 0 0 0 0 0 - 0 . 0 7 5 6 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 9 5 0 6 0 . 0 1 8 7 4 1 . 0 0 0 0 0 - 0 . 0 7 5 8 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 0 0 33 0 . 0 1 932 1 . 0 0 0 0 0 - 0 . 0 7 5 8 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 0 5 3 7 0 . 02 0 0 0 1 . 0 0 0 0 0 - 0 . 0 7 5 4 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1 0 1 0 0 . 0 2 0 7 8 1 . 0 0 0 0 0 - 0 . 0 7 4 6 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 1 3 3 1 0 . 0 2 1 6 9 1 . 0 0 0 0 0 - 0 . 0 7 1 4 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 1 6 3 8 0 . 0 2 3 0 1 1 . 0 0 0 0 0 - 0 . 0 6 8 7 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 1 9 4 1 0 . 0 2 4 7 7 1 . 0 0 0 0 0 - 0 . 0 6 6 9 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 2 1 9 9 0 . 0 2 7 1 1 1 . 0 0 0 0 0 - 0 . 0 6 5 5 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 2 4 2 5 0 . 0 3 0 1 0 1 . 0 0 0 0 0 - 0 . 0 6 4 8 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 2 62 8 0 . 0 3 3 7 5 1 . 0 0 0 0 0 - 0 . 0 6 4 8 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 2 8 0 7 0 . 0 3 8 0 0 1 . 0 0 0 0 0 - 0 . 0 6 52 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 2 9 6 7 0 . 0 4 2 7 6 1 . 0 0 0 0 0 - 0 . 0 6 5 9 0 . 0 1 0 0 0 . 1 0 0 0 12 . 0 0 0 1 . 3 1 0 5 0 . 0 4 8 0 1 1 . 0 0 0 0 0 - 0 . 0 6 6 9 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 32 2 4 0 . 0 5 3 6 3 1 . 0 0 0 0 0 - 0 . 0 6 8 0 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 332 6 0 . 0 5 9 7 0 1 . 0 0 0 0 0 - 0 . 0 6 9 4 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 3 4 1 5 0 . 0 6 6 0 5 1 . 0 0 0 0 0 - 0 . 0 7 0 8 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 3 4 8 8 0 . 0 7 2 7 5 1 . 0 0 0 0 0 - 0 . 0 7 2 4 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 3 5 4 7 0 . 0 7 9 8 8 1 . 0 0 0 0 0 - 0 . 0 7 4 2 0 . 0 1 0 0 0 . 1 0 0 0 15 . 0 0 0 1 . 3 5 9 7 0 . 0 8 7 3 1 1 . 0 0 0 0 0 - 0 . 0 7 6 1 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 3 5 POL . W2 42_2 0_9 ; 3

XFOIL Ve rsion 5 . 0

Calculated pol a r for : FFA-W1 - 2 4 2

1 Reynolds numbe r f ixed

xt r f • 1 . 0 0 0 ( s uct ion ) 1 . 0 0 0 (pressure ) Mach - 0 . 1 5 0 Re = 2 . 0 0 0 e 6 Nc rit = 9 . 0 0 0

alpha CL CD Re (CL) CM S xt r P xt r - - -- - -- -------- --------- --- ------ -------- --- ---- - ------- 9 . 0 0 0 0 0 - 0 . 9 1 0 3 0 0 . 0 1 3 3 2 2 . 0 0 0 0 0 - 0 . 0 3 1 6 0 0 . 6 3 9 2 0 0 . 3 0 5 6 0 - 8 . 5 0 0 0 0 - 0 . 8 2 3 5 0 0 . 0 0 9 8 4 2 . 0 0 0 0 0 - 0 . 0 4 4 6 0 0 . 6 2 0 5 0 0 . 3 6 0 4 0 - 8 . 0 0 0 0 0 - 0 . 7 5 4 0 0 0 . 0 0 92 6 2 . 0 0 0 0 0 - 0 . 0 4 8 1 0 0 . 6 0 1 8 0 0 . 3 7 0 9 0 - 7 . 5 0 0 0 0 - 0 . 6 8 6 0 0 0 . 0 0 8 8 8 2 . 0 0 0 0 0 - 0 . 0 5 1 0 0 0 . 5 8 6 8 0 0 . 3 8 2 1 0 - 7 . 0 0 0 0 0 - 0 . 6 1 9 0 0 0 . 0 0 8 6 1 2 . 0 0 0 0 0 - 0 . 0 5 3 4 0 0 . 57 2 6 0 0 . 3 9 0 9 0 - 6 . 5 0 0 0 0 - 0 . 5 5 2 2 0 0 . 0 0 8 4 0 2 . 0 0 0 0 0 - 0 . 0 5 5 7 0 0 . 5 5 9 2 0 0 . 3 9 8 7 0 - 6 . 0 0 0 0 0 - 0 . 4 8 6 8 0 0 . 0 0 8 3 2 2 . 0 0 0 0 0 - 0 . 0 5 7 5 0 0 . 5 4 3 5 0 0 . 4 0 4 0 0 - 5 . 5 0 0 0 0 - 0 . 42 0 1 0 0 . 0 0 8 1 3 2 . 0 0 0 0 0 - 0 . 0 5 9 8 0 0 . 53 3 0 0 0 . 4 0 9 1 0 - 5 . 0 0 0 0 0 - 0 . 3 5 3 8 0 0 . 0 0 8 0 1 2 . 0 0 0 0 0 - 0 . 0 6 1 8 0 0 . 52 0 1 0 0 . 4 1 4 3 0 - 4 . 5 0 0 0 0 - 0 . 2 8 8 0 0 0 . 0 0 7 9 2 2 . 0 0 0 0 0 - 0 . 0 6 3 7 0 0 . 5 0 62 0 0 . 4 1 8 0 0 - 4 . 0 0 0 0 0 - 0 . 2 2 2 5 0 0 . 0 0 7 8 7 2 . 0 0 0 0 0 - 0 . 0 6 5 5 0 0 . 4 9 8 8 0 0 . 42 0 9 0 -3 . 5 0 0 0 0 - 0 . 1 5 7 3 0 0 . 0 0 7 8 5 2 . 0 0 0 0 0 - 0 . 0 6 7 2 0 0 . 4 8 4 9 0 0 . 4 2 2 9 0 -3 . 0 0 0 0 0 - 0 . 0 9 1 6 0 0 . 0 0 7 7 8 2 . 0 0 0 0 0 - 0 . 0 6 9 0 0 0 . 4 7 6 5 0 0 . 4 2 7 7 0 -2 . 5 0 0 0 0 - 0 . 0 2 6 2 0 0 . 0 0 7 7 4 2 . 0 0 0 0 0 - 0 . 0 7 0 8 0 0 . 4 6 5 1 0 0 . 4 3 3 2 0 -2 . 0 0 0 0 0 0 . 0 3 8 8 0 0 . 0 0 7 7 4 2 . 0 0 0 0 0 - 0 . 0 7 2 5 0 0 . 4 5 4 6 0 0 . 4 3 7 0 0 - 1 . 5 0 0 0 0 0 . 1 0 3 6 0 0 . 0 0 7 7 6 2 . 0 0 0 0 0 - 0 . 0 7 4 0 0 0 . 4 4 4 6 0 0 . 4 4 0 2 0 - 1 . 0 0 0 0 0 0 . 1 6 8 1 0 0 . 0 0 7 8 1 2 . 0 0 0 0 0 - 0 . 0 7 5 5 0 0 . 4 3 3 1 0 0 . 4 4 2 2 0 - 0 . 5 0 0 0 0 0 . 2 3 3 0 0 0 . 0 0 7 8 1 2 . 0 0 0 0 0 - 0 . 0 7 7 1 0 0 . 4 2 4 3 0 0 . 4 4 8 0 0

0 . 0 0 0 0 0 0 . 2 9 7 5 0 0 . 0 0 7 8 6 2 . 0 0 0 0 0 - 0 . 0 7 8 7 0 0 . 4 1 1 8 0 0 . 4 5 3 3 0 0 . 5 0 0 0 0 0 . 3 6 1 7 0 0 . 0 0 7 92 2 . 0 0 0 0 0 - 0 . 0 8 0 1 0 0 . 4 0 4 0 0 0 . 4 5 7 3 0 1 . 0 0 0 0 . 4 2 5 6 0 . 0 0 8 0 3 2 . 0 0 0 0 0 - 0 . 0 8 1 4 0 . 3 9 0 5 0 . 4 5 9 8 1 . 5 0 0 0 . 4 8 9 4 0 . 0 0 8 1 3 2 . 0 0 0 0 0 - 0 . 0 8 2 7 0 . 3 8 3 7 0 . 4 6 2 7 2 . 0 0 0 0 . 5 5 3 4 0 . 0 0 8 2 1 2 . 0 0 0 0 0 - 0 . 0 8 4 1 0 . 3 7 1 8 0 . 4 6 9 2 2 . 5 0 0 0 . 6 1 6 7 0 . 0 0 8 3 5 2 . 0 0 0 0 0 - 0 . 0 8 5 4 0 . 3 6 3 4 0 . 4 7 3 7 3 . 0 0 0 0 . 6 7 9 9 0 . 0 0 8 4 9 2 . 0 0 0 0 0 - 0 . 0 8 6 5 0 . 3 5 0 6 0 . 4 7 7 2 3 . 5 0 0 0 . 7 4 2 5 0 . 0 0 8 6 9 2 . 0 0 0 0 0 - 0 . 0 8 7 6 0 . 3 4 3 0 0 . 4 7 9 5 4 . 0 0 0 0 . 8 0 52 0 . 0 0 8 8 5 2 . 0 0 0 0 0 - 0 . 0 8 8 7 0 . 3 3 0 5 0 . 4 8 42 4 . 5 0 0 0 . 8 6 7 5 0 . 0 0 9 0 5 2 . 0 0 0 0 0 - 0 . 0 8 9 7 0 . 32 2 5 0 . 4 8 9 8 5 . 0 0 0 0 . 92 9 5 0 . 0 0 92 7 2 . 0 0 0 0 0 - 0 . 0 9 0 6 0 . 3 1 0 5 0 . 4 9 3 6 5 . 5 0 0 0 . 9 9 0 7 0 . 0 0 9 5 4 2 . 0 0 0 0 0 - 0 . 0 9 1 4 0 . 3 0 1 8 0 . 4 9 6 4 6 . 0 0 0 1 . 0 5 1 6 0 . 0 0 9 8 1 2 . 0 0 0 0 0 - 0 . 0 92 1 0 . 2 9 0 5 0 . 4 9 8 9 6 . 5 0 0 1 . 1 1 2 0 0 . 0 1 0 1 1 2 . 0 0 0 0 0 - 0 . 0 92 8 0 . 2 8 0 1 0 . 5 0 4 8 7 . 0 0 0 1 . 1 7 2 1 0 . 0 1 0 4 2 2 . 0 0 0 0 0 - 0 . 0 9 3 4 0 . 2 6 9 9 0 . 5 0 9 8 7 . 5 0 0 1 . 2 3 0 8 0 . 0 1 0 8 2 2 . 0 0 0 0 0 - 0 . 0 9 3 8 0 . 2 5 62 0 . 5 1 3 3 8 . 0 0 0 1 . 2 8 7 5 0 . 0 1 1 3 5 2 . 0 0 0 0 0 - 0 . 0 9 3 9 0 . 2 4 1 0 0 . 5 1 5 9 8 . 5 0 0 1 . 3 4 3 1 0 . 0 1 1 9 3 2 . 0 0 0 0 0 - 0 . 0 9 3 7 0 . 2 2 62 0 . 5 1 8 0 9 . 0 0 0 1 . 3 9 8 9 0 . 0 1 2 4 4 2 . 0 0 0 0 0 - 0 . 0 9 3 7 0 . 2 1 2 6 0 . 52 5 4 9 . 5 0 0 1 . 45 2 6 0 . 0 1 3 0 5 2 . 0 0 0 0 0 - 0 . 0 9 3 3 0 . 1 9 9 6 0 . 52 9 8

1 0 . 0 0 0 1 . 5 0 1 9 0 . 0 1 3 9 1 2 . 0 0 0 0 0 - 0 . 0 92 3 0 . 1 8 3 2 0 . 5 32 9 1 0 . 5 0 0 1 . 5 4 9 7 0 . 0 1 4 7 7 2 . 0 0 0 0 0 - 0 . 0 9 1 0 0 . 1 7 1 1 0 . 5 3 5 4 1 1 . 0 0 0 1 . 5 9 4 3 0 . 0 1 57 2 2 . 0 0 0 0 0 - 0 . 0 8 9 4 0 . 1 5 62 0 . 5 3 93 1 1 . 5 0 0 1 . 62 7 4 0 . 0 1 6 8 6 2 . 0 0 0 0 0 - 0 . 0 8 5 9 0 . 1 42 2 0 . 5 4 5 7 12 . 0 0 0 1 . 64 2 4 0 . 0 1 8 6 5 2 . 0 0 0 0 0 - 0 . 0 8 0 3 0 . 1 3 2 5 0 . 5 4 9 3 12 . 5 0 0 1 . 6 5 7 9 0 . 0 2 1 0 1 2 . 0 0 0 0 0 - 0 . 0 7 6 3 0 . 1 1 9 1 0 . 5 5 2 0 1 3 . 0 0 0 1 . 6 6 4 9 0 . 02 4 4 9 2 . 0 0 0 0 0 - 0 . 0 7 3 0 0 . 1 0 6 4 0 . 5 5 4 1 1 3 . 5 0 0 1 . 6 62 3 0 . 0 2 9 62 2 . 0 0 0 0 0 - 0 . 0 7 1 1 0 . 0 9 8 1 0 . 5 5 7 2 1 4 . 0 0 0 1 . 6 5 4 6 0 . 0 3 6 1 5 2 . 0 0 0 0 0 - 0 . 0 7 0 6 0 . 0 8 4 1 0 . 5 63 0 1 4 . 5 0 0 1 . 6 4 8 4 0 . 0 4 3 2 4 2 . 0 0 0 0 0 - 0 . 0 7 1 0 0 . 0 7 62 0 . 5 6 6 4 1 5 . 0 0 0 1 . 6 4 5 0 0 . 0 5 0 3 5 2 . 0 0 0 0 0 - 0 . 0 7 1 7 0 . 0 6 8 2 0 . 5 6 9 1

FFA TN 1 9 9 0 - 1 5 3 6

XFOIL Vers ion 5 . 0

Calculated polar for : FFA-W1 -242

1 Reynolds number fixed

xt rf • 1 . 0 0 0 ( suction) 1 . 0 0 0 (pres sure ) Mach ..

alpha - - - - - - -- 8 . 5 0 0 0 0 - 8 . 0 0 0 0 0 -7 . 5 0 0 0 0 - 7 . 0 0 0 0 0 - 6 . 5 0 0 0 0 - 6 . 0 0 0 0 0 - 5 . 5 0 0 0 0 - 5 . 0 0 0 0 0 - 4 . 5 0 0 0 0 - 4 . 0 0 0 0 0 - 3 . 5 0 0 0 0 - 3 . 0 0 0 0 0 -2 . 5 0 0 0 0 - 2 . 0 0 0 0 0 - 1 . 5 0 0 0 0 - 1 . 0 0 0 0 0 - 0 . 5 0 0 0 0

0 . 0 0 0 0 0 0 . 5 0 0 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 50 0

0 . 1 5 0

CL --------

- 0 . 8 1 7 4 0 - 0 . 7 4 6 7 0 - 0 . 6 7 8 5 0 - 0 . 6 1 1 7 0 - 0 . 5 4 6 0 0 - o .. 4 7 9 7 0 - 0 . 4 1 3 9 0 - 0 . 3 4 8 5 0 - 0 . 2 8 3 2 0 - 0 . 2 1 8 2 0 - 0 . 1 5 2 7 0 - 0 . 0 8 7 4 0 - 0 . 0 2 2 4 0

0 . 0 4 2 4 0 0 . 1 0 7 1 0 0 . 1 7 1 6 0 0 . 2 3 6 2 0 0 . 3 0 0 7 0 0 . 3 6 5 0 0

0 . 4 2 7 3 0 . 4 9 1 1 0 . 5 5 4 7 0 . 6 1 7 9 0 . 6 8 1 1 0 . 7 4 4 2 0 . 8 0 6 8 0 . 8 6 9 1 0 . 9 3 12 0 . 9 92 5 1 . 0 5 4 1 1 . 1 1 4 4 1 . 1 7 4 9 1 . 2 32 9 1 . 2 8 9 7 1 . 3 4 7 5 1 . 4 0 32 1 . 4 57 9 1 . 5 0 7 8 1 . 5 5 6 9 1. 6 0 0 1 1 . 6 3 92 1 . 6 5 5 9 1. 6 6 6 3 1 . 6 7 8 3 1 . 6 7 5 6

Re =

CD ---------

0 . 0 0 9 0 7 0 . 0 0 8 32 0 . 0 0 7 8 6 0 . 0 0 7 6 1 0 . 0 0 7 4 8 0 . 0 0 7 3 0 0 . 0 0 7 1 8 0 . 0 0 7 12 0 . 0 0 7 0 8 0 . 0 0 7 0 7 0 . 0 0 7 0 1 0 . 0 0 6 97 0 . 0 0 6 9 7 0 . 0 0 6 9 7 0 . 0 0 7 0 0 0 . 0 0 7 0 4 0 . 0 0 7 0 7 0 . 0 0 7 1 2 0 . 0 0 7 1 8

0 . 0 0 7 2 8 0 . 0 0 7 3 8 0 . 0 0 7 4 8 0 . 0 0 7 6 2 0 . 0 0 7 7 6 0 . 0 0 7 9 0 0 . 0 0 8 0 8 0 . 0 0 8 2 7 0 . 0 0 8 4 7 0 . 0 0 8 7 4 0 . 0 0 8 9 6 0 . 0 0 92 8 0 . 0 0 9 5 6 0 . 0 1 0 0 4 0 . 0 1 0 5 9 0 . 0 1 1 0 1 0 . 0 1 1 5 6 0 . 0 1 2 1 2 0 . 0 1 2 9 7 0 . 0 1 3 7 9 0 . 0 1 4 8 7 0 . 0 1 5 9 3 0 . 0 1 7 4 4 0 . 0 1 9 8 2 0 . 02 2 6 6 0 . 0 2 7 3 9

3 . 0 0 0 e 6 Ncrit = 9 . 0 0 0

Re (CL) CM S xt r P xtr --------- -------- - - ----- -------

3 . 0 0 0 0 0 - 0 . 0 4 6 6 0 0 . 5 9 6 7 0 0 . 32 9 7 0 3 . 0 0 0 0 0 - 0 . 0 5 0 7 0 0 . 5 7 9 0 0 0 . 3 5 3 9 0 3 . 0 0 0 0 0 - 0 . 0 5 3 6 0 0 . 5 62 5 0 0 . 3 6 8 3 0 3 . 0 0 0 0 0 - 0 . 0 5 5 9 0 0 . 5 5 3 1 0 0 . 3 8 1 8 0 3 . 0 0 0 0 0 - 0 . 0 5 7 8 0 0 . 5 3 5 1 0 0 . 3 8 7 2 0 3 . 0 0 0 0 0 - 0 . 0 5 9 9 0 0 . 5 2 7 2 0 0 . 3 9 7 8 0 3 . 0 0 0 0 0 - 0 . 0 6 1 8 0 0 . 5 11 7 0 0 . 4 0 5 0 0 3 . 0 0 0 0 0 - 0 . 0 6 3 5 0 0 . 5 0 32 0 0 . 4 0 7 7 0 3 . 0 0 0 0 0 - 0 . 0 6 5 2 0 0 . 4 8 8 9 0 0 . 4 0 9 5 0 3 . 0 0 0 0 0 - 0 . 0 6 6 8 0 0 . 4 8 2 2 0 0 . 4 1 0 8 0 3 . 0 0 0 0 0 - 0 . 0 6 8 6 0 0 . 4 6 8 0 0 0 . 4 1 7 3 0 3 . 0 0 0 0 0 - 0 . 0 7 0 3 0 0 . 4 5 9 7 0 0 . 4 2 2 7 0 3 . 0 0 0 0 0 - 0 . 0 7 1 9 0 0 . 4 5 0 8 0 0 . 4 2 7 2 0 3 . 0 0 0 0 0 - 0 . 0 7 3 5 0 0 . 4 3 7 3 0 0 . 4 3 0 2 0 3 . 0 0 0 0 0 - 0 . 0 7 5 0 0 0 . 4 3 0 5 0 0 . 4 3 2 5 0 3 . 0 0 0 0 0 - 0 . 0 7 6 4 0 0 . 4 1 7 7 0 0 . 4 3 4 1 0 3 . 0 0 0 0 0 - 0 . 0 7 8 0 0 0 . 4 0 9 3 0 0 . 4 4 0 3 0 3 . 0 0 0 0 0 - 0 . 0 7 9 4 0 0 . 3 9 8 6 0 0 . 4 4 6 3 0 3 . 0 0 0 0 0 - 0 . 0 8 0 9 0 0 . 3 8 8 8 0 0 . 4 5 0 9 0 3 . 0 0 0 0 0 - 0 . 0 8 1 9 0 . 3 8 0 0 0 . 4 5 3 6 3 . 0 0 0 0 0 - 0 . 0 8 32 0 . 3 6 4 9 0 . 4 5 8 8 3 . 0 0 0 0 0 - 0 . 0 8 4 5 0 . 3 5 92 0 . 4 6 1 6 3 . 0 0 0 0 0 - 0 . 0 8 5 7 0 . 3 4 4 2 0 . 4 6 3 6 3 . 0 0 0 0 0 - 0 . 0 8 6 9 0 . 3 3 8 3 0 . 4 6 7 6 3 . 0 0 0 0 0 - 0 . 0 8 8 0 0 . 3 2 7 9 0 . 4 7 3 9 3 . 0 0 0 0 0 - 0 . 0 8 9 1 0 . 3 1 7 2 0 . 4 7 8 8 3 . 0 0 0 0 0 - 0 . 0 9 0 1 0 . 3 0 8 2 0 . 4 8 2 6 3 . 0 0 0 0 0 - 0 . 0 9 1 0 0 . 2 97 1 0 . 4 8 4 7 3 . 0 0 0 0 0 - 0 . 0 9 1 8 0 . 2 8 8 1 0 . 4 8 6 8 3 . 0 0 0 0 0 - 0 . 0 92 6 0 . 2 7 5 3 0 . 4 9 3 3 3 . 0 0 0 0 0 - 0 . 0 9 3 3 0 . 2 6 6 5 0 . 4 9 8 6 3 . 0 0 0 0 0 - 0 . 0 9 3 9 0 . 2 52 9 0 . 5 0 2 3 3 . 0 0 0 0 0 - 0 . 0 9 42 0 . 2 3 4 5 0 . 5 0 5 0 3 . 0 0 0 0 0 - 0 . 0 9 4 3 0 . 22 0 3 0 . 5 0 7 2 3 . 0 0 0 0 0 - 0 . 0 9 4 5 0 . 2 0 7 0 0 . 5 12 0 3 . 0 0 0 0 0 - 0 . 0 9 4 4 0 . 1 9 5 2 0 . 5 1 7 8 3 . 0 0 0 0 0 - 0 . 0 9 4 1 0 . 1 8 3 3 0 . 52 2 3 3 . 0 0 0 0 0 - 0 . 0 9 3 2 0 . 1 62 8 0 . 52 5 3 3 . 0 0 0 0 0 - 0 . 0 92 1 0 . 1 4 7 9 0 . 52 7 7 3 . 0 0 0 0 0 - 0 . 0 9 02 0 . 1 3 5 3 0 . 53 0 7 3 . 0 0 0 0 0 - 0 . 0 8 7 7 0 . 1 1 9 7 0 . 53 7 0 3 . 0 0 0 0 0 - 0 . 0 8 1 8 0 . 1 0 6 3 0 . 5 4 1 8 3 . 0 0 0 0 0 - 0 . 0 7 6 7 0 . 0 9 62 0 . 5 4 5 1 3 . 0 0 0 0 0 - 0 . 0 7 32 0 . 0 8 3 0 0 . 5 4 7 7 3 . 0 0 0 0 0 - 0 . 0 7 0 6 0 . 0 7 6 8 0 . 5 4 9 5

POL . W2 4 2_30_9 ; 3

FFA TN 1 9 9 0 - 1 5 3 7 POL . W2 4 2_3 0_TU1 ; 2

XFO I L Vers ion 5 . 0

Cal culated polar for : FFA-W1-2 42

1 Reynolds numbe r fixed

xt r f • 0 . 0 1 0 ( s uction ) 0 . 1 0 0 (pres sure ) Mach • 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncrit -= 9 . 0 0 0

alpha CL CD Re (CL) CM s xt r P xt r - - - - - - - - --- ---- -- ------- - -- ---- -- -- - ----- --- - --- - - - - ---

1 . 0 0 0 0 . 3 8 0 7 0 . 0 1 3 0 6 3 . 0 0 0 0 0 - 0 . 0 7 1 0 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 4 4 4 4 0 . 0 1 3 1 3 3 . 0 0 0 0 0 - 0 . 0 7 2 7 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 5 0 7 6 0 . 0 1 3 2 3 3 . 0 0 0 0 0 - 0 . 0 7 4 2 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 5 7 02 0 . 0 1 3 3 6 3 . 0 0 0 0 0 - 0 . 0 7 5 7 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 3 2 3 0 . 0 1 3 5 3 3 . 0 0 0 0 0 - 0 . 0 7 7 0 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 6 9 3 8 0 . 0 1 3 7 2 3 . 0 0 0 0 0 - 0 . 0 7 8 2 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 7 5 4 6 0 . 0 1 3 9 5 3 . 0 0 0 0 0 - 0 . 0 7 92 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 8 1 4 8 0 . 0 1 4 2 1 3 . 0 0 0 0 0 - 0 . 0 8 0 1 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 8 7 4 2 0 . 0 1 4 5 2 3 . 0 0 0 0 0 - 0 . 0 8 0 9 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 9 32 7 0 . 0 1 4 8 5 3 . 0 0 0 0 0 - 0 . 0 8 1 5 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 9 9 0 2 0 . 0 1 5 2 3 3 . 0 0 0 0 0 - 0 . 0 8 2 0 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 0 4 6 7 0 . 0 1 5 6 5 3 . 0 0 0 0 0 - 0 . 0 8 2 3 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 1 0 1 8 0 . 0 1 6 1 2 3 . 0 0 0 0 0 - 0 . 0 8 2 3 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1 5 5 5 0 . 0 1 6 6 4 3 . 0 0 0 0 0 - 0 . 0 8 2 2 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 2 0 7 3 0 . 0 1 7 2 3 3 . 0 0 0 0 0 - 0 . 0 8 1 8 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 2 5 6 8 0 . 0 1 7 8 9 3 . 0 0 0 0 0 - 0 . 0 8 1 0 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 3 0 2 7 0 . 0 1 8 6 4 3 . 0 0 0 0 0 - 0 . 0 7 9 8 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 32 6 8 0 . 0 1 9 5 8 3 . 0 0 0 0 0 - 0 . 0 7 4 9 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 3 57 6 0 . 02 0 9 4 3 . 0 0 0 0 0 -o. 0 7 2 1 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 3 8 3 8 0 . 0 2 2 7 6 3 . 0 0 0 0 0 - 0 . 0 6 9 6 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 4 0 5 1 0 . 0 2 5 2 3 3 . 0 0 0 0 0 - 0 . 0 6 7 5 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 4 2 4 2 0 . 0 2 8 3 9 3 . 0 0 0 0 0 - 0 . 0 6 63 0 . 0 1 0 0 0 . 1 0 0 0 12 . 0 0 0 1 . 4 4 0 4 0 . 0 3 2 2 8 3 . 0 0 0 0 0 - 0 . 0 6 5 9 0 . 0 1 0 0 0 . 1 0 0 0 12 . 5 0 0 1 . 4 5 4 4 0 . 0 3 6 8 0 3 . 0 0 0 0 0 - 0 . 0 6 6 0 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 4 6 7 3 0 . 0 4 1 8 1 3 . 0 0 0 0 0 - 0 . 0 6 6 5 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 4 7 8 5 0 . 0 4 7 2 4 3 . 0 0 0 0 0 - 0 . 0 6 7 3 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 3 8

XFOI L Vers ion 5 . 0

Calculated polar for : FFA-W1 - 2 7 1

1 Reynolds number fixed

xt rf • 1 . 0 0 0 ( suction) l. 0 0 0 (pres sure ) Mach • 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it

alpha CL CD Re (CL) CM - -- ---- -------- ------ - -- - -------- --------- 7 . 0 0 0 0 0 - 0 . 7 2 1 4 0 0 . 0 1 512 l . 0 0 0 0 0 - 0 . 0 3 1 2 0 - 6 . 5 0 0 0 0 - 0 . 6 5 0 0 0 0 . 0 1 4 32 l. 0 0 0 0 0 - 0 . 0 3 6 1 0 - 6 . 0 0 0 0 0 - 0 . 5 7 8 0 0 0 . 0 1 3 7 1 l. 0 0 0 0 0 - 0 . 0 4 0 7 0 - 5 . 5 0 0 0 0 - 0 . 5 0 6 1 0 0 . 0 1 32 2 1 . 0 0 0 0 0 - 0 . 0 4 4 9 0 - 5 . 0 0 0 0 0 - 0 . 4 3 4 5 0 0 . 0 1 2 8 3 1 . 0 0 0 0 0 - 0 . 0 4 8 9 0 - 4 . 5 0 0 0 0 - 0 . 3 5 9 4 0 0 . 0 12 2 0 1 . 0 0 0 0 0 - 0 . 0 5 4 1 0 - 4 . 0 0 0 0 0 - 0 . 2 8 6 2 0 0 . 0 1 1 7 8 1 . 0 0 0 0 0 - 0 . 0 5 8 4 0 - 3 . 5 0 0 0 0 - 0 . 2 1 5 6 0 0 . 0 1 1 5 6 1 . 0 0 0 0 0 - 0 . 0 6 1 7 0 - 3 . 0 0 0 0 0 - 0 . 1 4 6 4 0 0 . 0 1 1 4 3 1 . 0 0 0 0 0 - 0 . 0 6 4 6 0 - 2 . 5 0 0 0 0 - 0 . 0 7 7 7 0 0 . 0 1 1 3 5 1 . 0 0 0 0 0 - 0 . 0 6 7 2 0 - 2 . 0 0 0 0 0 - 0 . 0 1 0 0 0 0 . 0 1 1 3 4 1 . 0 0 0 0 0 - 0 . 0 6 9 6 0 - 1 . 5 0 0 0 0 0 . 0 6 0 0 0 0 . 0 1 1 1 3 1 . 0 0 0 0 0 - 0 . 0 72 7 0 - 1 . 0 0 0 0 0 0 . 1 2 8 4 0 0 . 0 1 1 0 5 1 . 0 0 0 0 0 - 0 . 0 7 5 3 0 - 0 . 5 0 0 0 0 0 . 1 9 5 7 0 0 . 0 1 1 0 7 1 . 0 0 0 0 0 - 0 . 0 7 7 5 0

0 . 0 0 0 0 0 0 . 2 6 2 5 0 0 . 0 1 1 0 9 1 . 0 0 0 0 0 - 0 . 0 7 9 6 0 1 . 0 0 0 0 . 3 9 4 8 0 . 0 1 1 1 7 1 . 0 0 0 0 0 - 0 . 0 8 3 4 1 . 5 0 0 0 . 4 6 0 6 0 . 0 1 12 7 1 . 0 0 0 0 0 - 0 . 0 8 5 2 2 . 0 0 0 0 . 5 2 5 9 0 . 0 1 1 3 9 1 . 0 0 0 0 0 - 0 . 0 8 6 9 2 . 5 0 0 0 . 5 9 1 2 0 . 0 1 152 1 . 0 0 0 0 0 - 0 . 0 8 8 5 3 . 0 0 0 0 . 6 5 6 9 0 . 0 1 1 5 9 1 . 0 0 0 0 0 - 0 . 0 9 0 3 3 . 5 0 0 0 . 7 2 1 3 0 . 0 1 1 7 8 1 . 0 0 0 0 0 - 0 . 0 9 1 8 4 . 0 0 0 0 . 7 8 5 3 0 . 0 1 1 9 7 1 . 0 0 0 0 0 - 0 . 0 9 3 1 4 . 5 0 0 0 . 8 4 8 6 0 . 0 1 222 1 . 0 0 0 0 0 - 0 . 0 9 4 3 5 . 0 0 0 0 . 9 1 1 2 0 . 0 1 2 4 8 1 . 0 0 0 0 0 - 0 . 0 9 5 3 5 . 5 0 0 0 . 9 7 4 2 0 . 0 1 2 7 0 1 . 0 0 0 0 0 - 0 . 0 9 6 5 6 . 0 0 0 1 . 0 3 6 0 0 . 0 1 3 0 0 1 . 0 0 0 0 0 - 0 . 0 9 7 5 6 . 5 0 0 l . 0 9 7 0 0 . 0 1 3 3 4 1 . 0 0 0 0 0 - 0 . 0 9 8 2 7 . 0 0 0 1 . 1 5 6 4 0 . 0 1 3 7 6 1 . 0 0 0 0 0 - 0 . 0 9 8 6 7 . 5 0 0 1 . 2 1 5 3 0 . 0 1 4 1 8 1 . 0 0 0 0 0 - 0 . 0 9 9 0 8 . 0 0 0 1 . 2 7 2 8 0 . 0 1 4 6 6 1 . 0 0 0 0 0 - 0 . 0 9 9 1 8 . 5 0 0 1 . 32 9 3 0 . 0 1 5 1 5 l . 0 0 0 0 0 - 0 . 0 9 9 2 9 . 0 0 0 l. 3 8 3 0 0 . 0 1 5 7 8 1 . 0 0 0 0 0 - 0 . 0 9 8 7 9 . 5 0 0 1 . 4 3 3 5 0 . 0 1 6 5 0 1 . 0 0 0 0 0 - 0 . 0 9 7 8

1 0 . 0 0 0 1 . 47 9 6 0 . 0 1 7 3 7 1 . 0 0 0 0 0 - 0 . 0 9 6 1 1 0 . 5 0 0 1 . 52 0 5 0 . 0 1 832 1 . 0 0 0 0 0 - 0 . 0 9 3 8 1 1 . 0 0 0 l . 5 3 9 8 0 . 0 1 97 5 1 . 0 0 0 0 0 - 0 . 0 8 8 2 1 1 . 5 0 0 l . 5 6 2 8 0 . 02 1 6 6 1 . 0 0 0 0 0 - 0 . 0 8 4 4 12 . 0 0 0 1 . 5 8 1 8 0 . 0 2 4 1 8 1 . 0 0 0 0 0 - 0 . 0 8 1 1 1 2 . 5 0 0 1 . 5 9 2 6 0 . 0 2 7 7 3 1 . 0 0 0 0 0 - 0 . 0 7 8 4 1 3 . 0 0 0 1 . 6 0 1 3 0 . 0 32 0 4 1 . 0 0 0 0 0 - 0 . 0 7 6 6 1 3 . 5 0 0 1 . 6 0 2 8 0 . 0 3 7 4 9 1 . 0 0 0 0 0 - 0 . 0 7 5 5 1 4 . 0 0 0 1 . 6 0 5 9 0 . 0 4 3 3 9 1 . 0 0 0 0 0 - 0 . 0 7 5 4 1 4 . 5 0 0 1 . 6 0 2 6 0 . 0 5 0 4 0 1 . 0 0 0 0 0 - 0 . 0 7 5 7 1 5 . 0 0 0 1 . 5 9 8 8 0 . 0 57 7 2 1 . 0 0 0 0 0 - 0 . 0 7 6 3 1 5 . 5 0 0 1 . 5 9 0 3 0 . 0 6 6 1 1 1 . 0 0 0 0 0 - 0 . 0 7 7 5 1 6 . 0 0 0 1 . 5 8 1 9 0 . 0 7 4 7 3 l. 0 0 0 0 0 - 0 . 0 7 9 0 1 6 . 5 0 0 1 . 57 0 6 0 . 0 8 4 1 4 l . 0 0 0 0 0 - 0 . 0 8 0 9 1 7 . 0 0 0 l . 5 5 9 3 0 . 0 9 3 9 6 1 . 0 0 0 0 0 - 0 . 0 8 32 17 . 5 0 0 1 . 5 4 52 0 . 1 0 4 62 1 . 0 0 0 0 0 - 0 . 0 8 6 0 1 8 . 0 0 0 l . 5 3 4 8 0 . 1 1 5 0 2 1 . 0 0 0 0 0 - 0 . 0 8 8 9

POL . W2 7 1_1 0_9 ; 3

9 . 0 0 0

S xt r P xt r ---- - - - ------ -

0 . 62 8 4 0 0 . 3 9 2 7 0 0 . 6 0 9 4 0 0 . 3 9 6 7 0 0 . 5 9 5 7 0 0 . 3 9 9 7 0 0 . 5 7 8 9 0 0 . 4 0 2 4 0 0 . 5 6 0 9 0 0 . 4 0 4 6 0 0 . 5 4 9 1 0 0 . 4 1 0 8 0 0 . 5 3 3 0 0 0 . 4 1 6 0 0 0 . 5 1 9 4 0 0 . 4 1 9 3 0 0 . 5 0 6 1 0 0 . 42 1 9 0 0 . 4 9 2 7 0 0 . 4 2 4 3 0 0 . 4 8 0 1 0 0 . 42 6 6 0 0 . 4 6 5 2 0 0 . 4 3 2 5 0 0 . 4 5 5 1 0 0 . 4 3 7 5 0 0 . 4 4 0 2 0 0 . 4 4 0 8 0 0 . 4 3 2 5 0 0 . 4 4 3 5 0 0 . 4 0 7 5 0 . 4 5 1 3 0 . 3 9 8 5 0 . 4 5 3 9 0 . 3 8 8 8 0 . 4 5 6 4 0 . 3 7 7 2 0 . 4 6 0 1 0 . 3 6 92 0 . 4 6 6 7 0 . 3 5 7 0 0 . 4 7 0 6 0 . 3 4 9 8 0 . 4 7 3 6 0 . 3 3 8 3 0 . 4 7 6 3 0 . 3 3 0 2 0 . 4 7 8 7 0 . 32 1 3 0 . 4 8 5 1 0 . 3 1 0 5 0 . 4 9 0 4 0 . 3 0 3 5 0 . 4 9 3 8 0 . 2 9 0 4 0 . 4 9 6 8 0 . 2 8 3 5 0 . 4 9 9 5 0 . 2 6 9 9 0 . 5 0 3 4 0 . 2 62 8 0 . 5 1 0 7 0 . 2 4 8 8 0 . 5 1 4 5 0 . 2 4 1 0 0 . 5 1 7 6 0 . 2 2 6 8 0 . 52 0 5 0 . 2 2 0 0 0 . 52 2 9 0 . 2 0 6 4 0 . 5 3 0 4 0 . 1 9 9 9 0 . 5 3 4 6 0 . 1 8 6 9 0 . 5 3 7 7 0 . 1 8 0 5 0 . 5 4 0 4 0 . 1 6 7 4 0 . 5 42 8 0 . 1 5 9 1 0 . 5 4 4 8 0 . 1 4 7 1 0 . 5 5 1 2 0 . 1 3 8 6 0 . 5 5 5 3 0 . 12 8 2 0 . 5 5 8 4 0 . 1 1 9 0 0 . 5 6 0 8 0 . 1 1 0 6 0 . 5 6 3 0 0 . 1 0 2 0 0 . 5 6 4 9 0 . 0 9 4 9 0 . 5 6 6 6 0 . 0 8 7 2 0 . 5 7 1 2 0 . 0 8 0 8 0 . 57 5 5

FFA TN 1 9 9 0 - 1 5 3 9 POL . W2 7 1_1 0_TU1 ; 2

XFOI L Ver s ion 5 . 0

Calculated polar for : FFA-W1 - 2 7 1

1 Reynolds number fixed

xt r f • 0 . 0 1 0 ( suct ion ) 0 . 1 0 0 (pre s sure) Mach • 0 . 1 5 0 Re • 1 . 0 0 0 e 6 Ncrit = 9 . 0 0 0

a lpha CL CD Re CCL) CM s xtr P xt r - - - - - -- -------- - - ------- --------- --- -- - -- - ------ ---- - - -

1 . 0 0 0 0 . 2 9 0 7 0 . 0 1 9 6 0 1 . 0 0 0 0 0 - 0 . 0 5 5 6 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 3 6 1 7 0 . 0 1 9 2 8 1 . 0 0 0 0 0 - 0 . 0 6 0 0 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 4 3 1 7 0 . 0 1 9 0 7 1 . 0 0 0 0 0 - 0 . 0 6 3 9 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 5 0 1 0 0 . 0 1 8 9 5 1 . 0 0 0 0 0 - 0 . 0 6 7 6 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 5 6 8 9 0 . 0 1 8 9 1 1 . 0 0 0 0 0 - 0 . 0 7 0 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 6 3 5 3 0 . 0 1 8 9 7 1 . 0 0 0 0 0 - 0 . 0 7 3 8 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 6 9 9 4 0 . 0 1 9 1 4 1 . 0 0 0 0 0 - 0 . 0 7 6 0 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 7 6 1 1 0 . 0 1 9 4 2 1 . 0 0 0 0 0 - 0 . 0 7 7 8 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 8 2 0 9 0 . 0 1 9 7 8 1 . 0 0 0 0 0 - 0 . 0 7 9 1 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 8 7 8 5 0 . 0 2 0 2 3 1 . 0 0 0 0 0 - 0 . 0 8 0 0 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 9 3 3 7 0 . 0 2 0 7 6 1 . 0 0 0 0 0 - 0 . 0 8 0 5 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 0 . 9 8 5 9 0 . 02 1 3 9 1 . 0 0 0 0 0 - 0 . 0 8 0 5 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 0 3 3 1 0 . 0 2 2 1 5 1 . 0 0 0 0 0 - 0 . 0 7 9 7 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 0 5 5 4 0 . 0 2 3 1 8 1 . 0 0 0 0 0 - 0 . 0 7 4 9 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 0 8 7 8 0 . 0 2 4 7 0 1 . 0 0 0 0 0 - 0 . 0 7 2 8 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 1 1 6 7 0 . 02 6 6 9 1 . 0 0 0 0 0 - 0 . 0 7 1 0 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 1 4 2 7 0 . 0 2 92 3 1 . 0 0 0 0 0 - 0 . 0 6 9 9 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 1 6 6 2 0 . 0 32 3 1 1 . 0 0 0 0 0 - 0 . 0 6 93 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 1 8 8 0 0 . 0 3 5 9 3 1 . 0 0 0 0 0 - 0 . 0 6 92 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 2 0 7 6 0 . 0 4 0 0 9 1 . 0 0 0 0 0 - 0 . 0 6 9 5 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 2 2 5 6 0 . 0 4 4 6 8 1 . 0 0 0 0 0 - 0 . 0 7 0 1 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 2 4 1 6 0 . 0 4 9 8 1 1 . 0 0 0 0 0 - 0 . 0 7 1 1 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 2 5 62 0 . 0 5 5 2 7 1 . 0 0 0 0 0 -o . 0 1 2 1 0 . 0 1 0 0 0 . 1 0 0 0 12 . 5 0 0 1 . 2 6 8 7 0 . 0 6 1 1 9 1 . 0 0 0 0 0 - 0 . 0 7 3 4 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 2 7 9 4 0 . 0 6 7 5 9 1 . 0 0 0 0 0 - 0 . 0 7 5 0 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 2 8 8 8 0 . 0 7 4 3 4 1 . 0 0 0 0 0 - 0 . 0 7 6 6 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 2 9 6 5 0 . 0 8 1 4 3 1 . 0 0 0 0 0 - 0 . 0 7 8 4 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 3 0 3 3 0 . 0 8 8 8 6 1 . 0 0 0 0 0 - 0 . 0 8 0 4 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 3 0 9 3 0 . 0 9 6 5 8 1 . 0 0 0 0 0 - 0 . 0 8 2 5 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 5 0 0 1 . 3 1 3 9 0 . 1 0 4 7 2 1 . 0 0 0 0 0 - 0 . 0 8 4 9 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 0 0 0 1 . 3 1 6 9 0 . 1 1 3 3 4 1 . 0 0 0 0 0 - 0 . 0 8 7 4 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 5 0 0 1 . 3 1 9 4 0 . 1 2 2 3 1 1 . 0 0 0 0 0 - 0 . 0 9 0 1 0 . 0 1 0 0 0 . 1 0 0 0 1 7 . 0 0 0 1 . 32 2 3 0 . 1 3 1 3 9 1 . 0 0 0 0 0 - 0 . 0 9 3 0 0 . 0 1 0 0 0 . 1 0 0 0 1 7 . 5 0 0 1 . 32 3 8 0 . 1 4 0 9 6 1 . 0 0 0 0 0 - 0 . 0 9 6 0 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 4 0 POL . W2 7 1_2 0_9 ; 3

XFOIL Vers ion 5 . 0

Ca l culated polar for : FFA-W1-2 7 1

1 Reynolds number f ixed

xt rf .. 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pre s sure ) Mach - 0 . 1 5 0 Re = 2 . 0 0 0 e 6 Nc rit = 9 . 0 0 0

alpha CL CD Re (CL) CM S xt r P xt r ------- -------- --------- --------- -------- ------- -------- 9 . 5 0 0 0 0 - 1 . 0 4 8 9 0 0 . 0 1 5 9 4 2 . 0 0 0 0 0 - 0 . 0 1 9 3 0 0 . 6 7 1 8 0 0 . 3 5 7 0 0 - 9 . 0 0 0 0 0 - 0 . 9 8 0 4 0 0 . 0 1 4 8 0 2 . 0 0 0 0 0 - 0 . 0 2 4 2 0 0 . 652 6 0 0 . 3 6 1 5 0 - 8 . 5 0 0 0 0 - 0 . 9 0 9 1 0 0 . 0 1 3 7 8 2 . 0 0 0 0 0 - 0 . 0 2 9 4 0 0 . 6 3 0 9 0 0 . 3 6 5 4 0 - 8 . 0 0 0 0 0 - 0 . 8 3 3 8 0 0 . 0 1 2 6 3 2 . 0 0 0 0 0 - 0 . 0 3 5 6 0 0 . 6 1 7 5 0 0 . 3 7 5 3 0 - 7 . 5 0 0 0 0 - 0 . 7 6 0 1 0 0 . 0 1 1 8 9 2 . 0 0 0 0 0 - 0 . 0 4 0 6 0 0 . 6 0 1 0 0 0 . 3 7 8 9 0 - 7 . 0 0 0 0 0 - 0 . 6 8 7 8 0 0 . 0 1 1 3 9 2 . 0 0 0 0 0 - 0 . 0 4 4 9 0 0 . 5 8 1 0 0 0 . 3 8 1 3 0 - 6 . 5 0 0 0 0 - 0 . 6 1 6 3 0 0 . 0 1 0 9 9 2 . 0 0 0 0 0 - 0 . 0 4 8 7 0 0 . 5 6 7 4 0 0 . 3 8 3 4 0 - 6 . 0 0 0 0 0 - 0 . 54 1 9 0 0 . 0 1 0 4 2 2 . 0 0 0 0 0 - 0 . 0 5 3 4 0 0 . 55 1 7 0 0 . 3 8 8 0 0 - 5 . 5 0 0 0 0 - 0 . 4 6 8 4 0 0 . 0 0 9 9 5 2 . 0 0 0 0 0 - 0 . 0 5 7 7 0 0 . 53 4 5 0 0 . 3 9 3 8 0 - 5 . 0 0 0 0 0 - 0 . 3 9 8 0 0 0 . 0 0 9 7 0 2 . 0 0 0 0 0 - 0 . 0 6 0 9 0 0 . 52 4 5 0 0 . 3 9 7 9 0 - 4 . 5 0 0 0 0 - 0 . 3 2 8 9 0 0 . 0 0 9 5 5 2 . 0 0 0 0 0 - 0 . 0 6 3 7 0 0 . 5 0 8 0 0 0 . 4 0 0 8 0 - 4 . 0 0 0 0 0 - 0 . 2 6 0 7 0 0 . 0 0 9 4 7 2 . 0 0 0 0 0 - 0 . 0 6 6 2 0 0 . 4 9 5 6 0 0 . 4 0 3 2 0 - 3 . 5 0 0 0 0 - 0 . 1 92 8 0 0 . 0 0 9 4 1 2 . 0 0 0 0 0 - 0 . 0 6 8 5 0 0 . 4 8 3 5 0 0 . 4 0 4 8 0 - 3 . 0 0 0 0 0 - 0 . 1 2 4 2 0 0 . 0 0 9 3 1 2 . 0 0 0 0 0 - 0 . 0 7 1 1 0 0 . 4 6 7 8 0 0 . 4 0 8 6 0 - 2 . 5 0 0 0 0 - 0 . 0 5 5 6 0 0 . 0 0 92 0 2 . 0 0 0 0 0 - 0 . 0 7 3 7 0 0 . 4 5 8 4 0 0 . 4 1 4 3 0 - 2 . 0 0 0 0 0 0 . 0 1 2 2 0 0 . 0 0 9 1 5 2 . 0 0 0 0 0 - 0 . 0 7 6 0 0 0 . 4 4 5 0 0 0 . 4 1 8 6 0 - 1 . 50 0 0 0 0 . 0 7 9 3 0 0 . 0 0 9 1 5 2 . 0 0 0 0 0 - 0 . 0 7 8 1 0 0 . 4 3 4 2 0 0 . 42 2 1 0 - 1 . 0 0 0 0 0 0 . 1 4 62 0 0 . 0 0 9 17 2 . 0 0 0 0 0 - 0 . 0 8 0 1 0 0 . 42 0 9 0 0 . 42 4 3 0 - 0 . 5 0 0 0 0 0 . 2 127 0 0 . 0 0 92 2 2 . 0 0 0 0 0 - 0 . 0 8 2 0 0 0 . 4 12 5 0 0 . 4 2 6 0 0

0 . 0 0 0 0 0 0 . 2 7 9 2 0 0 . 0 0 92 7 2 . 0 0 0 0 0 - 0 . 0 8 3 9 0 0 . 3 9 9 1 0 0 . 42 8 3 0 0 . 5 0 0 0 0 0 . 3 4 6 3 0 0 . 0 0 92 7 2 . 0 0 0 0 0 - 0 . 0 8 5 9 0 0 . 3 9 0 3 0 0 . 4 3 4 6 0 1 . 0 0 0 0 . 4 1 2 5 0 . 0 0 9 3 4 2 . 0 0 0 0 0 - 0 . 0 8 7 8 0 . 3 7 92 0 . 4 3 9 3 1 . 5 0 0 0 . 4 7 8 4 0 . 0 0 9 4 1 2 . 0 0 0 0 0 - 0 . 0 8 9 5 0 . 3 6 8 8 0 . 4 4 3 3 2 . 0 0 0 0 . 5 4 4 0 0 . 0 0 952 2 . 0 0 0 0 0 - 0 . 0 9 1 1 0 . 3 6 2 0 0 . 4 4 5 7 2 . 5 0 0 0 . 6 0 9 1 0 . 0 0 9 6 7 2 . 0 0 0 0 0 - 0 . 0 92 6 0 . 3 4 7 4 0 . 4 4 7 6 3 . 0 0 0 0 . 6 7 4 2 0 . 0 0 9 8 0 2 . 0 0 0 0 0 - 0 . 0 9 4 1 0 . 3 4 2 4 0 . 4 4 9 7 3 . 5 0 0 0 . 7 3 9 5 0 . 0 0 9 9 1 2 . 0 0 0 0 0 - 0 . 0 9 5 7 0 . 3 32 9 0 . 4 5 6 4 4 . 0 0 0 0 . 8 0 42 0 . 0 1 0 0 8 2 . 0 0 0 0 0 - 0 . 0 9 71 0 . 32 2 4 0 . 4 6 1 4 4 . 5 0 0 0 . 8 6 8 2 0 . 0 1 0 2 7 2 . 0 0 0 0 0 - 0 . 0 9 8 4 0 . 3 1 5 7 0 . 4 6 5 4 5 . 0 0 0 0 . 9 3 1 8 0 . 0 1 0 5 0 2 . 0 0 0 0 0 - 0 . 0 9 9 5 0 . 3 0 2 0 0 . 4 6 7 9 5 . 5 0 0 0 . 9 9 5 0 0 . 0 1 0 7 3 2 . 0 0 0 0 0 - 0 . 1 0 0 6 0 . 2 9 7 0 0 . 4 6 9 9 6 . 0 0 0 1. 0 5 7 8 0 . 0 1 1 0 0 2 . 0 0 0 0 0 - 0 . 1 0 1 6 0 . 2 8 4 9 0 . 4 7 4 2 6 . 5 0 0 1 . 1 2 0 1 0 . 0 1 1 2 8 2 . 0 0 0 0 0 - 0 . 1 0 2 6 0 . 2 7 6 3 0 . 4 8 0 4 7 . 0 0 0 1 . 1 8 1 6 0 . 0 1 1 6 1 2 . 0 0 0 0 0 - 0 . 1 0 3 3 0 . 2 6 7 6 0 . 4 8 5 0 7 . 5 0 0 1 . 2 4 2 2 0 . 0 1 1 9 7 2 . 0 0 0 0 0 - 0 . 1 0 3 9 0 . 2 5 62 0 . 4 8 8 8 8 . 0 0 0 1 . 3 0 0 9 0 . 0 1 2 4 5 2 . 0 0 0 0 0 - 0 . 1 0 42 0 . 2 4 3 8 0 . 4 9 1 1 8 . 5 0 0 1 . 3 5 8 9 0 . 0 1 2 9 3 2 . 0 0 0 0 0 - 0 . 1 0 4 3 0 . 2 3 3 1 0 . 4 9 3 2 9 . 0 0 0 1 . 4 1 5 6 0 . 0 1 3 4 6 2 . 0 0 0 0 0 - 0 . 1 0 4 3 0 . 2 1 9 6 0 . 5 0 0 5 9 . 5 0 0 1 . 4 6 9 5 0 . 0 1 4 1 2 2 . 0 0 0 0 0 - 0 . 1 0 3 8 0 . 2 0 9 6 0 . 5 0 5 8

1 0 . 0 0 0 1. 5222 0 . 0 1 4 7 4 2 . 0 0 0 0 0 - 0 . 1 0 3 1 0 . 1 9 5 4 0 . 5 0 9 4 1 0 . 5 0 0 1 . 5 6 9 0 0 . 0 1 5 6 3 2 . 0 0 0 0 0 - 0 . 1 0 1 5 0 . 1 8 7 8 0 . 5 1 2 5 1 1 . 0 0 0 1 . 6 1 2 4 0 . 0 1 6 5 4 2 . 0 0 0 0 0 - 0 . 0 9 9 3 0 . 1 7 42 0 . 5 1 4 5 1 1 . 5 0 0 1 . 6 3 1 5 0 . 0 1 7 9 6 2 . 0 0 0 0 0 - 0 . 0 9 3 4 0 . 1 6 3 0 0 . 5 1 9 9 12 . 0 0 0 1 . 6 5 0 4 0 . 0 1 9 8 8 2 . 0 0 0 0 0 - 0 . 0 8 8 5 0 . 1 5 2 8 0 . 52 5 4 12 . 50 0 1 . 6 6 3 0 0 . 02 2 5 8 2 . 0 0 0 0 0 - 0 . 0 8 42 0 . 1 4 1 1 0 . 52 9 3 1 3 . 0 0 0 1 . 6 6 8 7 0 . 02 6 4 0 2 . 0 0 0 0 0 - 0 . 0 8 0 9 0 . 1 3 3 0 0 . 5322 1 3 . 5 0 0 1 . 6 7 4 5 0 . 0 3 0 8 4 2 . 0 0 0 0 0 - 0 . 0 7 8 8 0 . 12 0 5 0 . 53 4 7 1 4 . 0 0 0 1 . 6 7 0 1 0 . 0 3 6 9 0 2 . 0 0 0 0 0 - 0 . 0 7 7 6 0 . 1 1 4 3 0 . 5 3 6 3 1 4 . 50 0 1 . 6 6 62 0 . 0 4 3 4 8 2 . 0 0 0 0 0 -o . 0 1 1 2 0 . 1 0 1 9 0 . 53 97 1 5 . 0 0 0 1 . 6 5 8 4 0 . 0 5 1 0 3 2 . 0 0 0 0 0 - 0 . 0 7 7 5 0 . 0 9 5 9 0 . 5 4 4 8

FFA TN 1 9 9 0 - 1 5 4 1 POL . W2 7 1_3 0_9 ; 3

XFOI L Ve rsion 5 . 0

Calculated pol a r for : FFA-W1 - 2 7 1

1 Reynolds number f ixed

xtrf • 1 . 0 0 0 ( suct ion) 1 . 0 0 0 (pressure ) Mach - 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncrit = 9 . 0 0 0

a lpha CL CD Re ( CL ) CM S xt r P xt r ------- -------- --------- --------- -- - ----- ------- -------

- 1 0 . 0 0 0 0 0 - 1 . 1 0 6 1 0 0 . 0 1 4 2 9 3 . 0 0 0 0 0 - 0 . 0 2 2 4 0 0 . 6 65 2 0 0 . 3 3 5 8 0 - 9 . 5 0 0 0 0 - 1 . 0 3 1 3 0 0 . 0 1 2 6 6 3 . 0 0 0 0 0 - 0 . 02 9 5 0 0 . 6 4 2 5 0 0 . 3 4 6 5 0 - 9 . 0 0 0 0 0 - 0 . 9 5 6 5 0 0 . 0 1 1 6 4 3 . 0 0 0 0 0 - 0 . 0 3 5 3 0 0 . 62 4 6 0 0 . 3 5 5 5 0 - 8 . 5 0 0 0 0 - 0 . 8 8 1 2 0 0 . 0 1 0 7 5 3 . 0 0 0 0 0 - 0 . 0 4 0 9 0 0 . 6 0 7 0 0 0 . 3 6 5 4 0 - 8 . 0 0 0 0 0 - 0 . 8 0 7 9 0 0 . 0 1 0 1 5 3 . 0 0 0 0 0 - 0 . 0 4 5 4 0 0 . 5 8 7 7 0 0 . 3 6 8 6 0 - 7 . 0 0 0 0 0 - 0 . 6 6 5 8 0 0 . 0 0 9 4 3 3 . 0 0 0 0 0 - 0 . 0 5 2 6 0 0 . 5 5 7 1 0 0 . 3 7 3 2 0 - 6 . 5 0 0 0 0 - 0 . 5 9 4 1 0 0 . 0 0 9 0 5 3 . 0 0 0 0 0 - 0 . 0 5 6 2 0 0 . 5 4 3 1 0 0 . 3 7 9 4 0 - 6 . 0 0 0 0 0 - 0 . 52 4 5 0 0 . 0 0 8 8 4 3 . 0 0 0 0 0 - 0 . 0 5 9 2 0 0 . 52 9 5 0 0 . 3 8 4 8 0 - 5 . 5 0 0 0 0 - 0 . 4 5 5 7 0 0 . 0 0 8 6 8 3 . 0 0 0 0 0 - 0 . 0 6 1 8 0 0 . 5 1 7 6 0 0 . 3 8 9 2 0 - 5 . 0 0 0 0 0 - 0 . 3 8 7 3 0 0 . 0 0 8 5 5 3 . 0 0 0 0 0 - 0 . 0 6 4 4 0 0 . 5 0 1 3 0 0 . 3 92 9 0 - 4 . 5 0 0 0 0 - 0 . 3 1 9 5 0 0 . 0 0 8 4 8 3 . 0 0 0 0 0 - 0 . 0 6 6 7 0 0 . 4 8 9 9 0 0 . 3 9 5 0 0 - 4 . 0 0 0 0 0 - 0 . 2 52 1 0 0 . 0 0 8 4 4 3 . 0 0 0 0 0 - 0 . 0 6 8 9 0 0 . 47 5 3 0 0 . 3 9 6 4 0 - 3 . 5 0 0 0 0 - 0 . 1 8 52 0 0 . 0 0 8 4 4 3 . 0 0 0 0 0 - 0 . 0 7 0 9 0 0 . 4 6 4 0 0 0 . 3 9 7 4 0 - 3 . 0 0 0 0 0 - 0 . 1 1 6 9 0 0 . 0 0 8 3 4 3 . 0 0 0 0 0 - 0 . 0 7 3 3 0 0 . 4 4 8 3 0 0 . 4 02 8 0 -2 . 5 0 0 0 0 - 0 . 0 4 9 4 0 0 . 0 0 8 2 8 3 . 0 0 0 0 0 - 0 . 0 7 5 5 0 0 . 4 4 1 7 0 0 . 4 0 8 1 0 -2 . 0 0 0 0 0 0 . 0 1 7 7 0 0 . 0 0 8 2 7 3 . 0 0 0 0 0 - 0 . 0 7 7 6 0 0 . 42 4 6 0 0 . 4 1 3 8 0 -1 . 5 0 0 0 0 0 . 0 8 4 6 0 0 . 0 0 8 2 6 3 . 0 0 0 0 0 - 0 . 0 7 9 6 0 0 . 4 1 6 8 0 0 . 4 1 7 1 0 - 1 . 0 0 0 0 0 0 . 1 5 1 2 0 0 . 0 0 8 3 0 3 . 0 0 0 0 0 -0 . 0 8 1 5 0 0 . 4 0 6 9 0 0 . 4 1 9 5 0 - 0 . 5 0 0 0 0 0 . 2 1 7 6 0 0 . 0 0 8 3 4 3 . 0 0 0 0 0 - 0 . 0 8 3 3 0 0 . 3 9 3 1 0 0 . 42 1 2 0

0 . 0 0 0 0 0 0 . 2 8 3 5 0 0 . 0 0 8 4 2 3 . 0 0 0 0 0 - 0 . 0 8 5 1 0 0 . 3 8 5 9 0 0 . 4 2 2 4 0 0 . 5 0 0 0 0 0 . 3 4 9 8 0 0 . 0 0 8 4 7 3 . 0 0 0 0 0 - 0 . 0 8 6 9 0 0 . 3 7 4 3 0 0 . 42 5 4 0 1 . 0 0 0 0 . 4 1 5 2 0 . 0 0 8 5 3 3 . 0 0 0 0 0 - 0 . 0 8 8 5 0 . 3 6 3 0 0 . 4 3 1 1 1 . 5 0 0 0 . 4 8 1 0 0 . 0 0 8 6 1 3 . 0 0 0 0 0 - 0 . 0 9 0 2 0 . 35 6 9 0 . 4 3 6 0 2 . 0 0 0 0 . 5 4 6 7 0 . 0 0 8 6 9 3 . 0 0 0 0 0 - 0 . 0 9 1 8 0 . 3 4 5 7 0 . 4 3 9 8 2 . 5 0 0 0 . 6 1 2 0 0 . 0 0 8 8 1 3 . 0 0 0 0 0 - 0 . 0 9 33 0 . 33 6 7 0 . 4 4 3 0 3 . 0 0 0 0 . 67 6 9 0 . 0 0 8 9 6 3 . 0 0 0 0 0 - 0 . 0 9 4 8 0 . 32 9 0 0 . 4 4 4 8 3 . 5 0 0 0 . 7 4 1 8 0 . 0 0 9 1 0 3 . 0 0 0 0 0 - 0 . 0 9 6 1 0 . 3 1 7 2 0 . 4 4 6 1 4 . 0 0 0 0 . 8 0 6 4 0 . 0 0 92 6 3 . 0 0 0 0 0 - 0 . 0 9 7 6 0 . 3 1 0 6 0 . 4 5 1 7 4 . 5 0 0 0 . 8 7 0 8 0 . 0 0 9 4 3 3 . 0 0 0 0 0 - 0 . 0 9 8 9 0 . 3 0 1 3 0 . 4 5 7 3 5 . 0 0 0 0 . 9 3 4 8 0 . 0 0 9 6 2 3 . 0 0 0 0 0 - 0 . 1 0 0 1 0 . 2 9 0 0 0 . 4 6 1 9 5 . 5 0 0 0 . 9 9 8 2 0 . 0 0 9 8 5 3 . 0 0 0 0 0 - 0 . 1 0 1 2 0 . 2 8 4 0 0 . 4 6 5 1 6 . 0 0 0 1 . 0 6 1 2 0 . 0 1 0 0 9 3 . 0 0 0 0 0 - 0 . 1 02 2 0 . 2 6 9 8 0 . 4 6 7 9 6 . 5 0 0 1 . 12 3 6 0 . 0 1 0 3 7 3 . 0 0 0 0 0 - 0 . 1 0 3 1 0 . 2 6 42 0 . 4 6 9 4 7 . 0 0 0 1 . 1 8 5 3 0 . 0 1 0 7 0 3 . 0 0 0 0 0 - 0 . 1 0 3 9 0 . 2 5 2 4 0 . 4 7 5 1 7 . 5 0 0 1 . 2 4 6 5 0 . 0 1 1 0 4 3 . 0 0 0 0 0 - 0 . 1 0 4 5 0 . 2 4 1 3 0 . 4 8 1 1 8 . 0 0 0 1 . 3 0 6 1 0 . 0 1 1 4 9 3 . 0 0 0 0 0 - 0 . 1 0 4 9 0 . 22 8 5 0 . 4 8 5 8 8 . 5 0 0 1 . 3 6 4 5 0 . 0 1 1 9 7 3 . 0 0 0 0 0 - 0 . 1 0 52 0 . 2 1 6 4 0 . 4 8 9 1 9 . 0 0 0 1 . 4 2 2 1 0 . 0 1 2 4 7 3 . 0 0 0 0 0 - 0 . 1 0 52 0 . 2 0 4 8 0 . 4 9 1 4 9 . 5 0 0 1 . 4 7 6 3 0 . 0 1 3 1 5 3 . 0 0 0 0 0 - 0 . 1 0 4 8 0 . 1 9 1 7 0 . 4 9 4 1

1 0 . 0 0 0 1 . 53 0 9 0 . 0 1 37 2 3 . 0 0 0 0 0 - 0 . 1 0 4 3 0 . 1 7 7 3 0 . 5 0 0 9 1 0 . 5 0 0 1 . 57 9 1 0 . 0 1 4 5 9 3 . 0 0 0 0 0 - 0 . 1 0 2 9 0 . 1 6 8 1 0 . 5 0 6 6 1 1. 0 0 0 1 . 62 5 7 0 . 0 1 5 4 0 3 . 0 0 0 0 0 - 0 . 1 0 12 0 . 1527 0 . 5 1 0 6 1 1 . 5 0 0 1 . 6 6 0 7 0 . 0 1 6 62 3 . 0 0 0 0 0 - 0 . 0 9 7 9 0 . 1 4 3 5 0 . 5 1 3 4 12 . 0 0 0 1 . 6 7 5 6 0 . 0 1 8 1 1 3 . 0 0 0 0 0 - 0 . 0 9 1 3 0 . 1 3 1 1 0 . 5 1 52 1 2 . 5 0 0 1 . 6 8 3 1 0 . 02 0 6 9 3 . 0 0 0 0 0 - 0 . 0 8 5 5 0 . 12 3 6 0 . 5 1 6 6 1 3 . 0 0 0 1 . 6 9 5 6 0 . 02 3 62 3 . 0 0 0 0 0 - 0 . 0 8 1 9 0 . 1 1 0 9 0 . 52 4 0 13 . 5 0 0 1 . 6 9 4 3 0 . 02 8 2 6 3 . 0 0 0 0 0 - 0 . 07 8 8 0 . 1 0 5 4 0 . 52 8 7

FFA TN 1 9 9 0 - 1 5 4 2 POL . W2 7 1_3 0_TU1 ; 2

XFOIL Vers ion 5 . 0

Ca lculated polar for : FFA-W1 - 2 71

1 Reynolds number f ixed

xt rf • 0 . 0 1 0 ( suction ) 0 . 1 0 0 (pre s sure ) Mach • 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncrit = 9 . 0 0 0

alpha CL CD Re ( CL ) CM S xt r P xt r - - - - - - - -------- ------ - -- ---- - -- - - -------- -- - - --- - -- -- - -

1 . 0 0 0 0 . 3 4 2 7 0 . 0 1 5 4 4 3 . 0 0 0 0 0 - 0 . 0 6 9 8 0 . 0 1 0 0 0 . 1 0 0 0 1 . 50 0 0 . 4 1 2 9 0 . 0 1 5 2 7 3 . 0 0 0 0 0 - 0 . 0 7 3 3 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 4 8 1 9 0 . 0 1 5 1 8 3 . 0 0 0 0 0 - 0 . 0 7 6 5 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 5 4 8 8 0 . 0 1 5 2 1 3 . 0 0 0 0 0 - 0 . 0 7 9 0 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 1 4 4 0 . 0 1 5 3 1 3 . 0 0 0 0 0 - o . 0 8 1 1 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 6 7 9 0 0 . 0 1 5 4 5 3 . 0 0 0 0 0 - 0 . 0 8 3 0 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 7 4 2 7 0 . 0 1 5 65 3 . 0 0 0 0 0 - 0 . 0 8 4 7 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 8 0 5 3 0 . 0 1 5 8 8 3 . 0 0 0 0 0 - 0 . 0 8 6 1 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 8 6 6 8 0 . 0 1 6 1 6 3 . 0 0 0 0 0 - 0 . 0 8 7 4 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 9 2 7 1 0 . 0 1 6 4 9 3 . 0 0 0 0 0 - 0 . 0 8 8 3 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 9 8 6 1 0 . 0 1 6 8 7 3 . 0 0 0 0 0 - 0 . 0 8 9 1 0 . 0 1 0 0 0 . 1 0 0 0 6 . 50 0 1 . 0 4 3 5 0 . 0 1 7 3 1 3 . 0 0 0 0 0 - 0 . 0 8 9 5 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 0 9 9 1 0 . 0 1 7 8 0 3 . 0 0 0 0 0 - 0 . 0 8 9 7 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1 52 4 0 . 0 1 8 3 7 3 . 0 0 0 0 0 - 0 . 0 8 9 4 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 2 0 2 5 0 . 0 1 9 0 2 3 . 0 0 0 0 0 - 0 . 0 8 8 7 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 2 4 6 7 0 . 0 1 9 7 8 3 . 0 0 0 0 0 - 0 . 0 8 7 0 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 2 6 3 1 0 . 02 0 9 3 3 . 0 0 0 0 0 - 0 . 0 8 0 9 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 2 9 1 4 0 . 0 2 2 5 4 3 . 0 0 0 0 0 - 0 . 0 7 7 8 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 3 1 4 4 0 . 0 2 4 6 9 3 . 0 0 0 0 0 - 0 . 0 7 5 1 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 335 6 0 . 0 2 7 4 2 3 . 0 0 0 0 0 - 0 . 0 7 3 3 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 3 5 5 1 0 . 0 3 0 7 5 3 . 0 0 0 0 0 - 0 . 0 7 2 1 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 37 1 9 0 . 0 3 4 6 6 3 . 0 0 0 0 0 - 0 . 0 7 1 5 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 3 8 7 4 0 . 0 3 9 1 6 3 . 0 0 0 0 0 - 0 . 0 7 1 5 0 . 0 1 0 0 0 . 1 0 0 0 12 . 5 0 0 1 . 4 0 2 8 0 . 0 4 3 9 5 3 . 0 0 0 0 0 - 0 . 0 7 1 7 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 4 1 4 7 0 . 0 4 9 4 6 3 . 0 0 0 0 0 - 0 . 0 7 2 4 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 4 2 5 1 0 . 0 5 52 8 3 . 0 0 0 0 0 - 0 . 0 7 32 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 4 3 POLAR . W2_1 52_3 0_9 ; 1

I S E S polar driver Vers ion 1 . 3

Calculated polar for : AIRFOI L FFA-W2 - 1 52

Vortex + doublet far field Entropy conse rved

Mach == 0 . 1 5 0 Re 3 . 0 0 0 e 6 Acrit = 9 . 0 0 0

a lpha CL CD CDi CM S xt r P xt r - - - - -- - - - ------ - ---- - --- --- - -- -- - --- - ---- ---- - - - - - -- -- -

4 . 0 0 0 0 . 7 7 62 0 . 0 0 5 1 4 0 . 0 0 0 0 0 - 0 . 0 5 8 7 0 . 4 8 1 6 0 . 8 4 5 1 4 . 5 0 0 0 . 8 3 4 6 0 . 0 0 5 3 0 0 . 0 0 0 0 0 - 0 . 0 5 9 6 0 . 4 6 6 3 0 . 8 6 0 2 5 . 0 0 0 0 . 8 92 7 0 . 0 0 5 4 2 0 . 0 0 0 0 0 - 0 . 0 6 0 4 0 . 4 5 4 8 0 . 8 7 5 6 5 . 5 0 0 0 . 9 5 0 1 0 . 0 0 5 62 0 . 0 0 0 0 0 - 0 . 0 6 1 2 0 . 4 3 7 8 0 . 8 9 0 1 6 . 0 0 0 1 . 0 0 6 6 0 . 0 0 5 92 0 . 0 0 0 0 0 - 0 . 0 6 1 9 0 . 4 1 62 0 . 9 0 3 3 6 . 2 5 0 1 . 0 3 4 3 0 . 0 0 6 1 1 0 . 0 0 0 0 0 - 0 . 0 62 2 0 . 4 0 1 7 0 . 9 0 9 8 6 . 5 0 0 1 . 0 6 1 5 0 . 0 0 6 3 5 0 . 0 0 0 0 0 - 0 . 0 62 5 0 . 3 8 3 0 0 . 9 1 6 1 6 . 7 5 0 1 . 0 8 7 5 0 . 0 0 6 7 2 0 . 0 0 0 0 0 - 0 . 0 62 6 0 . 3 5 5 8 0 . 92 3 3 7 . 0 0 0 1 . 1 1 0 9 0 . 0 0 7 2 7 0 . 0 0 0 0 0 - 0 . 0 62 5 0 . 3 1 8 3 0 . 9 3 2 0 7 . 2 5 0 1 . 1 3 2 0 0 . 0 0 7 9 7 0 . 0 0 0 0 0 - 0 . 0 62 1 0 . 2 7 1 0 0 . 9 4 1 7 7 . 5 0 0 1 . 1 5 1 8 0 . 0 0 8 6 6 0 . 0 0 0 0 0 - 0 . 0 6 1 5 0 . 2 2 9 5 0 . 9 5 2 7 7 . 7 5 0 1 . 1 6 8 6 0 . 0 0 9 3 5 0 . 0 0 0 0 0 - 0 . 0 6 0 4 0 . 1 9 3 6 0 . 9 7 0 2 8 . 0 0 0 1 . 1 9 1 0 0 . 0 1 0 0 1 0 . 0 0 0 0 0 - 0 . 0 6 0 6 0 . 1 6 0 7 1 . 0 0 0 0 8 . 2 5 0 1 . 2 0 9 3 0 . 0 1 0 72 0 . 0 0 0 0 0 - 0 . 0 6 0 0 0 . 1 3 4 5 1 . 0 0 0 0 8 . 5 0 0 1 . 2 2 62 0 . 0 1 1 4 3 0 . 0 0 0 0 0 - 0 . 0 5 9 4 0 . 1 1 3 3 1 . 0 0 0 0 8 . 7 5 0 1 . 2 4 0 2 0 . 0 1 2 2 1 0 . 0 0 0 0 0 - 0 . 0 5 8 3 0 . 0 9 5 9 1 . 0 0 0 0 9 . 0 0 0 1 . 2 3 9 8 0 . 0 1 3 2 6 0 . 0 0 0 0 0 - 0 . 0 5 5 5 0 . 0 8 5 4 1 . 0 0 0 0 9 . 2 5 0 1 . 2 4 2 2 0 . 0 1 4 5 3 0 . 0 0 0 0 0 - 0 . 0 5 4 4 0 . 0 7 5 9 1 . 0 0 0 0 9 . 5 0 0 1 . 2 4 1 9 0 . 0 1 6 0 1 0 . 0 0 0 0 0 - 0 . 0 5 3 4 0 . 0 6 8 5 1 . 0 0 0 0 9 . 7 5 0 1 . 2 3 8 4 0 . 0 1 7 62 0 . 0 0 0 0 0 - 0 . 0 5 1 2 0 . 0 6 1 8 1 . 0 0 0 0

1 0 . 0 0 0 1 . 2 3 5 8 0 . 0 1 9 4 9 0 . 0 0 0 0 0 - 0 . 0 5 0 1 0 . 0 5 5 2 1 . 0 0 0 0 1 0 . 2 5 0 1 . 2 3 1 1 0 . 0 2 1 2 1 0 . 0 0 0 0 0 - 0 . 0 4 7 4 0 . 0 5 0 3 1 . 0 0 0 0 1 0 . 5 0 0 1 . 2 327 0 . 0 2 3 1 3 0 . 0 0 0 0 0 - 0 . 0 4 8 3 0 . 0 4 52 1 . 0 0 0 0 1 0 . 6 6 7 1 . 2 2 8 0 0 . 0 2 4 3 9 0 . 0 0 0 0 0 - 0 . 0 4 6 8 0 . 0 4 2 4 1 . 0 0 0 0

FFA TN 1 9 9 0 - 1 5 4 4 POLAR . W2_1 5 2_3 0_TU1 ; 1

I SES polar drive r Ve rs ion 1 . 3

Ca lculated polar for : AIRFOIL FFA-W2 - 1 52

Vortex + doublet far field Ent ropy conse rved

Mach = 0 . 1 5 0 Re 3 . 0 0 0 e 6 Ac rit = 9 . 0 0 0

a lpha CL CD CDi CM S xt r P xt r --- - - - - ----- - - - - - - -- - - -- --------- -------- ---- - - - ---- - --

0 . 0 0 0 0 . 2 9 2 5 0 . 0 0 9 8 8 0 . 0 0 0 0 0 - 0 . 0 5 0 6 0 . 0 1 0 0 0 . 1 0 0 0 0 . 5 0 0 0 . 3 4 9 8 0 . 0 1 0 0 1 0 . 0 0 0 0 0 - 0 . 0 5 1 4 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 . 4 0 7 3 0 . 0 1 0 1 7 0 . 0 0 0 0 0 - 0 . 0 5 2 1 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 4 6 4 9 0 . 0 1 0 3 3 0 . 0 0 0 0 0 - 0 . 0 52 9 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 52 1 2 0 . 0 1 0 52 0 . 0 0 0 0 0 - 0 . 0 5 3 6 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 5 7 7 6 0 . 0 1 0 7 3 0 . 0 0 0 0 0 - 0 . 0 5 4 3 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 3 4 4 0 . 0 1 0 9 6 0 . 0 0 0 0 0 - 0 . 0 5 4 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 6 9 0 0 0 . 0 1 1 2 1 0 . 0 0 0 0 0 - 0 . 0 5 5 5 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 7 4 4 9 0 . 0 1 1 5 0 0 . 0 0 0 0 0 - 0 . 0 5 6 0 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 7 9 9 0 0 . 0 1 1 8 1 0 . 0 0 0 0 0 - 0 . 0 5 6 5 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 8 5 2 2 0 . 0 1 2 1 6 0 . 0 0 0 0 0 - 0 . 0 5 6 8 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 9 0 42 0 . 0 1 2 5 5 0 . 0 0 0 0 0 - 0 . 0 5 7 1 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 9 5 4 5 0 . 0 1 2 9 9 0 . 0 0 0 0 0 - 0 . 0 5 7 2 0 . 0 1 0 0 0 . 1 0 0 0 6 . 2 5 0 0 . 9 7 8 4 0 . 0 1 3 2 3 0 . 0 0 0 0 0 - 0 . 0 5 7 2 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 0 0 3 3 0 . 0 1 3 4 9 0 . 0 0 0 0 0 - 0 . 0 5 7 1 0 . 0 1 0 0 0 . 1 0 0 0 6 . 7 5 0 1 . 0 2 6 6 0 . 0 1 3 7 7 0 . 0 0 0 0 0 - 0 . 0 5 6 9 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 0 4 9 0 0 . 0 1 4 0 7 0 . 0 0 0 0 0 - 0 . 0 5 6 7 0 . 0 1 0 0 0 . 1 0 0 0 7 . 2 5 0 1 . 0 6 9 7 0 . 0 1 4 4 3 0 . 0 0 0 0 0 - 0 . 0 5 6 4 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1. 0 8 1 7 0 . 0 1 5 0 0 0 . 0 0 0 0 0 - 0 . 0 5 4 8 0 . 0 1 0 0 0 . 1 0 0 0 7 . 7 5 0 1 . 0 9 3 3 0 . 0 1 5 7 2 0 . 0 0 0 0 0 - 0 . 0 5 4 2 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 1 0 3 1 0 . 0 1 6 53 0 . 0 0 0 0 0 - 0 . 0 5 3 1 0 . 0 1 0 0 0 . 1 0 0 0 8 . 2 5 0 1 . 1 1 2 3 0 . 0 1 7 4 6 0 . 0 0 0 0 0 - 0 . 0 5 2 0 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 1 2 0 0 0 . 0 1 8 4 9 0 . 0 0 0 0 0 - 0 . 0 5 1 0 0 . 0 1 0 0 0 . 1 0 0 0 8 . 7 5 0 1 . 1 2 6 7 0 . 0 1 9 5 9 0 . 0 0 0 0 0 - 0 . 0 4 9 5 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 1 3 2 8 0 . 0 2 0 8 2 0 . 0 0 0 0 0 - 0 . 0 4 8 5 0 . 0 1 0 0 0 . 1 0 0 0 9 . 2 5 0 1 . 1 4 1 6 0 . 0 2 2 1 1 0 . 0 0 0 0 0 - 0 . 0 4 9 3 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 1 4 1 6 0 . 0 2 3 4 9 0 . 0 0 0 0 0 - 0 . 0 4 6 6 0 . 0 1 0 0 0 . 1 0 0 0 9 . 7 5 0 1 . 1 4 6 0 0 . 0 2 4.8 6 0 . 0 0 0 0 0 - 0 . 0 4 4 8 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 1 5 4 9 0 . 0 2 62 7 0 . 0 0 0 0 0 - 0 . 0 4 7 0 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 2 5 0 1 . 1 5 5 9 0 . 0 2 7 7 5 0 . 0 0 0 0 0 - 0 . 0 4 4 0 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 4 1 7 1 . 1 6 0 7 0 . 0 2 8 6 9 0 . 0 0 0 0 0 - 0 . 0 4 3 5 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 8 3 1 . 1 5 8 2 0 . 0 2 9 7 6 0 . 0 0 0 0 0 - 0 . 0 4 1 5 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 7 5 0 1 . 1 62 3 0 . 0 3 0 7 1 0 . 0 0 0 0 0 - 0 . 0 4 1 0 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 9 1 7 1 . 1 6 9 3 0 . 0 3 1 8 3 0 . 0 0 0 0 0 - 0 . 0 4 3 1 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 8 3 1 . 1 7 0 3 0 . 0 3 2 8 7 0 . 0 0 0 0 0 - 0 . 0 4 1 6 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 1 9 4 1 . 1 6 7 3 0 . 0 3 3 5 2 0 . 0 0 0 0 0 - 0 . 0 3 8 1 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 3 33 1 . 1 7 9 1 0 . 0 3 4 5 5 0 . 0 0 0 0 0 - 0 . 0 4 3 5 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 4 4 4 1 . 1 7 2 6 0 . 0 3 5 2 2 0 . 0 0 0 0 0 - 0 . 0 3 9 6 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 8 3 1 . 1 7 62 0 . 0 3 6 0 5 0 . 0 0 0 0 0 - 0 . 0 3 9 5 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 7 5 0 1 . 1 8 6 1 0 . 0 3 7 3 1 0 . 0 0 0 0 0 - 0 . 0 4 3 5 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 8 6 1 1 . 1 7 3 6 0 . 0 3 8 0 6 0 . 0 0 0 0 0 - 0 . 0 3 5 0 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 4 5

XFOI L Vers ion 5 . 0

Calculated pola r for : FFA-W2 - 1 52

1 Reynolds number fixed

xt rf = 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pres sure ) Mach = 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it

a lpha CL CD Re (CL) CM - -- - --- - ------- --------- --------- --------- 5 . 5 0 0 0 0 - 0 . 3 4 1 5 0 0 . 0 1 1 3 8 1 . 0 0 0 0 0 - 0 . 0 4 4 5 0 - 5 . 0 0 0 0 0 - 0 . 2 8 4 0 0 0 . 0 1 0 9 2 1 . 0 0 0 0 0 - 0 . 0 4 4 8 0 - 4 . 5 0 0 0 0 - 0 . 2 2 5 7 0 0 . 0 1 0 6 4 1 . 0 0 0 0 0 - 0 . 0 4 5 3 0 - 3 . 5 0 0 0 0 - 0 . 1 0 9 2 0 0 . 0 0 9 7 1 1 . 0 0 0 0 0 - 0 . 0 4 6 0 0 - 3 . 0 0 0 0 0 - 0 . 0 5 0 4 0 0 . 0 0 9 3 9 1 . 0 0 0 0 0 - 0 . 0 4 6 5 0 - 2 . 5 0 0 0 0 0 . 0 0 8 4 0 0 . 0 0 9 0 5 1 . 0 0 0 0 0 - 0 . 0 4 7 2 0 - 2 . 0 0 0 0 0 0 . 0 6 5 9 0 0 . 0 0 8 3 7 1 . 0 0 0 0 0 - 0 . 0 4 8 0 0 - 1 . 5 0 0 0 0 0 . 1 2 3 5 0 0 . 0 0 7 7 4 1 . 0 0 0 0 0 - 0 . 0 4 8 8 0 - 1 . 0 0 0 0 0 0 . 1 8 1 5 0 0 . 0 0 7 0 9 1 . 0 0 0 0 0 - 0 . 0 4 9 6 0

0 . 0 0 0 0 0 0 . 2 9 9 5 0 0 . 0 0 6 6 0 1 . 0 0 0 0 0 - 0 . 0 5 1 1 0 0 . 5 0 0 0 0 0 . 3 5 8 2 0 0 . 0 0 6 5 7 1 . 0 0 0 0 0 - 0 . 0 5 1 6 0 1 . 0 0 0 0 0 0 . 4 1 7 3 0 0 . 0 0 6 5 8 1 . 0 0 0 0 0 - 0 . 0 5 2 1 0 1 . 5 0 0 0 0 0 . 47 6 5 0 0 . 0 0 6 6 3 1 . 0 0 0 0 0 - 0 . 0 52 8 0 2 . 0 0 0 0 . 5 3 5 2 0 . 0 0 6 7 5 1 . 0 0 0 0 0 - 0 . 0 5 3 4 2 . 5 0 0 0 . 5 9 3 9 0 . 0 0 6 8 0 1 . 0 0 0 0 0 - 0 . 0 5 3 9 3 . 0 0 0 0 . 6 5 2 3 0 . 0 0 6 8 7 1 . 0 0 0 0 0 - 0 . 0 5 4 4 3 . 5 0 0 0 . 7 1 0 2 0 . 0 0 7 0 0 1 . 0 0 0 0 0 - 0 . 0 5 4 9 4 . 0 0 0 0 . 7 6 7 1 0 . 0 0 7 1 0 1 . 0 0 0 0 0 - 0 . 0 5 5 1 4 . 5 0 0 0 . 8 2 3 6 0 . 0 0 7 1 9 1 . 0 0 0 0 0 - 0 . 0 5 5 2 5 . 0 0 0 0 . 8 7 92 0 . 0 0 7 3 5 1 . 0 0 0 0 0 - 0 . 0 5 52 5 . 5 0 0 0 . 9 3 4 2 0 . 0 0 7 4 0 1 . 0 0 0 0 0 - 0 . 0 5 5 1 6 . 0 0 0 0 . 9 9 1 3 0 . 0 0 7 5 5 1 . 0 0 0 0 0 - 0 . 0 5 5 5 6 . 5 0 0 1 . 0 6 0 8 0 . 0 0 7 8 3 1 . 0 0 0 0 0 - 0 . 0 5 8 8 7 . 0 0 0 1 . 1 1 9 8 0 . 0 0 8 2 0 1 . 0 0 0 0 0 - 0 . 0 6 0 1 7 . 5 0 0 1 . 1 7 52 0 . 0 0 8 9 3 1 . 0 0 0 0 0 - 0 . 0 6 0 9 8 . 0 0 0 1 . 2 1 8 9 0 . 0 1 0 6 9 1 . 0 0 0 0 0 - 0 . 0 6 0 5 8 . 5 0 0 1". 2 4 0 7 0 . 0 1 3 9 0 1 . 0 0 0 0 0 - 0 . 0 5 8 2 9 . 0 0 0 1 . 2 5 1 7 0 . 0 1 7 0 7 1 . 0 0 0 0 0 - 0 . 0 5 53 9 . 5 0 0 1 : 2 6 0 3 0 . 0 2 1 0 0 1 . 0 0 0 0 0 - 0 . 0 5 3 5

1 0 . 0 0 0 1 . 2 6 7 6 0 . 02 5 4 0 1 . 0 0 0 0 0 - 0 . 0 5 2 2 1 0 . 5 0 0 1 . 2 7 6 1 0 . 0 2 9 9 3 1 . 0 0 0 0 0 - 0 . 0 5 1 1 1 1 . 0 0 0 1 . 2 8 5 4 0 . 0 3 4 5 0 1 . 0 0 0 0 0 - 0 . 0 5 0 2 1 1 . 5 0 0 1 . 2 9 8 0 0 . 0 3 8 9 3 1 . 0 0 0 0 0 - 0 . 0 4 9 4 1 2 . 0 0 0 1 . 3 1 0 0 0 . 0 4 3 5 4 1 . 0 0 0 0 0 - 0 . 0 4 8 9 1 2 . 5 0 0 1 . 3 2 3 8 0 . 0 4 8 1 4 1 . 0 0 0 0 0 - 0 . 0 4 8 5 1 3 . 0 0 0 1 . 3 3 6 3 0 . 0 52 9 4 1 . 0 0 0 0 0 - 0 . 0 4 8 2 1 3 . 5 0 0 1 . 3 4 7 6 0 . 0 5 8 12 1 . 0 0 0 0 0 - 0 . 0 4 8 1 1 4 . 0 0 0 1 . 3 4 3 5 0 . 0 6 5 4 2 1 . 0 0 0 0 0 - 0 . 0 4 7 9 1 4 . 5 0 0 1 . 3 5 7 4 0 . 0 7 0 6 0 1 . 0 0 0 0 0 - 0 . 0 4 8 4 1 5 . 0 0 0 1 . 3 6 8 4 0 . 0 7 6 3 9 1 . 0 0 0 0 0 - 0 . 0 4 9 0 1 5 . 5 0 0 1 . 3 7 7 0 0 . 0 8 2 6 8 1 . 0 0 0 0 0 - 0 . 0 4 9 9 1 6 . 0 0 0 1 . 3 8 2 6 0 . 0 8 9 5 5 1 . 0 0 0 0 0 - 0 . 0 5 0 9 1 6 . 5 0 0 1 . 3 8 2 1 0 . 0 9 7 7 6 1 . 0 0 0 0 0 - 0 . 0 5 2 4 1 7 . 0 0 0 1 . 3 6 5 4 0 . 1 0 92 7 1 . 0 0 0 0 0 - 0 . 0 5 4 8

POL . W2_1 5 2_1 0_9 ; 3

9 . 0 0 0

S xt r P xt r ------- -------0 . 62 3 1 0 0 . 0 2 4 2 0 0 . 6 1 5 3 0 0 . 0 2 7 5 0 0 . 6 1 0 2 0 0 . 0 2 9 4 0 0 . 5 9 9 1 0 0 . 0 4 6 0 0 0 . 5 9 3 1 0 0 . 0 6 5 0 0 0 . 5 8 9 0 0 0 . 1 0 8 1 0 0 . 5 8 3 9 0 0 . 2 3 1 4 0 0 . 5 7 6 5 0 0 . 3 8 0 7 0 0 . 5 7 2 7 0 0 . 5 5 0 1 0 0 . 5 6 1 7 0 0 . 7 3 4 8 0 0 . 5 5 6 5 0 0 . 7 8 5 6 0 0 . 5 5 2 6 0 0 . 8 1 3 1 0 0 . 5 4 7 4 0 0 . 8 3 3 6 0 0 . 5 4 0 1 0 . 8 5 1 8 0 . 5 3 6 0 0 . 8 6 8 6 0 . 5 3 1 1 0 . 8 8 4 1 0 . 5 2 3 3 0 . 8 9 8 8 0 . 5 1 8 6 0 . 9 1 4 4 0 . 5 1 2 9 0 . 92 8 6 0 . 5 0 3 2 0 . 9 4 3 9 0 . 4 92 1 0 . 9 6 1 6 0 . 4 7 9 3 0 . 9 8 4 7 0 . 4 6 3 9 1 . 0 0 0 0 0 . 4 4 4 6 1 . 0 0 0 0 0 . 4 0 3 4 1 . 0 0 0 0 0 . 3 1 2 5 1 . 0 0 0 0 0 . 1 9 1 0 1 . 0 0 0 0 0 . 1 3 3 6 1 . 0 0 0 0 0 . 0 9 8 2 1 . 0 0 0 0 0 . 0 7 4 1 1 . 0 0 0 0 0 . 0 5 4 7 1 . 0 0 0 0 0 . 0 3 9 8 1 . 0 0 0 0 0 . 0 2 8 5 1 . 0 0 0 0 0 . 0 2 2 0 1 . 0 0 0 0 0 . 0 1 7 5 1 . 0 0 0 0 0 . 0 1 5 8 1 . 0 0 0 0 0 . 0 1 3 3 1 . 0 0 0 0 0 . 0 1 0 0 1 . 0 0 0 0 0 . 0 0 9 7 1 . 0 0 0 0 0 . 0 0 92 1 . 0 0 0 0 0 . 0 0 8 6 1 . 0 0 0 0 0 . 0 0 7 9 1 . 0 0 0 0 0 . 0 0 7 0 1 . 0 0 0 0 0 . 0 0 5 9 1 . 0 0 0 0

FFA TN 1 9 9 0 - 1 5 4 6 POL . W2_152_1 0_TU1 ; 2

XFOI L Ve rs ion 5 . 0

Calculated polar for : FFA-W2 - 1 5 2

1 Reynolds number fixed

xt r f = 0 . 0 1 0 ( suct ion ) 0 . 1 0 0 (pressu re ) Mach = 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re ( CL) CM S xt r P xt r ------- -------- --------- --------- -------- ------- -------- 5 . 5 0 0 0 0 - 0 . 3 4 1 5 0 0 . 0 1 1 3 8 1 . 0 0 0 0 0 - 0 . 0 4 4 5 0 0 . 62 3 1 0 0 . 0 2 4 2 0 - 5 . 0 0 0 0 0 - 0 . 2 8 4 0 0 0 . 0 1 0 9 2 1 . 0 0 0 0 0 - 0 . 0 4 4 8 0 0 . 6 1 5 3 0 0 . 0 2 7 5 0 - 4 . 5 0 0 0 0 - 0 . 2 2 5 7 0 0 . 0 1 0 6 4 1 . 0 0 0 0 0 - 0 . 0 4 5 3 0 0 . 6 1 0 2 0 0 . 0 2 9 4 0 - 3 . 0 0 0 0 0 - 0 . 0 5 8 6 0 0 . 0 1 1 9 2 1 . 0 0 0 0 0 - 0 . 0 4 6 9 0 0 . 0 1 0 0 0 0 . 0 6 3 5 0 -2 . 5 0 0 0 0 - 0 . 0 0 0 9 0 0 . 0 1 1 7 1 1 . 0 0 0 0 0 - 0 . 0 4 7 4 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 2 . 0 0 0 0 0 0 . 0 5 7 7 0 0 . 0 1 1 7 6 1 . 0 0 0 0 0 - 0 . 0 4 8 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 5 0 0 0 0 0 . 1 1 6 3 0 0 . 0 1 1 8 3 1 . 0 0 0 0 0 - 0 . 0 4 8 6 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 0 0 0 0 0 0 . 1 7 4 6 0 0 . 0 1 1 9 3 1 . 0 0 0 0 0 - 0 . 0 4 9 3 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0

0 . 0 0 0 0 0 0 . 2 9 0 9 0 0 . 0 12 1 8 1 . 0 0 0 0 0 - 0 . 0 5 0 6 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 5 0 0 0 0 0 . 3 4 8 7 0 0 . 0 1 2 3 5 1 . 0 0 0 0 0 - 0 . 0 5 1 2 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 1 . 0 0 0 0 0 0 . 4 0 62 0 0 . 0 12 5 4 1 . 0 0 0 0 0 - 0 . 0 5 1 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 1 . 5 0 0 0 0 0 . 4 6 3 4 0 0 . 0 12 7 6 1 . 0 0 0 0 0 - 0 . 0 5 2 5 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 2 . 0 0 0 0 . 5 2 0 2 0 . 0 1 3 0 1 1 . 0 0 0 0 0 - 0 . 0 5 3 1 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 5 7 6 5 0 . 0 1 3 2 9 1 . 0 0 0 0 0 - 0 . 0 5 3 7 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 3 2 2 0 . 0 1 3 6 1 1 . 0 0 0 0 0 - 0 . 0 5 4 2 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 6 8 7 3 0 . 0 1 3 9 7 1 . 0 0 0 0 0 - 0 . 0 5 4 6 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 7 4 1 6 0 . 0 1 4 37 1 . 0 0 0 0 0 - 0 . 0 5 5 0 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 7 9 4 9 0 . 0 1 4 8 3 1 . 0 0 0 0 0 - 0 . 0552 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 8 4 7 1 0 . 0 1 5 3 4 1 . 0 0 0 0 0 - 0 . 0 5 5 4 0 . 0 1 0 0 0 . 1 0 0 0 5 . 50 0 0 . 8 9 7 7 0 . 0 1 5 9 3 1 . 0 0 0 0 0 - 0 . 0 5 5 4 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 9 4 6 3 0 . 0 1 6 6 0 1 . 0 0 0 0 0 - 0 . 0552 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 0 . 9 9 1 6 0 . 0 1 7 4 2 1 . 0 0 0 0 0 - 0 . 0 5 4 7 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 0 2 3 6 0 . 0 1 8 6 9 1 . 0 0 0 0 0 - 0 . 052 9 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 0 5 8 4 0 . 0 2 0 3 4 1 . 0 0 0 0 0 - 0 . 0 5 2 3 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 0 9 0 5 0 . 0 2 2 3 0 1 . 0 0 0 0 0 - 0 . 0 5 1 6 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 1 2 0 2 0 . 0 2 4 5 6 1 . 0 0 0 0 0 - 0 . 0 5 0 9 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 1 4 8 1 0 . 0 2 7 0 7 1 . 0 0 0 0 0 - 0 . 0 5 0 3 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 1 7 4 3 0 . 0 2 9 8 3 1 . 0 0 0 0 0 - 0 . 0 4 9 7 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 1 9 8 9 0 . 0 3 2 7 9 1 . 0 0 0 0 0 - 0 . 0 4 9 1 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 2 2 2 1 0 . 0 3 5 9 8 1 . 0 0 0 0 0 - 0 . 0 4 8 5 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 2 4 3 9 0 . 0 3 9 3 9 1 . 0 0 0 0 0 - 0 . 0 4 8 0 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 2 6 4 4 0 . 0 4 3 0 2 1 . 0 0 0 0 0 - 0 . 0 4 7 5 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 2 8 4 1 0 . 0 4 6 8 6 1 . 0 0 0 0 0 - 0 . 0 4 7 2 0 . 0 1 0 0 0 . 1 0 0 0 12 . 5 0 0 1 . 3 0 2 5 0 . 0 5 0 9 3 1 . 0 0 0 0 0 - 0 . 0 4 6 9 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 3 1 9 7 0 . 0 5 52 4 1 . 0 0 0 0 0 - 0 . 0 4 6 7 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 3 3 4 7 0 . 0 5 9 9 5 1 . 0 0 0 0 0 - 0 . 0 4 6 6 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 3 4 8 6 0 . 0 7 1 9 0 1 . 0 0 0 0 0 - 0 . 0 4 6 9 0 . 0 0 9 7 0 . 1 0 0 0 1 5 . 0 0 0 1 . 3 5 9 9 0 . 0 7 7 6 1 1 . 0 0 0 0 0 - 0 . 0 4 7 6 0 . 0 0 92 0 . 1 0 0 0 1 5 . 5 0 0 1 . 3 6 8 5 0 . 0 8 3 8 5 1 . 0 0 0 0 0 - 0 . 0 4 8 4 0 . 0 0 8 7 0 . 1 0 0 0 1 6 . 0 0 0 1 . 3 7 4 5 0 . 0 9 0 6 6 1 . 0 0 0 0 0 - 0 . 0 4 9 5 0 . 0 0 8 0 0 . 1 0 0 0 1 6 . 5 0 0 1 . 3 7 5 1 0 . 0 9 8 6 9 1 . 0 0 0 0 0 - 0 . 0 5 1 0 0 . 0 0 7 1 0 . 1 0 0 0 1 7 . 0 0 0 1 . 3 6 1 0 0 . 1 0 9 6 8 1 . 0 0 0 0 0 - 0 . 0 5 3 3 0 . 0 0 6 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 4 7 POL . W2_1 5 2_2 0_9 ; 2

XFOI L Vers ion 5 . 0

Calculated polar for : FFA-W2 - 1 5 2

1 Reynolds number fixed

xt r f = 1 . 0 0 0 ( suct ion) 1 . 0 0 0 (pres sure ) Mach = 0 . 1 5 0 Re = 2 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xt r ------- ------- - --------- -- ------- ---- - --- ----- - - ---- - --- 6 . 0 0 0 0 0 - 0 . 4 0 3 1 0 0 . 0 1 0 7 0 2 . 0 0 0 0 0 - 0 . 0 4 3 7 0 0 . 6 0 5 5 0 0 . 0 1 6 9 0 - 5 . 0 0 0 0 0 - 0 . 2 8 9 4 0 0 . 0 0 9 0 5 2 . 0 0 0 0 0 - 0 . 0 4 3 7 0 0 . 5 9 32 0 0 . 0 2 4 0 0 - 4 . 5 0 0 0 0 - 0 . 2 3 0 4 0 0 . 0 0 8 7 2 2 . 0 0 0 0 0 - 0 . 0 4 4 2 0 0 . 5 8 9 1 0 0 . 02 8 3 0 - 4 . 0 0 0 0 0 - 0 . 1 7 1 0 0 0 . 0 0 8 5 2 2 . 0 0 0 0 0 - 0 . 0 4 4 9 0 0 . 5 8 3 2 0 0 . 0 2 9 9 0 - 3 . 5 0 0 0 0 - 0 . 1 1 1 5 0 0 . 0 0 8 2 5 2 . 0 0 0 0 0 - 0 . 0 4 5 4 0 0 . 5 7 6 3 0 0 . 0 3 8 9 0 - 3 . 0 0 0 0 0 - 0 . 0 52 0 0 0 . 0 0 8 0 0 2 . 0 0 0 0 0 - 0 . 0 4 6 1 0 0 . 5 7 3 0 0 0 . 0 4 6 3 0 - 2 . 5 0 0 0 0 0 . 0 0 7 7 0 0 . 0 0 7 7 7 2 . 0 0 0 0 0 - 0 . 0 4 6 8 0 0 . 5 6 8 6 0 0 . 0 7 2 3 0 - 2 . 0 0 0 0 0 0 . 0 6 7 0 0 0 . 0 0 7 4 4 2 . 0 0 0 0 0 - 0 . 0 4 7 6 0 0 . 5 6 1 0 0 0 . 1 2 0 5 0 - 1 . 5 0 0 0 0 0 . 12 5 9 0 0 . 0 0 6 9 4 2 . 0 0 0 0 0 - 0 . 0 4 8 5 0 0 . 5 5 6 9 0 0 . 2 2 8 6 0 - 1 . 0 0 0 0 0 0 . 1 8 5 1 0 0 . 0 0 6 4 8 2 . 0 0 0 0 0 - 0 . 0 4 9 5 0 0 . 5 52 8 0 0 . 3 4 1 6 0

0 . 0 0 0 0 0 0 . 3 0 3 8 0 0 . 0 0 5 6 5 2 . 0 0 0 0 0 - 0 . 0 5 1 5 0 0 . 5 4 0 4 0 0 . 5 9 9 9 0 0 . 5 0 0 0 0 0 . 3 6 3 9 0 0 . 0 0 5 4 2 2 . 0 0 0 0 0 - 0 . 0 52 5 0 0 . 5 3 7 1 0 0 . 6 8 6 7 0 1 . 0 0 0 0 0 0 . 42 4 0 0 0 . 0 0 5 3 1 2 . 0 0 0 0 0 - 0 . 0 5 3 4 0 0 . 5 3 3 0 0 0 . 7 52 2 0 1 . 5 0 0 0 0 0 . 4 8 4 3 0 0 . 0 0 5 3 3 2 . 0 0 0 0 0 - 0 . 0 5 4 3 0 0 . 52 6 1 0 0 . 7 8 0 5 0 2 . 0 0 0 0 . 5 4 4 5 0 . 0 0 5 3 7 2 . 0 0 0 0 0 - 0 . 0 5 5 2 0 . 52 0 6 0 . 8 0 4 5 2 . 5 0 0 0 . 6 0 4 6 0 . 0 0 5 4 1 2 . 0 0 0 0 0 - 0 . 0 5 6 1 0 . 5 1 6 4 0 . 8 2 3 7 3 . 0 0 0 0 . 6 6 4 7 0 . 0 0 5 4 8 2 . 0 0 0 0 0 - 0 . 0 5 7 1 0 . 5 1 0 1 0 . 8 3 8 4 3 . 5 0 0 0 . 7 2 4 5 0 . 0 0 5 5 8 2 . 0 0 0 0 0 - 0 . 0 5 7 9 0 . 5 0 2 4 0 . 8 5 2 6 4 . 0 0 0 0 . 7 8 4 2 0 . 0 0 5 6 5 2 . 0 0 0 0 0 - 0 . 0 5 8 8 0 . 4 9 7 8 0 . 8 6 8 1 4 . 5 0 0 0 . 8 4 3 2 0 . 0 0 5 8 0 2 . 0 0 0 0 0 - 0 . 0 5 9 6 0 . 4 8 2 5 0 . 8 8 3 4 5 . 0 0 0 0 . 9 0 1 9 0 . 0 0 5 9 5 2 . 0 0 0 0 0 - 0 . 0 6 0 3 0 . 4 7 0 6 0 . 8 9 8 2 5 . 5 0 0 0 . 9 6 0 3 0 . 0 0 6 1 4 2 . 0 0 0 0 0 - 0 . 0 6 1 0 0 . 4 5 9 2 0 . 9 0 9 0 6 . 0 0 0 1 . 0 1 7 9 0 . 0 0 6 3 8 2 . 0 0 0 0 0 - 0 . 0 6 1 6 0 . 4 4 1 9 0 . 92 2 9 6 . 5 0 0 1 . 0 7 3 0 0 . 0 0 6 8 9 2 . 0 0 0 0 0 - 0 . 0 6 1 9 0 . 4 0 4 5 0 . 9 3 7 0 7 . 0 0 0 1 . 1 2 0 6 0 . 0 0 8 1 0 2 . 0 0 0 0 0 - 0 . 0 6 1 3 0 . 3 2 3 5 0 . 9 5 4 8 7 . 5 0 0 1 . 1 6 1 1 0 . 0 0 9 5 7 2 . 0 0 0 0 0 - 0 . 0 5 9 8 0 . 2 3 9 3 0 . 9 8 8 2 8 . 0 0 0 1 . 2 0 3 6 0 . 0 1 1 8 2 2 . 0 0 0 0 0 - 0 . 0 6 0 1 0 . 1 4 4 7 1 . 0 0 0 0 8 . 5 0 0 1 . 2 4 3 6 0 . 0 1 3 4 4 2 . 0 0 0 0 0 - 0 . 0 5 9 3 0 . 0 9 7 1 1 . 0 0 0 0 9 . 0 0 0 1. 2 6 7 0 0 . 0 1 5 6 8 2 . 0 0 0 0 0 - 0 . 0 5 7 2 0 . 0 7 1 6 1 . 0 0 0 0 9 . 5 0 0 1 . 2 8 6 8 0 . 0 1 8 5 7 2 . 0 0 0 0 0 - 0 . 0 5 5 8 0 . 0 5 1 3 1 . 0 0 0 0

1 0 . 0 0 0 1 . 3 0 2 8 0 . 02 2 0 7 2 . 0 0 0 0 0 - 0 . 0 5 4 6 0 . 0 3 6 6 1 . 0 0 0 0 1 0 . 5 0 0 1 . 3 1 7 9 0 . 0 2 5 8 5 2 . 0 0 0 0 0 - 0 . 0 5 3 5 0 . 0 2 6 6 1 . 0 0 0 0 1 1 . 0 0 0 1 . 3 3 6 7 0 . 0 2 9 4 1 2 . 0 0 0 0 0 - 0 . 0 5 2 7 0 . 0 1 8 1 1 . 0 0 0 0 1 1 . 5 0 0 1 . 3 5 0 3 0 . 0 3 3 5 6 2 . 0 0 0 0 0 - 0 . 0 5 1 8 0 . 0 1 5 9 1 . 0 0 0 0 1 2 . 0 0 0 1 . 3 6 7 3 0 . 0 3 7 5 3 2 . 0 0 0 0 0 - 0 . 0 5 1 2 0 . 0 1 2 7 1 . 0 0 0 0 1 2 . 5 0 0 1 . 3 8 2 3 0 . 0 4 1 7 7 2 . 0 0 0 0 0 - 0 . 0 5 0 5 0 . 0 1 0 0 1 . 0 0 0 0 1 3 . 0 0 0 1 . 3 9 8 4 0 . 0 4 6 0 4 2 . 0 0 0 0 0 - 0 . 0 5 0 1 0 . 0 0 9 6 1 . 0 0 0 0 1 3 . 5 0 0 1 . 4 1 1 8 0 . 0 5 0 6 8 2 . 0 0 0 0 0 - 0 . 0 4 9 8 0 . 0 0 9 0 1 . 0 0 0 0 1 4 . 0 0 0 1 . 4 2 3 0 0 . 0 5 5 7 3 2 . 0 0 0 0 0 - 0 . 0 4 9 6 0 . 0 0 8 1 1 . 0 0 0 0 1 5 . 0 0 0 1 . 4 2 0 9 0 . 0 6 9 4 5 2 . 0 0 0 0 0 - 0 . 0 4 9 5 0 . 0 0 5 0 1 . 0 0 0 0 1 5 . 5 0 0 1 . 4 3 3 3 0 . 0 7 4 9 4 2 . 0 0 0 0 0 - 0 . 0 5 0 1 0 . 0 0 4 9 1 . 0 0 0 0 1 6 . 0 0 0 1 . 4 4 4 7 0 . 0 8 0 6 9 2 . 0 0 0 0 0 - 0 . 0 5 0 8 0 . 0 0 4 8 1 . 0 0 0 0 1 6 . 5 0 0 1 . 4 5 3 0 0 . 0 8 7 1 4 2 . 0 0 0 0 0 - 0 . 0 5 1 8 0 . 0 0 4 7 1 . 0 0 0 0 1 7 . 0 0 0 1 . 4 5 9 6 0 . 0 9 4 0 5 2 . 0 0 0 0 0 - 0 . 0 5 3 1 0 . 0 0 4 6 1 . 0 0 0 0

FFA TN 1 9 9 0 - 1 5 4 8

XFOI L Vers ion 5 . 0

Calculated pol a r for : FFA-W2 - 1 52

1 Reynolds numbe r fixed

xtrf = 1 . 0 0 0 ( suct ion ) 1 . 00 0 (pres sure ) Mach = 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncr it

a lpha CL CD Re ( CL ) CM ------- -------- --------- --------- --------- 6 . 0 0 0 0 0 - 0 . 4 0 8 6 0 0 . 0 0 9 3 1 3 . 0 0 0 0 0 - 0 . 0 4 2 7 0 - 5 . 5 0 0 0 0 - 0 . 3 4 8 9 0 0 . 0 0 9 2 6 3 . 0 0 0 0 0 - 0 . 0 4 3 4 0 - 5 . 0 0 0 0 0 - 0 . 2 9 1 2 0 0 . 0 0 8 5 9 3 . 0 0 0 0 0 - 0 . 0 4 3 6 0 - 4 . 5 0 0 0 0 - 0 . 2 3 2 4 0 0 . 0 0 8 0 1 3 . 0 0 0 0 0 - 0 . 0 4 3 8 0 - 4 . 0 0 0 0 0 - 0 . 1 7 2 8 0 0 . 0 0 7 7 7 3 . 0 0 0 0 0 - 0 . 0 4 4 4 0 - 3 . 5 0 0 0 0 - 0 . 1 1 3 0 0 0 . 0 0 7 5 7 3 . 0 0 0 0 0 - 0 . 0 4 5 1 0 - 3 . 0 0 0 0 0 - 0 . 0 52 9 0 0 . 0 0 7 4 1 3 . 0 0 0 0 0 - 0 . 0 4 5 9 0 -2 . 5 0 0 0 0 0 . 0 0 7 0 0 0 . 0 0 7 2 1 3 . 0 0 0 0 0 - 0 . 0 4 6 6 0 -2 . 0 0 0 0 0 0 . 0 6 6 8 0 0 . 0 0 6 9 5 3 . 0 0 0 0 0 - 0 . 0 4 7 5 0 - 1 . 5 0 0 0 0 0 . 1 2 6 3 0 0 . 0 0 6 5 9 3 . 0 0 0 0 0 - 0 . 0 4 8 4 0 - 1 . 0 0 0 0 0 0 . 1 8 5 9 0 0 . 0 0 62 0 3 . 0 0 0 0 0 - 0 . 0 4 9 3 0

0 . 0 0 0 0 0 0 . 3 0 5 3 0 0 . 0 0 5 3 6 3 . 0 0 0 0 0 - 0 . 0 5 1 5 0 0 . 5 0 0 0 0 0 . 3 6 5 4 0 0 . 0 0 5 1 0 3 . 0 0 0 0 0 - 0 . 0 5 2 5 0 1 . 0 0 0 0 0 0 . 4 2 5 7 0 0 . 0 0 4 9 0 3 . 0 0 0 0 0 - 0 . 0 5 3 6 0 1 . 5 0 0 0 . 4 8 6 2 0 . 0 0 4 8 3 3 . 0 0 0 0 0 - 0 . 0 5 5 0 2 . 0 0 0 0 . 5 4 6 8 0 . 0 0 4 8 4 3 . 0 0 0 0 0 - 0 . 0 5 5 6 2 . 5 0 0 0 . 6 0 7 4 0 . 0 0 4 8 9 3 . 0 0 0 0 0 - 0 . 0 5 6 6 3 . 0 0 0 0 . 6 6 7 8 0 . 0 0 4 9 4 3 . 0 0 0 0 0 - 0 . 0 5 7 6 3 . 5 0 0 0 . 7 2 8 1 0 . 0 0 5 0 1 3 . 0 0 0 0 0 - 0 . 0 5 8 6 4 . 0 0 0 0 . 7 8 8 1 0 . 0 0 5 1 2 3 . 0 0 0 0 0 - 0 . 0 5 9 6 4 . 5 0 0 0 . 8 4 7 7 0 . 0 0 52 8 3 . 0 0 0 0 0 - 0 . 0 6 0 5 5 . 0 0 0 0 . 9 0 7 0 0 . 0 0 5 4 7 3 . 0 0 0 0 0 - 0 . 0 6 1 4 5 . 5 0 0 0 . 9 6 5 6 0 . 0 0 5 7 0 3 . 0 0 0 0 0 - 0 . 0 62 2 6 . 0 0 0 1 . 0 2 2 9 0 . 0 0 6 1 1 3 . 0 0 0 0 0 - 0 . 0 6 2 9 7 . 0 0 0 1 . 1 2 1 0 0 . 0 0 8 7 8 3 . 0 0 0 0 0 - 0 . 0 62 8 7 . 5 0 0 1 . 1 6 5 9 0 . 0 1 0 1 4 3 . 0 0 0 0 0 - 0 . 0 62 1 8 . 0 0 0 1 . 2 0 4 5 0 . 0 1 1 52 3 . 0 0 0 0 0 - 0 . 0 6 0 3 8 . 5 0 0 1 . 2 5 0 0 0 . 0 1 2 8 6 3 . 0 0 0 0 0 - 0 . 0 6 0 2 9 . 0 0 0 1 . 2 8 7 2 0 . 0 1 4 2 9 3 . 0 0 0 0 0 - 0 . 0 5 9 1 9 . 5 0 0 1 . 3 0 8 2 0 . 0 1 6 7 6 3 . 0 0 0 0 0 - 0 . 0 5 7 2

1 0 . 0 0 0 1 . 32 6 7 0 . 0 1 9 8 7 3 . 0 0 0 0 0 - 0 . 0 5 5 9 1 0 . 5 0 0 1 . 3 4 8 7 0 . 0 2 2 9 3 3 . 0 0 0 0 0 - 0 . 0 5 5 0 11 . 0 0 0 1 . 3 6 6 0 0 . 0 2 6 5 0 3 . 0 0 0 0 0 - 0 . 0 5 4 0 1 1 . 5 0 0 1 . 3 8 7 2 0 . 0 2 9 8 6 3 . 0 0 0 0 0 - 0 . 0 5 3 2 1 2 . 0 0 0 1 . 4 0 4 0 0 . 0 3 3 7 0 3 . 0 0 0 0 0 - 0 . 0 5 2 5 1 2 . 5 0 0 1 . 4 1 9 7 0 . 0 3 7 7 6 3 . 0 0 0 0 0 - 0 . 0 5 1 7 1 3 . 0 0 0 1 . 4 3 4 4 0 . 0 4 2 0 1 3 . 0 0 0 0 0 - 0 . 0 5 1 1 1 3 . 5 0 0 1. 4 3 7 2 0 . 0 4 7 7 2 3 . 0 0 0 0 0 - 0 . 0 5 02 1 4 . 0 0 0 1 . 4 5 2 0 0 . 0 5 2 2 3 3 . 0 0 0 0 0 - 0 . 0 5 0 0 1 5 . 0 0 0 1 . 4 7 9 2 0 . 0 6 2 0 2 3 . 0 0 0 0 0 - 0 . 0 5 0 0 1 5 . 5 0 0 1 . 4 9 0 6 0 . 0 6 7 2 6 3 . 0 0 0 0 0 - 0 . 0 5 0 2 1 6 . 0 0 0 1 . 5 0 0 6 · o . o 7 2 9 4 3 . 0 0 0 0 0 - 0 . 0 5 0 6 1 6 . 5 0 0 1 . 5 0 8 6 0 . 0 7 9 1 6 3 . 0 0 0 0 0 - 0 . 0 5 1 3 1 7 . 0 0 0 1 . 5 1 5 1 0 . 0 8 5 7 5 3 . 0 0 0 0 0 - 0 . 0 5 2 2

9 . 0 0 0

S xt r -- - - ---0 . 5 9 2 1 0 0 . 5 8 7 4 0 0 . 5 8 0 2 0 0 . 5 7 5 8 0 0 . 5 7 1 7 0 0 . 5 6 6 4 0 0 . 5 5 8 9 0 0 . 5 5 5 9 0 0 . 5 52 1 0 0 . 5 4 5 1 0 0 . 5 3 9 6 0 0 . 5 3 1 7 0 0 . 52 4 8 0 0 . 52 0 0 0 0 . 5 1 7 0 0 . 5 0 9 9 0 . 5 0 2 5 0 . 4 9 8 4 0 . 4 9 12 0 . 4 8 1 0 0 . 4 6 4 8 0 . 4 4 7 9 0 . 4 3 0 1 0 . 4 0 2 5 0 . 2 2 2 0 0 . 1 5 6 6 0 . 1 0 0 5 0 . 0 6 9 3 0 . 0 4 6 9 0 . 0 32 8 0 . 0 2 4 2 0 . 0 1 7 4 0 . 0 1 4 2 0 . 0 1 0 6 0 . 0 0 9 7 0 . 0 0 8 9 0 . 0 0 7 9 0 . 0 0 5 1 0 . 0 0 5 0 0 . 0 0 4 8 0 . 0 0 4 6 0 . 0 0 4 4 0 . 0 0 4 3 0 . 0 0 4 0

P xt r -------

0 . 0 1 7 0 0 0 . 0 1 7 3 0 0 . 0 1 8 7 0 0 . 0 2 6 0 0 0 . 0 2 9 5 0 0 . 0 3 3 4 0 0 . 0 4 2 5 0 0 . 0 5 6 7 0 0 . 0 9 1 3 0 0 . 1 5 9 5 0 0 . 2 5 8 9 0 0 . 5 0 4 8 0 0 . 6 0 3 1 0 0 . 6 9 1 3 0

0 . 7 4 0 0 0 . 7 7 2 1 0 . 7 92 3 0 . 8 1 1 7 0 . 8 2 9 2 0 . 8 4 5 1 0 . 8 5 9 0 0 . 8 7 0 9 0 . 8 8 7 1 0 . 9 0 0 8 0 . 92 6 7 0 . 9 4 4 8 0 . 9 7 7 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0 1 . 0 0 0 0

POL . W2_1 52_30_9 ; 4

FFA TN 1 9 9 0 - 1 5 4 9

XFOIL Ve rsion 5 . 0

Calculated polar for : FFA-W2 - 1 5 2

1 Reynolds number f ixed

xt rf = 0 . 0 1 0 ( suct ion) 0 . 1 0 0 (pressure ) Mach =

a lpha - - - - - - -

2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 50 0 1 3 . 0 0 0 1 5 . 0 0 0 1 5 . 5 0 0 1 6 . 0 0 0 1 6 . 5 0 0 1 7 . 0 0 0

1 . 5 0 0 1 . 0 0 0 0 . 5 0 0 0 . 0 0 0

- 1 . 0 0 0 - 1 . 5 0 0 -2 . 0 0 0 -2 . 5 0 0 - 3 . 0 0 0 - 3 . 5 0 0 - 4 . 0 0 0 - 4 . 5 0 0 - 5 . 0 0 0 - 5 . 5 0 0 - 6 . 0 0 0

0 . 1 5 0

CL - -------

0 . 52 9 7 0 . 5 8 7 7 0 . 6 4 52 0 . 7 02 4 0 . 7 5 9 1 0 . 8 1 5 2 0 . 8 7 0 6 0 . 9 2 5 3 0 . 9 7 9 0 1 . 0 3 1 6 1 . 0 8 2 6 1 . 1 3 1 7 1 . 1 7 7 0 1 . 2 0 6 9 1 . 2 4 0 1 1 . 2 7 0 8 1 . 2 9 9 1 1 . 3 2 5 3 1 . 3 4 9 7 1 . 3 7 2 4 1 . 3 92 0 1 . 4 0 7 5 1 . 4 2 2 3 1 . 4 6 7 3 1 . 4 7 8 8 1 . 4 8 9 7 1 . 4 9 8 0 1 . 5 0 4 5 0 . 4 7 1 5 0 . 4 1 3 0 0 . 3 5 4 3 0 . 2 9 5 4 0 . 1 7 7 1 0 . 1 1 7 8 0 . 0 5 8 6

- 0 . 0 0 02 - 0 . 0 5 9 3 - 0 . 1 1 3 0 - 0 . 1 7 2 8 - 0 . 2 3 2 4 - 0 . 2 9 1 2 - 0 . 3 4 8 9 - 0 . 4 0 8 6

Re = 3 . 0 0 0 e 6 Ncr it

CD Re ( CL ) CM --------- --- ------ --------

0 . 0 1 0 6 3 3 . 0 0 0 0 0 - 0 . 0 5 4 0 0 . 0 1 0 8 5 3 . 0 0 0 0 0 - 0 . 0 5 4 7 0 . 0 1 1 0 9 3 . 0 0 0 0 0 - 0 . 0 5 5 4 0 . 0 1 1 3 6 3 . 0 0 0 0 0 - 0 . 0 5 6 1 0 . 0 1 1 6 6 3 . 0 0 0 0 0 - 0 . 0 5 6 7 0 . 0 1 1 9 8 3 . 0 0 0 0 0 - 0 . 0 5 7 3 0 . 0 12 3 4 3 . 0 0 0 0 0 - 0 . 0 5 7 8 0 . 0 12 7 4 3 . 0 0 0 0 0 - 0 . 0 5 8 2 0 . 0 1 3 1 9 3 . 0 0 0 0 0 - 0 . 0 5 8 5 0 . 0 1 3 6 8 3 . 0 0 0 0 0 - 0 . 0 5 8 7 0 . 0 1 4 2 4 3 . 0 0 0 0 0 - 0 . 0 5 8 7 0 . 0 1 4 8 8 3 . 0 0 0 0 0 - 0 . 0 5 8 5 0 . 0 1 5 6 6 3 . 0 0 0 0 0 - 0 . 0 5 7 9 0 . 0 1 6 9 8 3 . 0 0 0 0 0 - 0 . 0 5 5 8 0 . 0 1 8 6 6 3 . 0 0 0 0 0 - 0 . 0 5 4 9 0 . 0 2 0 6 9 3 . 0 0 0 0 0 - 0 . 0 5 4 1 0 . 0 2 3 0 3 3 . 0 0 0 0 0 - 0 . 0 5 3 3 0 . 0 2 5 6 4 3 . 0 0 0 0 0 - 0 . 0 52 5 0 . 0 2 8 5 4 3 . 0 0 0 0 0 - 0 . 0 5 1 7 0 . 0 3 1 6 6 3 . 0 0 0 0 0 - 0 . 0 5 1 0 0 . 0 3 5 1 7 3 . 0 0 0 0 0 - 0 . 0 5 0 3 0 . 0 3 9 1 5 3 . 0 0 0 0 0 - 0 . 0 4 9 5 0 . 0 4 3 3 6 3 . 0 0 0 0 0 - 0 . 0 4 8 9 0 . 0 6 3 1 7 3 . 0 0 0 0 0 - 0 . 0 4 7 9 0 . 0 6 8 4 4 3 . 0 0 0 0 0 - 0 . 0 4 8 1 0 . 0 7 3 9 5 3 . 0 0 0 0 0 - 0 . 0 4 8 5 0 . 0 8 0 1 1 3 . 0 0 0 0 0 - 0 . 0 4 9 3 0 . 0 8 6 6 5 3 . 0 0 0 0 0 - 0 . 0 5 0 2 0 . 0 1 0 4 4 3 . 0 0 0 0 0 - 0 . 0 5 3 2 0 . 0 1 0 2 6 3 . 0 0 0 0 0 - 0 . 0 5 2 4 0 . 0 1 0 1 0 3 . 0 0 0 0 0 - 0 . 0 5 1 6 0 . 0 0 9 9 6 3 . 0 0 0 0 0 - 0 . 0 5 0 9 0 . 0 0 9 7 4 3 . 0 0 0 0 0 - 0 . 0 4 93 0 . 0 0 9 6 5 3 . 0 0 0 0 0 - 0 . 0 4 8 5 0 . 0 0 9 6 4 3 . 0 0 0 0 0 - 0 . 0 4 7 8 0 . 0 0 9 7 9 3 . 0 0 0 0 0 - 0 . 0 4 7 0 0 . 0 0 9 8 7 3 . 0 0 0 0 0 - 0 . 0 4 6 4 0 . 0 0 7 5 7 3 . 0 0 0 0 0 - 0 . 0 4 5 1 0 . 0 0 7 7 7 3 . 0 0 0 0 0 - 0 . 0 4 4 4 0 . 0 0 8 0 1 3 . 0 0 0 0 0 - 0 . 0 4 3 8 0 . 0 0 8 5 9 3 . 0 0 0 0 0 - 0 . 0 4 3 6 0 . 0 0 92 6 3 . 0 0 0 0 0 - 0 . 0 4 3 4 0 . 0 0 9 3 1 3 . 0 0 0 0 0 - 0 . 0 4 2 7

POL . W2_1 52_3 0_TU1 ; 2

9 . 0 0 0

S xt r P xt r ------- -------0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 0 9 8 0 . 1 0 0 0 0 . 0 0 9 0 0 . 1 0 0 0 0 . 0 0 8 1 0 . 1 0 0 0 0 . 0 0 4 8 0 . 1 0 0 0 0 . 0 0 4 7 0 . 1 0 0 0 0 . 0 0 4 5 0 . 1 0 0 0 0 . 0 0 4 3 0 . 1 0 0 0 0 . 0 0 4 1 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 0 8 5 8 0 . 0 1 0 0 0 . 0 5 4 7 0 . 0 1 0 0 0 . 0 4 1 8 0 . 5 6 6 4 0 . 0 3 3 4 0 . 5 7 1 7 0 . 0 2 9 5 0 . 5 7 5 8 0 . 02 6 0 0 . 5 8 0 2 0 . 0 1 8 7 0 . 5 8 7 4 0 . 0 1 7 3 0 . 5 9 2 1 0 . 0 1 7 0

FFA TN 1 9 9 0 - 1 5 5 0

XFOI L Vers ion 5 . 0

Calculated polar for : FFA-W2 -2 1 0

1 Reynolds number fixed

xt rf = 1 . 0 0 0 ( suction) 1 . 0 0 0 (pre s sure ) Mach = 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it

a lpha CL CD Re (CL) CM ------- -------- ------ - -- --------- - - ------- 6 . 0 0 0 0 0 - 0 . 5 6 9 0 0 0 . 0 0 8 8 9 1 . 0 0 0 0 0 - 0 . 0 2 4 7 0 - 5 . 5 0 0 0 0 - 0 . 5 0 6 8 0 0 . 0 0 8 5 8 1 . 0 0 0 0 0 - 0 . 0 2 6 1 0 - 5 . 0 0 0 0 0 - 0 . 4 4 4 5 0 0 . 0 0 8 3 8 1 . 0 0 0 0 0 - 0 . 0 2 7 4 0 - 4 . 5 0 0 0 0 - 0 . 3 8 1 8 0 0 . 0 0 8 2 9 1 . 0 0 0 0 0 - 0 . 0 2 8 6 0 - 4 . 0 0 0 0 0 - 0 . 3 1 9 1 0 0 . 0 0 8 2 1 1 . 0 0 0 0 0 - 0 . 0 2 9 9 0 - 3 . 5 0 0 0 0 - 0 . 2 5 6 4 0 0 . 0 0 8 1 3 1 . 0 0 0 0 0 - 0 . 0 3 1 2 0 - 3 . 0 0 0 0 0 - 0 . 1 9 3 7 0 0 . 0 0 8 1 2 1 . 0 0 0 0 0 - 0 . 0 3 2 5 0 - 2 . 5 0 0 0 0 - 0 . 1 3 1 0 0 0 . 0 0 8 0 5 1 . 0 0 0 0 0 - 0 . 0 3 3 7 0 - 2 . 0 0 0 0 0 - 0 . 0 6 8 2 0 0 . 0 0 8 0 4 1 . 0 0 0 0 0 - 0 . 0 3 5 0 0 - 1 . 5 0 0 0 0 - 0 . 0 0 5 7 0 0 . 0 0 8 0 7 1 . 0 0 0 0 0 - 0 . 0 3 6 3 0 - 1 . 0 0 0 0 0 0 . 0 5 7 0 0 0 . 0 0 8 0 3 1 . 0 0 0 0 0 - 0 . 0 3 7 6 0

0 . 0 0 0 0 0 0 . 1 8 1 9 0 0 . 0 0 8 1 3 1 . 0 0 0 0 0 - 0 . 0 4 0 0 0 0 . 5 0 0 0 0 0 . 2 4 4 4 0 0 . 0 0 8 12 1 . 0 0 0 0 0 - 0 . 0 4 1 3 0 1 . 0 0 0 0 0 0 . 3 0 6 8 0 0 . 0 0 8 1 9 1 . 0 0 0 0 0 - 0 . 0 4 2 5 0 1 . 5 0 0 0 0 0 . 3 6 8 9 0 0 . 0 0 8 2 9 1 . 0 0 0 0 0 - 0 . 0 4 3 7 0 2 . 0 0 0 0 . 4 3 1 0 0 . 0 0 8 3 3 1 . 0 0 0 0 0 - 0 . 0 4 4 9 2 . 5 0 0 0 . 4 9 3 0 0 . 0 0 8 4 5 1 . 0 0 0 0 0 - 0 . 0 4 6 1 3 . 0 0 0 0 . 5 5 4 7 0 . 0 0 8 5 7 1 . 0 0 0 0 0 - 0 . 0 4 7 2 3 . 5 0 0 0 . 6 1 6 4 0 . 0 0 8 6 6 1 . 0 0 0 0 0 - 0 . 0 4 8 3 4 . 0 0 0 0 . 6 7 7 7 0 . 0 0 8 8 4 1 . 0 0 0 0 0 - 0 . 0 4 9 3 4 . 5 0 0 0 . 7 3 9 0 0 . 0 0 8 9 7 1 . 0 0 0 0 0 - 0 . 0 5 0 3 5 . 0 0 0 0 . 8 0 0 1 0 . 0 0 9 1 2 1 . 0 0 0 0 0 - 0 . 0 5 1 4 5 . 5 0 0 0 . 8 6 0 8 0 . 0 0 9 3 2 1 . 0 0 0 0 0 - 0 . 0 52 3 6 . 0 0 0 0 . 9 2 11 0 . 0 0 9 5 6 1 . 0 0 0 0 0 - 0 . 0 5 32 6 . 5 0 0 0 . 9 8 1 0 0 . 0 0 9 7 9 1 . 0 0 0 0 0 - 0 . 0 5 4 0 7 . 0 0 0 1 . 0 4 0 2 0 . 0 1 0 1 1 1 . 0 0 0 0 0 - 0 . 0 5 4 8 7 . 5 0 0 1 . 0 9 8 2 0 . 0 1 0 5 3 1 . 0 0 0 0 0 - 0 . 0 5 5 4 8 . 0 0 0 1 . 1 5 5 0 0 . 0 1 1 0 3 1 . 0 0 0 0 0 - 0 . 0 5 5 8 8 . 5 0 0 1 . 2 0 9 2 0 . 0 1 1 7 3 1 . 0 0 0 0 0 - 0 . 0 5 6 0 9 . 0 0 0 1 . 2 5 32 0 . 0 1 3 2 4 1 . 0 0 0 0 0 - 0 . 0 5 52 9 . 5 0 0 1 . 2 8 7 3 0 . 0 1 5 3 0 1 . 0 0 0 0 0 - 0 . 0 5 3 5

1 0 . 0 0 0 1 . 3 0 4 0 0 . 0 1 7 7 9 1 . 0 0 0 0 0 - 0 . 0 5 0 0 1 0 . 5 0 0 1 . 3 0 7 4 0 . 0 2 1 6 9 1 . 0 0 0 0 0 - 0 . 0 4 7 8 1 1 . 0 0 0 1 . 3 0 9 3 0 . 0 2 6 6 8 1 . 0 0 0 0 0 - 0 . 0 4 7 2 1 1 . 5 0 0 1 . 3 0 8 4 0 . 0 3 2 3 8 1 . 0 0 0 0 0 - 0 . 0 4 7 0 1 2 . 0 0 0 1 . 3 1 5 0 0 . 0 3 7 5 5 1 . 0 0 0 0 0 - 0 . 0 4 7 0 12 . 5 0 0 1 . 3 1 8 5 0 . 0 4 3 1 9 1 . 0 0 0 0 0 - 0 . 0 4 7 0 1 3 . 0 0 0 1 . 3 2 6 9 0 . 0 4 8 5 7 1 . 0 0 0 0 0 - 0 . 0 4 7 3 1 3 . 5 0 0 1 . 3 3 2 5 0 . 0 5 4 3 3 1 . 0 0 0 0 0 - 0 . 0 4 7 7 1 4 . 0 0 0 1 . 3 3 7 5 0 . 0 6 0 3 6 1 . 0 0 0 0 0 - 0 . 0 4 8 3 1 4 . 5 0 0 1 . 3 4 5 1 0 . 0 6 6 3 1 1 . 0 0 0 0 0 - 0 . 0 4 9 1 1 5 . 0 0 0 1 . 3 4 8 2 0 . 0 7 2 9 8 1 . 0 0 0 0 0 - 0 . 0 5 0 0 1 5 . 5 0 0 1 . 3 5 6 7 0 . 0 7 9 11 1 . 0 0 0 0 0 - 0 . 0 5 1 1 1 6 . 0 0 0 1 . 3 6 33 0 . 0 8 5 6 9 1 . 0 0 0 0 0 - 0 . 0 52 5 1 6 . 5 0 0 1 . 3 6 7 6 0 . 0 92 6 8 1 . 0 0 0 0 0 - 0 . 0 5 3 9 1 7 . 0 0 0 1 . 3 7 0 6 0 . 1 0 0 2 4 1 . 0 0 0 0 0 - 0 . 0 5 5 8

POL . W2_2 1 0_1 0_9 ; 2

9 . 0 0 0

S xt r P xt r ------ - -------0 . 5 8 4 7 0 0 . 3 8 7 8 0 0 . 57 5 6 0 0 . 4 1 4 8 0 0 . 5 6 8 3 0 0 . 4 4 3 2 0 0 . 5 6 0 1 0 0 . 4 5 4 5 0 0 . 5 5 1 6 0 0 . 4 6 1 4 0 0 . 5 4 5 7 0 0 . 4 7 0 1 0 0 . 5 3 5 7 0 0 . 4 7 5 3 0 0 . 5 3 0 4 0 0 . 4 8 3 9 0 0 . 52 4 0 0 0 . 4 9 0 1 0 0 . 5 1 5 4 0 0 . 4 9 4 7 0 0 . 5 1 0 0 0 0 . 5 0 3 3 0 0 . 4 9 5 6 0 0 . 5 1 3 8 0 0 . 4 9 0 1 0 0 . 52 1 7 0 0 . 4 8 3 0 0 0 . 52 7 8 0 0 . 4 7 5 7 0 0 . 5 3 2 2 0 0 . 4 7 0 7 0 . 5 4 0 3 0 . 4 62 2 0 . 5 4 5 9 0 . 4 5 6 4 0 . 5 5 0 4 0 . 4 5 0 5 0 . 5 57 9 0 . 4 4 0 7 0 . 5 6 3 9 0 . 4 3 5 6 0 . 5 6 8 8 0 . 42 8 0 0 . 5 7 5 5 0 . 4 1 8 5 0 . 5 8 1 8 0 . 4 0 3 9 0 . 5 8 6 5 0 . 3 9 4 2 0 . 5 9 3 0 0 . 3 7 9 1 0 . 5 9 9 8 0 . 3 5 9 6 0 . 6 0 4 7 0 . 3 3 9 9 0 . 6 1 0 9 0 . 3 1 0 8 0 . 6 1 8 0 0 . 2 5 1 0 0 . 62 2 9 0 . 1 92 5 0 . 62 7 9 0 . 1 4 8 3 0 . 6 3 6 1 0 . 11 6 8 0 . 6 4 1 1 0 . 0 9 6 4 0 . 6 4 5 4 0 . 0 7 8 0 0 . 6 5 3 4 0 . 0 6 53 0 . 6 5 8 7 0 . 0 5 9 0 0 . 6 6 3 6 0 . 0 4 9 7 0 . 6 7 1 4 0 . 0 4 7 2 0 . 6 7 7 0 0 . 0 4 3 4 0 . 6 8 1 7 0 . 0 3 8 4 0 . 6 9 0 2 0 . 0 3 4 1 0 . 6 9 6 1 0 . 0 3 3 1 0 . 7 0 1 1 0 . 0 3 1 8 0 . 7 0 9 8 0 . 0 3 0 1 0 . 7 1 6 8 0 . 0 2 8 0 0 . 7 2 42

FFA TN 1 9 9 0 - 1 5 5 1 POL . W2_2 1 0_10_TU1 ; 2

XFOI L Vers ion S . O

Calculated polar for : FFA-W2-2 1 0

1 Reynolds number fixed

xt rf -= 0 . 0 1 0 ( suct ion) 0 . 1 0 0 (pre s sure ) Mach -= 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Nc r it 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xt r - -- -- - - -------- --------- - - ------- --- - -- - - ------- -------- 4 . 0 0 0 0 0 - 0 . 32 2 8 0 0 . 0 1 3 7 5 1 . 0 0 0 0 0 - 0 . 0 2 6 6 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 5 0 0 0 0 - 0 . 2 6 1 9 0 0 . 0 1 3 62 1 . 0 0 0 0 0 - 0 . 0 2 7 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 0 0 0 0 0 - 0 . 2 0 1 0 0 0 . 0 13 52 1 . 0 0 0 0 0 - 0 . 02 9 1 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 -2 . 5 0 0 0 0 - 0 . 1 4 0 0 0 0 . 0 1 3 4 5 1 . 0 0 0 0 0 - 0 . 0 3 0 4 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 2 . 0 0 0 0 0 - 0 . 0 7 9 0 0 0 . 0 1 3 4 1 1 . 0 0 0 0 0 - 0 . 0 3 1 7 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 5 0 0 0 0 - 0 . 0 1 8 1 0 0 . 0 1 3 3 9 1 . 0 0 0 0 0 - 0 . 0 3 2 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 0 0 0 0 0 0 . 0 4 2 8 0 0 . 0 1 3 4 1 1 . 0 0 0 0 0 - 0 . 0 3 4 2 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0

0 . 0 0 0 0 0 0 . 1 6 4 1 0 0 . 0 1 3 5 1 1 . 0 0 0 0 0 - 0 . 0 3 6 5 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 5 0 0 0 0 0 . 22 4 5 0 0 . 0 1 3 6 1 1 . 0 0 0 0 0 - 0 . 0 3 7 7 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 1 . 0 0 0 0 0 0 . 2 8 4 6 0 0 . 0 1 3 7 3 1 . 0 0 0 0 0 - 0 . 0 3 8 8 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 1 . 5 0 0 0 0 0 . 3 4 4 4 0 0 . 0 1 3 8 9 1 . 0 0 0 0 0 - 0 . 0 3 9 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 2 . 0 0 0 0 . 4 0 3 9 0 . 0 1 4 0 8 1 . 0 0 0 0 0 - 0 . 0 4 0 9 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 4 6 3 0 0 . 0 1 4 3 0 1 . 0 0 0 0 0 - 0 . 0 4 1 8 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 52 1 5 0 . 0 1 4 5 5 1 . 0 0 0 0 0 - 0 . 0 4 2 7 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 5 7 95 0 . 0 1 4 8 5 1 . 0 0 0 0 0 - 0 . 0 4 3 6 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 6 3 6 9 0 . 0 1 5 1 8 1 . 0 0 0 0 0 - 0 . 0 4 4 3 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 6 9 3 4 0 . 0 1 5 5 6 1 . 0 0 0 0 0 - 0 . 0 4 4 9 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 7 4 9 0 0 . 0 1 6 0 0 1 . 0 0 0 0 0 - 0 . 0 4 5 5 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 8 0 3 5 0 . 0 1 6 4 9 1 . 0 0 0 0 0 - 0 . 0 4 5 9 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 8 5 6 6 0 . 0 1 7 0 5 1 . 0 0 0 0 0 - 0 . 0 4 6 1 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 0 . 9 0 7 8 0 . 0 1 7 7 0 1 . 0 0 0 0 0 - 0 . 0 4 62 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 0 . 9 5 6 7 0 . 0 1 8 4 5 1 . 0 0 0 0 0 - 0 . 0 4 6 0 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 0 0 2 1 0 . 0 1 93 4 1 . 0 0 0 0 0 - 0 . 0 4 5 6 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 0 3 0 7 0 . 0 2 0 6 8 1 . 0 0 0 0 0 - 0 . 0 4 3 3 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 0 62 3 0 . 0 2 2 7 4 1 . 0 0 0 0 0 - 0 . 0 4 3 0 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 0 9 0 3 0 . 0 2 5 3 4 1 . 0 0 0 0 0 - 0 . 0 4 3 1 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 1 1 53 0 . 0 2 8 3 7 1 . 0 0 0 0 0 - 0 . 0 4 32 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 1 3 7 9 0 . 0 3 1 7 9 1 . 0 0 0 0 0 - 0 . 0 4 3 4 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 1 5 7 9 0 . 0 3 5 5 4 1 . 0 0 0 0 0 - 0 . 0 4 3 5 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 1 7 6 7 0 . 0 3 9 5 3 1 . 0 0 0 0 0 - 0 . 0 4 3 8 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 1 93 6 0 . 0 4 3 8 1 1 . 0 0 0 0 0 - 0 . 0 4 4 0 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 2 0 9 5 0 . 0 4 8 3 5 1 . 0 0 0 0 0 - 0 . 0 4 4 5 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 2 2 4 2 0 . 0 5 3 1 0 1 . 0 0 0 0 0 - 0 . 0 4 4 9 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 2 3 7 8 0 . 0 5 8 0 8 1 . 0 0 0 0 0 - 0 . 0 4 5 5 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 2 5 1 1 0 . 0 6 3 2 5 1 . 0 0 0 0 0 - 0 . 0 4 62 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 2 6 3 5 0 . 0 6 8 5 9 1 . 0 0 0 0 0 - 0 . 0 4 7 0 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 2 7 5 1 0 . 0 7 4 2 4 1 . 0 0 0 0 0 - 0 . 0 4 8 0 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 2 8 62 0 . 0 8 0 1 5 1 . 0 0 0 0 0 - 0 . 0 4 92 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 5 0 0 1 . 2 9 6 9 0 . 0 8 62 1 1 . 0 0 0 0 0 - 0 . 0 5 0 4 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 0 0 0 1 . 3 0 7 4 0 . 0 92 3 7 1 . 0 0 0 0 0 - 0 . 0 5 1 8 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 5 0 0 1 . 3 1 6 6 0 . 0 9 9 0 2 1 . 0 0 0 0 0 - 0 . 0 5 3 4 0 . 0 1 0 0 0 . 1 0 0 0 1 7 . 0 0 0 1 . 32 5 0 0 . 1 0 5 9 5 1 . 0 0 0 0 0 - 0 . 0 5 5 3 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 5 2 POL . W2_2 1 0_20_9 ; 2

XFOI L Version 5 . 0

Ca lculated polar for : FFA-W2- 2 1 0

1 Reynolds number fixed

xt rf = 1 . 0 0 0 ( suct ion} 1 . 0 0 0 (pressure ) Mach == 0 . 1 5 0 Re = 2 . 0 0 0 e 6 Ncr it 9 . 0 0 0

alpha CL CD Re (CL) CM S xtr P xt r ----- - - -------- --------- --------- -------- ------- -------- 6 . 0 0 0 0 0 - 0 . 5 6 7 4 0 0 . 0 0 7 8 9 2 . 0 0 0 0 0 - 0 . 0 2 5 0 0 0 . 5 5 5 4 0 0 . 32 1 4 0 - 5 . 5 0 0 0 0 - 0 . 5 0 5 2 0 0 . 0 0 7 4 0 2 . 0 0 0 0 0 - 0 . 0 2 6 5 0 0 . 5 4 9 0 0 0 . 3 6 1 0 0 - 5 . 0 0 0 0 0 - 0 . 4 4 2 8 0 0 . 0 0 7 02 2 . 0 0 0 0 0 - 0 . 02 8 0 0 0 . 5 4 1 4 0 0 . 3 9 9 0 0 - 4 . 5 0 0 0 0 - 0 . 3 8 0 1 0 0 . 0 0 6 7 8 2 . 0 0 0 0 0 - 0 . 0 2 9 4 0 0 . 5 3 3 4 0 0 . 42 8 9 0 - 4 . 0 0 0 0 0 - 0 . 3 1 7 2 0 0 . 0 0 6 7 0 2 . 0 0 0 0 0 - 0 . 0 3 0 7 0 0 . 52 8 2 0 0 . 4 3 8 3 0 - 3 . 5 0 0 0 0 - 0 . 2 5 4 1 0 0 . 0 0 6 6 4 2 . 0 0 0 0 0 - 0 . 0 3 2 0 0 0 . 5 1 8 4 0 0 . 4 4 8 4 0 - 3 . 0 0 0 0 0 - 0 . 1 9 1 1 0 0 . 0 0 6 5 9 2 . 0 0 0 0 0 - 0 . 0 3 3 3 0 0 . 5 1 3 1 0 0 . 4 5 4 5 0 -2 . 5 0 0 0 0 - 0 . 1 2 8 2 0 0 . 0 0 6 5 6 2 . 0 0 0 0 0 - 0 . 0 3 4 5 0 0 . 5 0 7 6 0 0 . 4 6 0 5 0 - 2 . 0 0 0 0 0 - 0 . 0 6 5 1 0 0 . 0 0 6 5 5 2 . 0 0 0 0 0 - 0 . 0 3 5 9 0 0 . 4 9 7 3 0 0 . 4 6 9 1 0 - 1 . 5 0 0 0 0 - 0 . 0 0 2 2 0 0 . 0 0 6 5 3 2 . 0 0 0 0 0 - 0 . 0 3 7 1 0 0 . 4 9 3 3 0 0 . 4 7 4 8 0 - 1 . 0 0 0 0 0 0 . 0 6 0 7 0 0 . 0 0 6 5 4 2 . 0 0 0 0 0 - 0 . 0 3 8 4 0 0 . 4 8 7 6 0 0 . 4 8 0 4 0

0 . 0 0 0 0 0 0 . 1 8 6 4 0 0 . 0 0 6 5 7 2 . 0 0 0 0 0 - 0 . 0 4 1 0 0 0 . 4 7 4 1 0 0 . 4 9 3 6 0 0 . 5 0 0 0 0 0 . 2 4 92 0 0 . 0 0 6 6 0 2 . 0 0 0 0 0 - 0 . 0 4 2 3 0 0 . 4 6 8 3 0 0 . 4 9 9 9 0 1 . 0 0 0 0 0 0 . 3 1 1 9 0 0 . 0 0 6 6 6 2 . 0 0 0 0 0 - 0 . 0 4 3 5 0 0 . 4 5 9 0 0 0 . 5 0 7 3 0 1 . 5 0 0 0 0 0 . 3 7 4 5 0 0 . 0 0 6 7 0 2 . 0 0 0 0 0 - 0 . 0 4 4 8 0 0 . 4 5 5 1 0 0 . 5 1 2 4 0 2 . 0 0 0 0 . 4 3 7 0 0 . 0 0 6 7 7 2 . 0 0 0 0 0 - 0 . 0 4 6 0 0 . 4 4 8 1 0 . 5 1 7 5 2 . 5 0 0 0 . 4 9 9 5 0 . 0 0 6 8 5 2 . 0 0 0 0 0 - 0 . 0 4 7 2 0 . 4 4 0 0 0 . 52 5 2 3 . 0 0 0 0 . 5 6 1 8 0 . 0 0 6 9 2 2 . 0 0 0 0 0 - 0 . 0 4 8 4 0 . 4 3 5 3 0 . 5 3 0 6 3 . 5 0 0 0 . 62 3 9 0 . 0 0 7 0 3 2 . 0 0 0 0 0 - 0 . 0 4 9 6 0 . 4272 0 . 5 3 4 9 4 . 0 0 0 0 . 6 8 6 0 0 . 0 0 71 4 2 . 0 0 0 0 0 - 0 . 0 5 0 7 0 . 4 1 9 6 0 . 5 4 3 8 4 . 5 0 0 0 . 7 4 7 7 0 . 0 0 7 2 8 2 . 0 0 0 0 0 - 0 . 0 5 1 8 0 . 4 1 2 1 0 . 5 4 8 7 5 . 0 0 0 0 . 8 0 92 0 . 0 0 7 4 5 2 . 0 0 0 0 0 - 0 . 0 5 2 8 0 . 4 0 0 9 0 . 5 5 2 3 5 . 5 0 0 0 . 8 7 0 3 0 . 0 0 7 6 4 2 . 0 0 0 0 0 - 0 . 0 5 3 9 0 . 3 8 6 6 0 . 5 6 1 6 6 . 0 0 0 0 . 9 3 1 0 0 . 0 0 7 8 8 2 . 0 0 0 0 0 - 0 . 0 5 4 8 0 . 3 7 5 9 0 . 5 6 6 8 6 . 5 0 0 0 . 9 9 1 1 0 . 0 0 8 1 8 2 . 0 0 0 0 0 - 0 . 0 5 5 7 0 . 3 5 9 0 0 . 57 0 5 7 . 0 0 0 1 . 0 4 9 7 0 . 0 0 8 62 2 . 0 0 0 0 0 - 0 . 0 5 6 4 0 . 3 3 4 1 0 . 5 7 9 3 7 . 5 0 0 1 . 1 0 7 4 0 . 0 0 9 1 3 2 . 0 0 0 0 0 - 0 . 0 5 7 0 0 . 3 0 6 8 0 . 5 8 4 8 8 . 0 0 0 1 . 1 5 9 3 0 . 0 1 0 2 0 2 . 0 0 0 0 0 - 0 . 0 5 7 1 0 . 2 5 57 0 . 5 8 8 6 8 . 5 0 0 1 . 2 0 7 3 0 . 0 1 1 5 3 2 . 0 0 0 0 0 - 0 . 0 5 6 7 0 . 2 0 3 1 0 . 5 9 5 7 9 . 0 0 0 1 . 2 5 0 7 0 . 0 1 3 0 9 2 . 0 0 0 0 0 - 0 . 0 5 5 9 0 . 1 5 1 6 0 . 6 0 2 4 9 . 5 0 0 1 . 2 8 9 8 0 . 0 1 4 7 5 2 . 0 0 0 0 0 - 0 . 0 5 4 6 0 . 1 1 2 5 0 . 6 0 6 5

1 0 . 0 0 0 1 . 3 2 0 9 0 . 0 1 6 6 1 2 . 0 0 0 0 0 - 0 . 0 5 2 5 0 . 0 8 0 9 0 . 6 1 2 5 1 0 . 5 0 0 1 . 3 3 7 2 0 . 0 1 8 9 8 2 . 0 0 0 0 0 - 0 . 0 4 9 7 0 . 0 6 5 9 0 . 6 1 92 1 1 . 0 0 0 1 . 3 5 1 3 0 . 0 2 2 5 8 2 . 0 0 0 0 0 - 0 . 0 4 8 9 0 . 0 5 7 6 0 . 62 4 3 1 1 . 5 0 0 1 . 3 6 7 4 0 . 0 2 6 42 2 . 0 0 0 0 0 - 0 . 0 4 8 7 0 . 0 4 9 1 0 . 62 8 9 1 2 . 0 0 0 1 . 3 7 6 5 0 . 0 3 1 1 3 2 . 0 0 0 0 0 - 0 . 0 4 8 5 0 . 0 4 5 3 0 . 6 3 6 1 1 2 . 5 0 0 1 . 3 8 8 9 0 . 0 3 5 7 0 2 . 0 0 0 0 0 - 0 . 0 4 8 4 0 . 0 3 9 8 0 . 6 4 1 0 1 3 . 0 0 0 1 . 4 0 2 1 0 . 0 4 0 2 9 2 . 0 0 0 0 0 - 0 . 0 4 8 4 0 . 0 3 4 6 0 . 6 4 5 3 1 3 . 5 0 0 1 . 4 0 8 6 0 . 0 4 5 7 3 2 . 0 0 0 0 0 - 0 . 0 4 8 6 0 . 0 3 3 3 0 . 6 5 3 0 1 4 . 0 0 0 1. 4 1 4 7 0 . 0 5 1 3 3 2 . 0 0 0 0 0 - 0 . 0 4 8 8 0 . 0 3 1 5 0 . 6 5 8 4 1 4 . 5 0 0 1 . 4 2 0 5 0 . 0 5 7 1 4 2 . 0 0 0 0 0 - 0 . 0 4 92 0 . 0 2 9 4 0 . 6 6 2 5 1 5 . 0 0 0 1 . 4 2 92 0 . 0 62 8 2 2 . 0 0 0 0 0 - 0 . 0 4 9 8 0 . 0 2 6 9 0 . 6 6 8 9 1 5 . 5 0 0 1 . 4 3 6 4 0 . 0 6 8 7 9 2 . 0 0 0 0 0 - 0 . 0 5 0 5 0 . 0 2 4 5 0 . 6 7 6 3 1 6 . 0 0 0 1 . 4 3 8 2 0 . 0 7 5 6 8 2 . 0 0 0 0 0 - 0 . 0 5 1 5 0 . 0 2 1 9 0 . 6 8 0 7 1 6 . 5 0 0 1 . 4 4 0 8 0 . 0 8 2 7 0 2 . 0 0 0 0 0 - 0 . 0 5 2 7 0 . 02 0 8 0 . 6 8 6 9

FFA TN 1 9 9 0 - 1 5 5 3 POL . W2_2 1 0_30_9 ; 2

XFOI L Vers ion 5 . 0

Calculated polar for : FFA-W2 -2 1 0

1 Reyno lds number fixed

xt rf = 1 . 0 0 0 ( s uct ion) 1 . 0 0 0 (pres sure ) Mach "" 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xt r ------- -------- --------- --------- -------- ------- -------- 6 . 0 0 0 0 0 - 0 . 5 6 6 5 0 0 . 0 0 7 8 9 3 . 0 0 0 0 0 - 0 . 0 2 4 6 0 0 . 5 4 1 3 0 0 . 2 5 4 2 0 - 5 . 5 0 0 0 0 - 0 . 5 0 4 6 0 0 . 0 0 7 0 9 3 . 0 0 0 0 0 - 0 . 0 2 6 5 0 0 . 53 3 5 0 0 . 32 0 2 0 - 5 . 0 0 0 0 0 - 0 . 4 4 1 9 0 0 . 0 0 6 6 9 3 . 0 0 0 0 0 - 0 . 0 2 8 0 0 0 . 52 8 4 0 0 . 3 5 6 5 0 - 4 . 5 0 0 0 0 - 0 . 3 7 9 2 0 0 . 0 0 62 8 3 . 0 0 0 0 0 - 0 . 0 2 9 6 0 0 . 5 1 9 7 0 0 . 4 0 0 0 0 - 4 . 0 0 0 0 0 - 0 . 3 1 6 3 0 0 . 0 0 6 0 9 3 . 0 0 0 0 0 - 0 . 0 3 1 0 0 0 . 5 1 3 2 0 0 . 4 2 7 3 0 -3 . 5 0 0 0 0 - 0 . 2 5 3 2 0 0 . 0 0 6 0 3 3 . 0 0 0 0 0 - 0 . 0 3 2 3 0 0 . 5 0 7 6 0 0 . 4 3 5 8 0 -3 . 0 0 0 0 0 - 0 . 1 9 0 0 0 0 . 0 0 5 9 9 3 . 0 0 0 0 0 - 0 . 0 3 3 6 0 0 . 4 9 8 1 0 0 . 4 4 0 2 0 -2 . 5 0 0 0 0 - 0 . 1 2 6 9 0 0 . 0 0 5 9 7 3 . 0 0 0 0 0 - 0 . 0 3 4 9 0 0 . 4 9 3 5 0 0 . 4 4 9 9 0 -2 . 0 0 0 0 0 - 0 . 0 6 3 8 0 0 . 0 0 5 9 5 3 . 0 0 0 0 0 - 0 . 0 3 6 2 0 0 . 4 8 7 5 0 0 . 4 5 6 0 0 - 1 . 5 0 0 0 0 - 0 . 0 0 0 8 0 0 . 0 0 5 9 5 3 . 0 0 0 0 0 - 0 . 0 3 7 5 0 0 . 4 7 8 4 0 0 . 4 6 1 3 0 - 1 . 0 0 0 0 0 0 . 0 62 3 0 0 . 0 0 5 9 4 3 . 0 0 0 0 0 - 0 . 0 3 8 8 0 0 . 4 7 4 2 0 0 . 4 7 0 6 0

0 . 0 0 0 0 0 0 . 1 8 8 2 0 0 . 0 0 5 9 7 3 . 0 0 0 0 0 - 0 . 0 4 1 4 0 0 . 4 5 9 4 0 0 . 4 8 1 6 0 0 . 5 0 0 0 0 0 . 2 5 1 2 0 0 . 0 0 6 0 0 3 . 0 0 0 0 0 - 0 . 0 42 6 0 0 . 4 5 5 3 0 0 . 4 8 92 0 1 . 0 0 0 0 0 0 . 3 1 4 0 0 0 . 0 0 6 0 4 3 . 0 0 0 0 0 - 0 . 0 4 3 9 0 0 . 4 4 9 3 0 0 . 4 9 4 2 0 1 . 5 0 0 0 0 0 . 3 7 6 7 0 0 . 0 0 6 0 9 3 . 0 0 0 0 0 - 0 . 0 4 52 0 0 . 4 4 0 1 0 0 . 4 9 9 3 0 2 . 0 0 0 0 . 4 3 9 4 0 . 0 0 6 1 3 3 . 0 0 0 0 0 - 0 . 0 4 6 4 0 . 4 3 6 5 0 . 5 0 8 0 2 . 5 0 0 0 . 5 0 2 0 0 . 0 0 62 1 3 . 0 0 0 0 0 - 0 . 0 4 7 7 0 . 42 9 0 0 . 5 1 2 4 3 . 0 0 0 0 . 5 6 4 4 0 . 0 0 6 3 0 3 . 0 0 0 0 0 - 0 . 0 4 8 9 0 . 4 2 0 5 0 . 5 1 6 6 3 . 5 0 0 0 . 62 6 8 0 . 0 0 6 3 8 3 . 0 0 0 0 0 - 0 . 0 5 0 1 0 . 4 1 5 4 0 . 52 5 7 4 . 0 0 0 0 . 6 8 9 0 0 . 0 0 6 4 9 3 . 0 0 0 0 0 - 0 . 0 5 1 2 0 . 4 0 5 1 0 . 5 3 0 5 4 . 5 0 0 0 . 7 5 0 9 0 . 0 0 6 6 3 3 . 0 0 0 0 0 - 0 . 0 5 2 3 0 . 3 9 7 9 0 . 5 3 5 2 5 . 0 0 0 0 . 8 1 2 6 0 . 0 0 6 8 0 3 . 0 0 0 0 0 - 0 . 0 5 3 4 0 . 3 8 3 6 0 . 5 4 3 5 5 . 5 0 0 0 . 8 7 3 6 0 . 0 0 7 0 3 3 . 0 0 0 0 0 - 0 . 0 5 4 5 0 . 3 6 62 0 . 5 4 8 6 6 . 0 0 0 0 . 9 3 4 1 0 . 0 0 7 3 1 3 . 0 0 0 0 0 - 0 . 0 5 5 4 0 . 3 4 9 9 0 . 5 52 6 6 . 5 0 0 0 . 9 9 3 5 0 . 0 0 7 7 3 3 . 0 0 0 0 0 - 0 . 0 5 62 0 . 32 42 0 . 5 6 1 3 7 . 0 0 0 1 . 0 5 2 0 0 . 0 0 8 2 1 3 . 0 0 0 0 0 - 0 . 0 5 7 0 0 . 2 9 9 9 0 . 5 6 6 7 7 . 5 0 0 1 . 1 0 8 4 0 . 0 0 8 9 0 3 . 0 0 0 0 0 - 0 . 0 5 7 5 0 . 2 6 4 1 0 . 5 7 0 7 8 . 0 0 0 1 . 1 5 7 8 0 . 0 1 0 2 6 3 . 0 0 0 0 0 - 0 . 0 5 7 3 0 . 1 93 4 0 . 5 7 8 6 8 . 5 0 0 1 . 2 0 6 1 0 . 0 1 1 5 5 3 . 0 0 0 0 0 - 0 . 0 5 7 0 0 . 1 4 8 6 0 . 5 8 4 4 9 . 0 0 0 1 . 2 5 2 5 0 . 0 1 2 8 3 3 . 0 0 0 0 0 - 0 . 0 5 6 4 0 . 1 1 0 6 0 . 5 8 8 3 9 . 5 0 0 1 . 2 9 4 4 0 . 0 1 42 8 3 . 0 0 0 0 0 - 0 . 0 5 5 3 0 . 0 7 8 7 0 . 5 9 5 4

1 0 . 0 0 0 1 . 3 3 6 4 0 . 0 1 552 3 . 0 0 0 0 0 - 0 . 0 5 4 3 0 . 0 62 8 0 . 6 0 1 9 1 0 . 5 0 0 1 . 3 6 6 8 0 . 0 1 6 8 4 3 . 0 0 0 0 0 - 0 . 0 5 1 7 0 . 0 5 0 4 0 . 6 0 6 0 1 1 . 0 0 0 1 . 3 8 2 8 0 . 0 1 9 7 4 3 . 0 0 0 0 0 - 0 . 0 4 9 9 0 . 0 4 62 0 . 6 1 0 4 1 1 . 5 0 0 1 . 4 0 2 3 0 . 0 2 3 0 3 3 . 0 0 0 0 0 - 0 . 0 4 9 5 0 . 0 4 0 3 0 . 6 1 8 9 1 2 . 0 0 0 1 . 4 2 2 7 0 . 0 2 6 4 8 3 . 0 0 0 0 0 - 0 . 0 4 9 2 0 . 0 3 4 6 0 . 62 3 5 12 . 5 0 0 1 . 4 3 2 0 0 . 0 3 1 1 5 3 . 0 0 0 0 0 - 0 . 0 4 9 0 0 . 0 3 3 0 0 . 62 6 6 1 3 . 0 0 0 1 . 4 4 0 1 0 . 0 3 6 1 4 3 . 0 0 0 0 0 - 0 . 0 4 8 9 0 . 0 3 0 9 0 . 63 4 0 1 3 . 5 0 0 1 . 4 4 8 9 0 . 0 4 1 2 1 3 . 0 0 0 0 0 - 0 . 0 4 8 9 0 . 02 8 5 0 . 6 3 9 7 1 4 . 0 0 0 1 . 4 6 0 2 0 . 0 4 6 1 3 3 . 0 0 0 0 0 - 0 . 0 4 9 0 0 . 0 2 5 9 0 . 6 4 4 1 1 4 . 5 0 0 1 . 4 7 0 5 0 . 0 5 1 2 6 3 . 0 0 0 0 0 - 0 . 0 4 9 1 0 . 0 2 3 6 0 . 6 4 9 9 1 5 . 0 0 0 1 . 4 7 7 0 0 . 0 5 6 9 8 3 . 0 0 0 0 0 - 0 . 0 4 9 4 0 . 0 2 1 3 0 . 6 5 6 7 1 6 . 0 0 0 1 . 4 9 1 3 0 . 0 6 8 7 0 3 . 0 0 0 0 0 - 0 . 0 5 0 8 0 . 0 2 0 3 0 . 6 6 6 5 1 6 . 5 0 0 1 . 4 9 5 5 0 . 0 7 5 2 1 3 . 0 0 0 0 0 - 0 . 0 5 1 8 0 . 0 1 9 6 0 . 6 7 4 3 1 7 . 0 0 0 1. 4 9 8 9 0 . 0 8 2 0 5 3 . 0 0 0 0 0 - 0 . 0 5 3 0 0 . 0 1 8 8 0 . 6 7 92

FFA TN 1 9 9 0 - 1 5 5 4

XFOI L Vers ion 5 . 0

Ca lculated polar fo r : FFA-W2 -2 1 0

1 Reynolds number fixed

xt rf = 0 . 0 1 0 ( suction ) 0 . 1 0 0 (pressure ) Mach =

a lpha -------- 6 . 0 0 0 0 0 - 5 . 5 0 0 0 0 - 5 . 0 0 0 0 0 - 4 . 5 0 0 0 0 - 4 . 0 0 0 0 0 - 3 . 5 0 0 0 0 - 3 . 0 0 0 0 0 -2 . 5 0 0 0 0 -2 . 0 0 0 0 0 - 1 . 5 0 0 0 0 - 1 . 0 0 0 0 0

0 . 0 0 0 0 0 0 . 5 0 0 0 0 1 . 0 0 0 0 0 1 . 5 0 0 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 50 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0 1 5 . 5 0 0 1 6 . 0 0 0 1 6 . 5 0 0 17 . 0 0 0

0 . 1 5 0

CL --------

- 0 . 5 6 3 5 0 - 0 . 5 0 1 6 0 - 0 . 4 3 9 5 0 - 0 . 3 7 7 3 0 - 0 . 32 0 4 0 - 0 . 2 5 8 6 0 - 0 . 1 9 6 8 0 - 0 . 1 3 5 0 0 - 0 . 0 7 3 3 0 - 0 . 0 1 1 6 0

0 . 0 5 0 0 0 0 . 1 7 2 9 0 0 . 2 3 4 1 0 0 . 2 9 52 0 0 . 3 5 6 0 0

0 . 4 1 6 7 0 . 4 7 70 0 . 5 3 7 0 0 . 5 9 6 6 0 . 6 5 5 8 0 . 7 1 4 5 0 . 7 7 2 6 0 . 8 3 0 1 0 . 8 8 6 8 0 . 9 4 2 5 0 . 9 9 7 2 1 . 0 5 0 4 1 . 1 0 2 0 1 . 1 5 1 2 1 . 1 9 6 8 1 . 2 2 2 9 1 . 2 5 1 8 1 . 2 7 7 5 1 . 3 0 0 2 1 . 32 0 5 1 . 3 3 8 2 1 . 3 5 3 9 1 . 3 6 8 5 1 . 3 8 2 1 1 . 3 9 4 1 1 . 4 0 6 0 1 . 4 1 7 6 1 . 4 2 7 6 1 . 4 3 6 7 1 . 4 4 5 6 1 . 4 5 4 9

Re =

CD ---------

0 . 0 0 9 8 1 0 . 0 0 9 5 9 0 . 0 0 9 3 8 0 . 0 0 9 2 0 0 . 0 1 1 0 6 0 . 0 1 1 0 0 0 . 0 1 0 9 5 0 . 0 1 0 92 0 . 0 1 0 9 1 0 . 0 1 0 92 0 . 0 1 0 9 5 0 . 0 1 1 0 6 0 . 0 1 1 1 5 0 . 0 1 1 2 6 0 . 0 1 1 3 9

0 . 0 1 1 5 4 0 . 0 1 1 7 1 0 . 0 1 1 9 1 0 . 0 1 2 1 4 0 . 0 1 2 3 9 0 . 0 1 2 6 7 0 . 0 1 2 9 9 0 . 0 1 3 3 4 0 . 0 1 3 7 2 0 . 0 1 4 1 6 0 . 0 1 4 6 4 0 . 0 1 5 1 9 0 . 0 1 5 8 1 0 . 0 1 652 0 . 0 1 7 3 5 0 . 0 1 8 6 8 0 . 02 0 8 1 0 . 0 2 3 52 0 . 0 2 6 72 0 . 0 3 0 3 1 0 . 0 3 4 2 3 0 . 0 3 8 52 0 . 0 4 2 9 6 0 . 0 4 7 6 9 0 . 0 5 2 6 7 0 . 0 57 8 0 0 . 0 6 3 1 1 0 . 0 6 8 7 3 0 . 0 7 4 6 4 0 . 0 8 0 7 5 0 . 0 8 6 8 1

3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

Re (CL) CM S xt r P xt r --------- ----- - -- - ------ - - -----

3 . 0 0 0 0 0 - 0 . 022 8 0 0 . 5 4 1 1 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 2 4 1 0 0 . 5 3 3 4 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 2 5 4 0 0 . 52 8 3 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 2 6 7 0 0 . 5 1 9 5 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 2 8 3 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 2 9 6 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 3 0 9 0 . 0 . 0 1 0 0 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 3 2 1 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 3 3 4 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 3 4 6 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 3 5 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 3 8 3 0 0 . 0 1 0 0 0 0 . 10 0 0 0 3 . 0 0 0 0 0 - 0 . 0 3 9 5 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 0 7 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 1 8 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 2 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 3 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 4 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 5 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 6 8 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 7 6 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 8 3 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 9 0 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 9 6 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 5 0 0 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 5 0 3 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 5 0 4 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 5 0 4 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 5 0 1 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 9 4 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 6 6 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 5 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 5 7 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 5 6 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 5 6 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 5 6 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 5 8 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 5 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 6 1 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 6 5 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 6 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 7 5 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 8 3 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 4 9 3 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 5 0 4 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 0 - 0 . 0 5 1 5 0 . 0 1 0 0 0 . 1 0 0 0

POL . W2_2 1 0_3 0_TU 1 ; 1

FFA TN 1 9 9 0 - 1 5 5 5

XFOIL Vers ion 5 . 0

Calculated polar for : 5 0 % NACA 6 3- 6 1 8 AND 5 0 % FFA-W3-2

1 Reynolds number fixed

xtrf = 1 . 0 0 0 ( suction ) 1 . 0 0 0 (pres sure ) Mach = 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xt r ------- -------- --------- - - - - - � - - - -------- ------- -------- 6 . 0 0 0 0 0 - 0 . 3 1 6 0 0 0 . 0 0 8 9 8 1 . 0 0 0 0 0 - 0 . 0 8 6 3 0 0 . 6 4 3 8 0 0 . 2 8 5 0 0 - 5 . 5 0 0 0 0 - 0 . 2 5 1 1 0 0 . 0 0 8 1 0 1 . 0 0 0 0 0 - 0 . 0 8 9 0 0 0 . 6 3 3 5 0 0 . 3 6 8 8 0 - 5 . 0 0 0 0 0 - 0 . 1 8 7 8 0 0 . 0 0 7 7 7 1 . 0 0 0 0 0 - 0 . 0 9 0 6 0 0 . 62 0 9 0 0 . 4 1 1 6 0 - 4 . 5 0 0 0 0 - 0 . 1 2 5 2 0 0 . 0 0 7 6 6 1 . 0 0 0 0 0 - 0 . 0 9 1 9 0 0 . 6 0 7 2 0 0 . 4 3 1 1 0 - 4 . 0 0 0 0 0 - 0 . 0 6 2 8 0 0 . 0 0 7 6 1 1 . 0 0 0 0 0 - 0 . 0 9 3 0 0 0 . 5 9 7 4 0 0 . 4 4 6 3 0 - 3 . 5 0 0 0 0 - 0 . 0 0 0 8 0 0 . 0 0 7 6 4 1 . 0 0 0 0 0 - 0 . 0 9 4 1 0 0 . 5 8 4 4 0 0 . 4 6 6 7 0 - 3 . 0 0 0 0 0 0 . 0 6 1 3 0 0 . 0 0 7 6 6 1 . 0 0 0 0 0 - 0 . 0 9 5 1 0 0 . 5 7 5 7 0 0 . 4 7 9 6 0 - 2 . 5 0 0 0 0 0 . 1 2 3 2 0 0 . 0 0 7 7 2 1 . 0 0 0 0 0 - 0 . 0 9 6 1 0 0 . 5 6 2 9 0 0 . 4 8 5 2 0 - 2 . 0 0 0 0 0 0 . 1 8 5 0 0 0 . 0 0 7 7 7 1 . 0 0 0 0 0 - 0 . 0 9 7 1 0 0 . 5 5 4 3 0 0 . 4 9 0 5 0 - 1 . 0 0 0 0 0 0 . 3 0 8 5 0 0 . 0 0 7 8 8 1 . 0 0 0 0 0 - 0 . 0 9 92 0 0 . 5 3 4 3 0 0 . 5 0 3 3 0 - 0 . 5 0 0 0 0 0 . 3 6 9 8 0 0 . 0 0 7 9 8 1 . 0 0 0 0 0 - 0 . 1 0 0 1 0 0 . 52 3 6 0 0 . 5 0 7 6 0

0 . 0 0 0 0 0 0 . 4 3 1 3 0 0 . 0 0 8 0 3 1 . 0 0 0 0 0 - 0 . 1 0 1 1 0 0 . 5 1 5 6 0 0 . 5 1 4 8 0 0 . 5 0 0 0 0 0 . 4 92 3 0 0 . 0 0 8 1 5 1 . 0 0 0 0 0 - 0 . 1 0 2 1 0 0 . 5 0 4 8 0 0 . 52 0 4 0 1 . 0 0 0 0 0 0 . 5 5 3 4 0 0 . 0 0 8 2 5 1 . 0 0 0 0 0 - 0 . 1 0 2 9 0 0 . 4 9 8 6 0 0 . 52 4 5 0 1 . 5 0 0 0 . 6 1 4 0 0 . 0 0 8 3 9 1 . 0 0 0 0 0 - 0 . 1 0 3 8 0 . 4 8 8 2 0 . 52 8 3 2 . 0 0 0 0 . 6 7 4 8 0 . 0 0 8 4 8 1 . 0 0 0 0 0 - 0 . 1 0 4 7 0 . 4 8 1 1 0 . 5 3 5 6 2 . 5 0 0 0 . 7 3 5 1 0 . 0 0 8 6 3 1 . 0 0 0 0 0 - 0 . 1 0 5 5 0 . 4 7 3 0 0 . 5 4 0 5 3 . 0 0 0 0 . 7 9 4 9 0 . 0 0 8 8 2 1 . 0 0 0 0 0 - 0 . 1 0 6 1 0 . 4 6 3 7 0 . 5 4 4 8 3 . 5 0 0 0 . 8 5 4 7 0 . 0{) 8 9 8 1 . 0 0 0 0 0 - 0 . 1 0 6 8 0 . 4 5 7 1 0 . 5 4 8 4 4 . 0 0 0 0 . 9 1 4 1 0 . 0 0 9 1 8 1 . 0 0 0 0 0 - 0 . 1 0 7 5 0 . 4 4 5 0 0 . 5 5 6 0 4 . 5 0 0 0 . 9 7 3 4 0 . 0 0 9 3 6 1 . 0 0 0 0 0 - 0 . 1 0 8 1 0 . 4 3 8 6 0 . 5 6 1 2 5 . 0 0 0 1 . 0 3 1 9 0 . 0 0 9 6 2 1 . 0 0 0 0 0 - 0 . 1 0 8 5 0 . 42 62 0 . 5 6 5 4 5 . 5 0 0 1 . 0 9 0 2 0 . 0 0 9 8 5 1 . 0 0 0 0 0 - 0 . 1 0 9 0 0 . 4 1 8 6 0 . 5 6 9 7 6 . 0 0 0 1 . 1 4 7 9 0 . 0 1 0 1 5 1 . 0 0 0 0 0 - 0 . 1 0 9 3 0 . 4 0 4 3 0 . 5 7 7 5 6 . 5 0 0 1 . 2 0 4 8 0 . 0 1 0 4 9 1 . 0 0 0 0 0 - 0 . 1 0 9 6 0 . 3 8 9 5 0 . 5 8 2 3 7 . 0 0 0 1 . 2 6 0 0 0 . 0 1 0 9 3 1 . 0 0 0 0 0 - 0 . 1 0 9 5 0 . 3 7 0 5 0 . 5 8 7 0 7 . 5 0 0 1 . 3 1 4 4 0 . 0 1 1 4 0 1 . 0 0 0 0 0 - 0 . 1 0 9 4 0 . 3 5 42 0 . 5 9 4 2 8 . 0 0 0 1 . 3 6 5 0 0 . 0 1 2 1 1 1 . 0 0 0 0 0 - 0 . 1 0 8 7 0 . 32 4 4 0 . 6 0 0 5 8 . 5 0 0 1 . 4 1 1 4 0 . 0 1 3 0 5 1 . 0 0 0 0 0 - 0 . 1 0 7 5 0 . 2 9 4 1 0 . 6 0 5 4 9 . 0 0 0 1 . 4 4 9 4 0 . 0 1 4 4 0 1 . 0 0 0 0 0 - 0 . 1 0 5 1 0 . 2 4 9 8 0 . 6 12 2 9 . 5 0 0 1. 4 6 33 0 . 0 1 6 5 1 1 . 0 0 0 0 0 - 0 . 0 9 9 4 0 . 2 0 0 2 0 . 6 1 9 4

1 0 . 0 0 0 1 . 4 7 3 0 0 . 0 1 9 1 2 1 . 0 0 0 0 0 - 0 . 0 9 4 3 0 . 1 62 5 0 . 62 4 6 1 0 . 5 0 0 1 . 4 7 3 5 0 . 0 2 2 8 9 1 . 0 0 0 0 0 - 0 . 0 8 9 9 0 . 12 7 3 0 . 6 3 0 0 1 1 . 0 0 0 1 . 4 7 6 7 0 . 0 2 7 1 6 1 . 0 0 0 0 0 - 0 . 0 8 7 0 0 . 1 0 2 8 0 . 6 3 9 0 1 1 . 5 0 0 1 . 4 8 0 4 0 . 0 3 1 9 8 1 . 0 0 0 0 0 - 0 . 0 8 5 1 0 . 0 8 32 0 . 6 4 4 7 1 2 . 0 0 0 1 . 4 8 2 1 0 . 0 3 7 4 1 1 . 0 0 0 0 0 - 0 . 0 8 3 8 0 . 0 7 0 6 0 . 6 5 0 9 1 2 . 5 0 0 1 . 4 8 7 2 0 . 0 4 2 9 3 1 . 0 0 0 0 0 - 0 . 0 8 3 1 0 . 0 6 0 2 0 . 6 5 9 4 1 3 . 0 0 0 1 . 4 9 3 4 0 . 0 4 8 5 2 1 . 0 0 0 0 0 - 0 . 0 8 2 6 0 . 0 5 1 0 0 . 6 6 57 1 3 . 5 0 0 1 . 4 9 62 0 . 0 5 4 8 7 1 . 0 0 0 0 0 - 0 . 0 8 2 5 0 . 0 4 5 9 0 . 6 7 4 9 1 4 . 0 0 0 1 . 5 0 0 8 0 . 0 6 1 2 0 1 . 0 0 0 0 0 - 0 . 0 8 2 7 0 . 0 4 1 6 0 . 6 8 2 8 1 4 . 5 0 0 1 . 5 0 6 8 0 . 0 6 7 5 3 1 . 0 0 0 0 0 - 0 . 0 8 2 9 0 . 0 3 6 1 0 . 6 9 0 4 1 5 . 0 0 0 1 . 5 1 12 0 . 0 7 4 2 7 1 . 0 0 0 0 0 - 0 . 0 8 3 5 0 . 0 3 4 3 0 . 7 0 0 8

POL . W3_1 95_1 0_9 ; 1

FFA TN 1 9 9 0 - 1 5 5 6 POL . W3_1 9 5_1 0_TU1 ; 1

XFOI L Ve rs ion 5 . 0

Calculated polar for : 5 0 % NACA 63 - 6 1 8 AND 5 0 % FFA-W3-2

1 Reynolds number fixed

xtrf = 0 . 0 1 0 ( suct ion ) 0 . 1 0 0 (pre s sure ) Mach = 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncrit 9 . 0 0 0

a lpha CL CD Re (CL) CM s xt r P xt r ------- -------- ------ - -- --- - - ---- -------- - - --- - - ----- - -

0 . 0 0 0 0 . 3 8 7 9 0 . 0 1 3 4 0 1 . 0 0 0 0 0 - 0 . 0 92 8 0 . 0 1 0 0 0 . 1 0 0 0 0 . 5 0 0 0 . 4 4 7 0 0 . 0 1 3 5 7 1 . 0 0 0 0 0 - 0 . 0 9 3 6 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 . 5 0 5 7 0 . 0 1 3 7 6 1 . 0 0 0 0 0 - 0 . 0 9 4 3 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 5 6 3 8 0 . 0 1 3 9 8 1 . 0 0 0 0 0 - 0 . 0 9 5 0 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 62 1 4 0 . 0 1 4 2 3 1 . 0 0 0 0 0 - 0 . 0 9 5 5 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 6 7 8 4 0 . 0 1 452 1 . 0 0 0 0 0 - 0 . 0 9 6 0 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 7 3 4 7 0 . 0 1 4 8 5 1 . 0 0 0 0 0 - 0 . 0 9 6 3 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 7 9 0 2 0 . 0 1 52 1 1 . 0 0 0 0 0 - 0 . 0 9 6 6 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 8 4 4 8 0 . 0 1 5 6 1 1 . 0 0 0 0 0 - 0 . 0 9 67 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 8 9 8 3 0 . 0 1 6 0 7 1 . 0 0 0 0 0 - 0 . 0 9 6 6 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 9 5 0 4 0 . 0 1 6 5 8 1 . 0 0 0 0 0 - 0 . 0 9 6 4 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 1 . 0 0 1 0 0 . 0 1 7 1 4 1 . 0 0 0 0 0 - 0 . 0 9 5 9 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 1 . 0 4 9 3 0 . 0 1 7 7 8 1 . 0 0 0 0 0 - 0 . 0 9 52 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 0 8 9 5 0 . 0 1 8 5 0 1 . 0 0 0 0 0 - 0 . 0 9 3 0 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 1 2 6 5 0 . 0 1 9 4 2 1 . 0 0 0 0 0 - 0 . 0 9 0 7 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1 6 32 0 . 0 2 0 62 1 . 0 0 0 0 0 - 0 . 0 8 8 9 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 1 9 6 1 0 . 0 2 2 1 4 1 . 0 0 0 0 0 - 0 . 0 8 7 1 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 2 2 6 0 0 . 0 2 4 0 2 1 . 0 0 0 0 0 - 0 . 0 8 5 4 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 2 5 3 4 0 . 0 2 6 3 1 1 . 0 0 0 0 0 - 0 . 0 8 3 9 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 2 7 8 3 0 . 0 2 9 0 0 1 . 0 0 0 0 0 - 0 . 0 8 2 7 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 3 0 1 4 0 . 0 3 2 1 0 1 . 0 0 0 0 0 - 0 . 0 8 1 7 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 3 2 2 1 0 . 0 3 5 6 0 1 . 0 0 0 0 0 - 0 . 0 8 1 0 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 3 4 1 2 0 . 0 3 9 4 9 1 . 0 0 0 0 0 - 0 . 0 8 0 4 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 3 5 8 7 0 . 0 4 3 7 4 1 . 0 0 0 0 0 - 0 . 0 8 0 1 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 3 7 4 7 0 . 0 4 8 2 8 1 . 0 0 0 0 0 - 0 . 0 7 9 9 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 3 8 9 3 0 . 0 5 3 1 9 1 . 0 0 0 0 0 - 0 . 0 7 9 9 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 4 0 2 4 0 . 0 5 8 4 6 1 . 0 0 0 0 0 - 0 . 0 8 0 1 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 4 1 4 0 0 . 0 6 4 0 0 1 . 0 0 0 0 0 - 0 . 0 8 0 4 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 4 2 4 9 0 . 0 6 9 8 1 1 . 0 0 0 0 0 - 0 . 0 8 0 9 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 4 3 5 1 0 . 0 7 5 8 8 1 . 0 0 0 0 0 - 0 . 0 8 1 5 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 4 4 4 4 0 . 0 8 2 1 8 1 . 0 0 0 0 0 - 0 . 0 8 2 3 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 5 7

XFOI L Ve rsion 5 . 0

Calculated polar for : 5 0 % NACA 6 3- 6 1 8 AND 5 0 % FFA-W3-2

1 Reynolds number fixed

xt rf ... 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pre s sure ) Mach =

alpha -- -- - - -- 6 . 0 0 0 0 0 - 5 . 5 0 0 0 0 - 5 . 0 0 0 0 0 - 4 . 5 0 0 0 0 - 4 . 0 0 0 0 0 - 3 . 5 0 0 0 0 - 3 . 0 0 0 0 0 -2 . 5 0 0 0 0 -2 . 0 0 0 0 0 - 1 . 5 0 0 0 0 - 1 . 0 0 0 0 0 - 0 . 5 0 0 0 0

0 . 0 0 0 0 0 0 . 5 0 0 0 0 1 . 0 0 0 0 0 1 . 5 0 0 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0 1 5 . 5 0 0 1 6 . 0 0 0 1 6 . 5 0 0 1 7 . 0 0 0

0 . 1 5 0

CL --------

- 0 . 3 1 4 2 0 - 0 . 2 4 7 1 0 - 0 . 1 8 0 7 0 - 0 . 1 1 6 9 0 - 0 . 0 5 3 8 0

0 . 0 0 8 9 0 0 . 0 7 1 6 0 0 . 1 3 4 0 0 0 . 1 9 6 1 0 0 . 2 5 8 4 0 0 . 3 2 0 5 0 0 . 3 8 2 3 0 0 . 4 4 4 0 0 0 . 5 0 5 8 0 0 . 5 6 7 4 0 0 . 62 8 8 0

0 . 6 8 9 8 0 . 7 5 0 6 0 . 8 1 1 8 0 . 8 7 2 3 0 . 9 3 2 5 0 . 9 9 2 3 1 . 0 5 1 4 1 . 1 1 0 0 1 . 1 6 7 8 1 . 2 2 4 0 1 . 2 7 9 1 1 . 3 3 1 3 1 . 3753 1 . 4 1 6 3 1 . 4 4 8 5 1 . 4 6 9 1 1 . 4 8 5 9 1 . 5 0 0 1 1 . 5 1 0 0 1 . 5 1 7 8 1 . 5 2 9 9 1 . 5 4 5 4 1 . 5 5 2 4 1 . 5 5 9 1 1 . 5 6 6 8 1 . 57 4 7 1 . 5 8 0 8 1 . 5 8 3 8 1 . 5 9 1 1 1 . 5 9 5 3 1 . 5 9 7 4

Re =

CD ---------

0 . 0 0 8 9 9 0 . 0 0 7 7 5 0 . 0 0 6 7 9 0 . 0 0 6 4 9 0 . 0 0 6 3 6 0 . 0 0 6 3 0 0 . 0 0 62 3 0 . 0 0 62 4 0 . 0 0 6 3 0 0 . 0 0 632 0 . 0 0 6 3 7 0 . 0 0 6 4 5 0 . 0 0 6 5 3 0 . 0 0 6 5 9 0 . 0 0 6 6 9 0 . 0 0 6 7 8

0 . 0 0 6 9 1 0 . 0 0 7 0 6 0 . 0 0 7 1 5 0 . 0 0 7 3 1 0 . 0 0 7 4 8 0 . 0 0 7 6 7 0 . 0 0 7 9 1 0 . 0 0 8 1 9 0 . 0 0 8 5 1 0 . 0 0 8 9 4 0 . 0 0 9 4 4 0 . 0 1 0 1 1 0 . 0 1 1 3 5 0 . 0 1 2 6 7 0 . 0 1 4 3 6 0 . 0 1 5 9 4 0 . 0 1 8 0 2 0 . 0 2 0 62 0 . 02 4 0 3 0 . 0 2 8 0 3 0 . 0 3 2 1 2 0 . 0 3 6 1 3 0 . 0 4 1 2 5 0 . 0 4 6 6 7 0 . 0 5 2 2 5 0 . 0 5 7 9 1 0 . 0 6 4 0 3 0 . 0 7 0 8 4 0 . 0 7 7 2 1 0 . 0 8 4 1 1 0 . 0 9 1 3 1

2 . 0 0 0 e 6 Ncr it 9 . 0 0 0

Re (CL) CM S xt r P xt r --------- -------- - - ----- -------

2 . 0 0 0 0 0 - 0 . 0 8 52 0 0 . 6 1 0 2 0 0 . 1 3 3 5 0 2 . 0 0 0 0 0 - 0 . 0 8 9 0 0 0 . 5 9 5 8 0 0 . 2 4 4 6 0 2 . 0 0 0 0 0 - 0 . 0 9 2 0 0 0 . 5 8 5 7 0 0 . 3 4 6 9 0 2 . 0 0 0 0 0 - 0 . 0 9 3 7 0 0 . 5 7 4 6 0 0 . 3 9 0 4 0 2 . 0 0 0 0 0 - 0 . 0 9 5 1 0 0 . 5 6 3 5 0 0 . 4 1 3 8 0 2 . 0 0 0 0 0 - 0 . 0 9 6 3 0 0 . 5 5 3 2 0 0 . 4 2 6 8 0 2 . 0 0 0 0 0 - 0 . 0 9 7 6 0 0 . 5 4 1 0 0 0 . 4 5 4 8 0 2 . 0 0 0 0 0 - 0 . 0 9 8 7 0 0 . 5 3 4 5 0 0 . 4 6 6 3 0 2 . 0 0 0 0 0 - 0 . 0 9 9 7 0 0 . 5 2 0 6 0 0 . 4 7 1 7 0 2 . 0 0 0 0 0 - 0 . 1 0 0 9 0 0 . 5 1 4 0 0 0 . 4 7 9 6 0 2 . 0 0 0 0 0 - 0 . 1 0 1 9 0 0 . 5 0 6 4 0 0 . 4 8 7 7 0 2 . 0 0 0 0 0 - 0 . 1 0 3 0 0 0 . 4 9 3 8 0 0 . 4 92 6 0 2 . 0 0 0 0 0 - 0 . 1 0 3 9 0 0 . 4 8 8 3 0 0 . 4 9 5 8 0 2 . 0 0 0 0 0 - 0 . 1 0 5 0 0 0 . 4 8 0 3 0 0 . 5 0 3 1 0 2 . 0 0 0 0 0 - 0 . 1 0 6 0 0 0 . 4 6 9 3 0 0 . 5 1 0 5 0 2 . 0 0 0 0 0 - 0 . 1 0 6 9 0 0 . 4 6 4 1 0 0 . 5 1 4 7 0 2 . 0 0 0 0 0 - 0 . 1 0 7 8 0 . 4 5 6 8 0 . 5 1 8 1 2 . 0 0 0 0 0 - 0 . 1 0 8 6 0 . 4 4 5 0 0 . 52 0 4 2 . 0 0 0 0 0 - 0 . 1 0 9 5 0 . 4 3 9 8 0 . 52 8 7 2 . 0 0 0 0 0 - 0 . 1 1 0 3 0 . 4 3 0 3 0 . 5353 2 . 0 0 0 0 0 - 0 . 1 1 1 1 0 . 4 1 9 8 0 . 5 3 9 2 2 . 0 0 0 0 0 - 0 . 1 1 1 7 0 . 4 1 3 1 0 . 542 1 2 . 0 0 0 0 0 - 0 . 1 1 2 3 0 . 3 9 6 7 0 . 5 4 4 6 2 . 0 0 0 0 0 - 0 . 1 1 2 8 0 . 3 8 2 1 0 . 5 5 3 0 2 . 0 0 0 0 0 - 0 . 1 1 32 0 . 3 6 6 5 0 . 5 5 9 7 2 . 0 0 0 0 0 - 0 . 1 1 3 3 0 . 3 4 3 9 0 . 5 6 3 8 2 . 0 0 0 0 0 - 0 . 1 1 3 2 0 . 32 1 3 0 . 5 6 6 9 2 . 0 0 0 0 0 - 0 . 1 1 2 8 0 . 2 9 3 5 0 . 5 7 1 7 2 . 0 0 0 0 0 - 0 . 1 1 1 2 0 . 2 4 0 4 0 . 5 7 9 5 2 . 0 0 0 0 0 - 0 . 1 0 9 3 0 . 1 9 5 0 0 . 5 8 5 8 2 . 0 0 0 0 0 - 0 . 1 0 62 0 . 1 4 2 4 0 . 5 8 9 7 2 . 0 0 0 0 0 - 0 . 1 0 1 0 0 . 1 1 3 2 0 . 5 92 6 2 . 0 0 0 0 0 - 0 . 0 9 6 4 0 . 0 9 1 0 0 . 6 0 1 2 2 . 0 0 0 0 0 - 0 . 0 92 6 0 . 0 7 2 1 0 . 6 0 7 9 2 . 0 0 0 0 0 - 0 . 0 8 9 5 0 . 0 6 1 0 0 . 6 1 2 5 2 . 0 0 0 0 0 - 0 . 0 8 7 0 0 . 0 5 0 4 0 . 6 1 6 5 2 . 0 0 0 0 0 - 0 . 0 8 5 4 0 . 0 4 4 0 0 . 62 5 5 2 . 0 0 0 0 0 - 0 . 0 8 4 3 0 . 0 3 7 6 0 . 6 3 2 8 2 . 0 0 0 0 0 - 0 . 0 8 3 3 0 . 0 3 5 5 0 . 6 3 7 7 2 . 0 0 0 0 0 - 0 . 0 8 2 6 0 . 0 3 3 4 0 . 6 4 2 3 2 . 0 0 0 0 0 - 0 . 0 8 2 3 0 . 0 3 0 9 0 . 6 5 4 1 2 . 0 0 0 0 0 - 0 . 0 8 2 1 0 . 02 8 1 0 . 6 6 0 3 2 . 0 0 0 0 0 - 0 . 0 8 2 1 0 . 0 2 52 0 . 6 6 4 9 2 . 0 0 0 0 0 - 0 . 0 8 2 5 0 . 02 3 1 0 . 67 6 4 2 . 0 0 0 0 0 - 0 . 0 8 3 0 0 . 0 2 2 8 0 . 6 8 4 2 2 . 0 0 0 0 0 - 0 . 0 8 3 8 0 . 02 2 3 0 . 6 9 0 5 2 . 0 0 0 0 0 - 0 . 0 8 4 6 0 . 0 2 1 4 0 . 7 0 3 3

POL . W3_1 95_20_9 ; 2

FFA TN 1 9 9 0 - 1 5 5 8

XFOIL Vers ion 5 . 0

Calculated polar for : 5 0 % NACA 6 3- 6 1 8 AND 5 0 % FFA-W3-2

1 Reynolds number fixed

xt rf = 1 . 0 0 0 ( suct ion) 1 . 0 0 0 (pre s sure ) Mach =

a lpha -------- 6 . 0 0 0 0 0 - 5 . 5 0 0 0 0 - 5 . 0 0 0 0 0 - 4 . 50 0 0 0 - 4 . 0 0 0 0 0 - 3 . 5 0 0 0 0 - 3 . 0 0 0 0 0 -2 . 5 0 0 0 0 -2 . 0 0 0 0 0 - 1 . 5 0 0 0 0 - 1 . 0 0 0 0 0 - 0 . 5 0 0 0 0

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 12 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0

0 . 1 5 0 Re =

CL CD -------- -------- -

- 0 . 3 1 1 9 0 0 . 0 0 8 6 8 - 0 . 2 4 5 9 0 0 . 0 0 7 7 0 - 0 . 1 8 0 1 0 0 . 0 0 6 8 8 - 0 . 1 1 5 2 0 0 . 0 0 6 3 1 - 0 . 0 5 1 1 0 0 . 0 0 5 9 6

0 . 0 1 1 9 0 0 . 0 0 5 8 5 0 . 0 7 4 8 0 0 . 0 0 5 7 7 0 . 1 3 7 3 0 0 . 0 0 5 7 4 0 . 1 9 9 7 0 0 . 0 0 5 7 4 0 . 2 6 1 9 0 0 . 0 0 5 7 9 0 . 32 4 0 0 0 . 0 0 5 8 3 0 . 3 8 6 2 0 0 . 0 0 5 8 8

0 . 4 4 8 0 0 . 0 0 5 9 5 0 . 5 0 9 7 0 . 0 0 6 0 3 0 . 5 7 1 4 0 . 0 0 6 1 1 0 . 6 3 2 9 0 . 0 0 6 2 0 0 . 6 9 4 2 0 . 0 0 6 3 1 0 . 7 5 52 0 . 0 0 6 4 3 0 . 8 1 6 3 0 . 0 0 6 5 4 0 . 8 7 6 9 0 . 0 0 6 6 9 0 . 9 3 7 2 0 . 0 0 6 8 6 0 . 9 9 7 1 0 . 0 0 7 0 5 1 . 0 5 6 6 0 . 0 0 7 2 7 1 . 1 1 4 8 0 . 0 0 7 5 9 1 . 1 7 2 3 0 . 0 0 7 9 6 1 . 2 2 7 6 0 . 0 0 8 4 8 1 . 2 7 9 9 0 . 0 0 92 3 1 . 3 2 9 8 0 . 0 1 0 1 1 1 . 3 7 6 7 0 . 0 1 1 1 4 1 . 4 1 62 0 . 0 1 2 6 0 1 . 4 5 32 0 . 0 1 4 0 3 1 . 4 8 3 3 0 . 0 1 52 4 1 . 5 0 6 7 0 . 0 1 6 8 4 1 . 5 2 3 3 0 . 0 1 9 1 1 1 . 5 3 9 0 0 . 0 2 1 8 6 1 . 5 5 8 9 0 . 0 2 4 6 9 1 . 5 7 4 5 0 . 0 2 8 1 8 1 . 5 8 6 4 0 . 0 3 2 32 1 . 5 9 9 1 0 . 0 3 6 7 0 1 . 6 1 32 0 . 0 4 1 1 5 1 . 6 2 2 4 0 . 0 4 6 3 5 1 . 6 3 1 1 0 . 0 5 1 7 9 1 . 6 3 4 3 0 . 0 5 8 0 9

3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

Re ( CL) CM S xt r P xt r -------- - -------- ------- -------

3 . 0 0 0 0 0 - 0 . 0 8 5 7 0 0 . 5 8 4 5 0 0 . 0 9 4 0 0 3 . 0 0 0 0 0 - 0 . 0 8 8 8 0 0 . 5 7 6 4 0 0 . 1 7 5 7 0 3 . 0 0 0 0 0 - 0 . 0 9 1 6 0 0 . 5 6 3 7 0 0 . 2 6 3 5 0 3 . 0 0 0 0 0 - 0 . 0 9 3 9 0 0 . 5 5 5 5 0 0 . 3 2 9 6 0 3 . 0 0 0 0 0 - 0 . 0 9 5 7 0 0 . 5 4 2 8 0 0 . 3 8 4 9 0 3 . 0 0 0 0 0 - 0 . 0 9 7 0 0 0 . 5 3 4 3 0 0 . 4 0 6 3 0 3 . 0 0 0 0 0 - 0 . 0 9 8 3 0 0 . 52 3 6 0 0 . 42 8 1 0 3 . 0 0 0 0 0 - 0 . 0 9 9 5 0 0 . 5 1 4 8 0 0 . 4 4 7 5 0 3 . 0 0 0 0 0 - 0 . 1 0 0 6 0 0 . 5 0 4 1 0 0 . 4 6 1 4 0 3 . 0 0 0 0 0 - 0 . 1 0 1 7 0 0 . 4 9 6 7 0 0 . 4 6 7 1 0 3 . 0 0 0 0 0 - 0 . 1 0 2 8 0 0 . 4 8 5 1 0 0 . 4 7 3 2 0 3 . 0 0 0 0 0 - 0 . 1 0 3 8 0 0 . 4 8 0 4 0 0 . 4 8 0 9 0 3 . 0 0 0 0 0 - 0 . 1 0 4 8 0 . 4 6 9 6 0 . 4 8 6 0 3 . 0 0 0 0 0 - 0 . 1 0 5 8 0 . 4 6 2 9 0 . 4 8 9 3 3 . 0 0 0 0 0 - 0 . 1 0 6 8 0 . 4 5 5 5 0 . 4 9 8 2 3 . 0 0 0 0 0 - 0 . 1 0 7 8 0 . 4 4 5 1 0 . 5 0 3 8 3 . 0 0 0 0 0 - 0 . 1 0 8 7 0 . 4 4 0 2 0 . 5 0 7 0 3 . 0 0 0 0 0 - 0 . 1 0 9 6 0 . 4 3 0 3 0 . 5 1 1 3 3 . 0 0 0 0 0 - 0 . 1 1 0 4 0 . 4 2 2 7 0 . 5 1 8 3 3 . 0 0 0 0 0 - 0 . 1 1 1 2 0 . 4 1 4 8 0 . 52 3 0 3 . 0 0 0 0 0 - 0 . 1 1 2 0 0 . 4 0 32 0 . 52 6 7 3 . 0 0 0 0 0 - 0 . 1 1 2 6 0 . 3 9 4 0 0 . 52 92 3 . 0 0 0 0 0 - 0 . 1 1 3 3 0 . 3 8 0 6 0 . 5 3 6 5 3 . 0 0 0 0 0 - 0 . 1 1 3 7 0 . 3 6 1 0 0 . 5 4 1 9 3 . 0 0 0 0 0 - 0 . 1 1 4 0 0 . 3 4 1 1 0 . 5 4 6 0 3 . 0 0 0 0 0 - 0 . 1 1 4 0 0 . 3 1 2 9 0 . 5 4 8 5 3 . 0 0 0 0 0 - 0 . 1 1 3 6 0 . 2 7 4 8 0 . 5 5 5 4 3 . 0 0 0 0 0 - 0 . 11 2 9 0 . 2 3 4 8 0 . 5 6 1 4 3 . 0 0 0 0 0 - 0 . 1 1 1 7 0 . 1 9 0 6 0 . 5 6 5 8 3 . 0 0 0 0 0 - 0 . 1 0 9 5 0 . 1 4 5 0 0 . 5 6 8 5 3 . 0 0 0 0 0 - 0 . 1 0 7 0 0 . 1 0 7 0 0 . 5 7 6 1 3 . 0 0 0 0 0 - 0 . 1 0 3 1 0 . 0 8 2 4 0 . 5 8 2 1 .3 . 0 0 0 0 0 - 0 . 0 9 8 9 0 . 0 6 5 1 0 . 5 8 6 1 3 . 0 0 0 0 0 - 0 . 0 9 4 8 0 . 0 5 1 1 0 . 5 9 1 1 3 . 0 0 0 0 0 - 0 . 0 9 1 7 0 . 0 4 4 8 0 . 5 9 92 3 . 0 0 0 0 0 - 0 . 0 8 9 6 0 . 0 3 7 9 0 . 6 0 4 4 3 . 0 0 0 0 0 - 0 . 0 8 7 7 0 . 0 3 4 4 0 . 6 0 8 0 3 . 0 0 0 0 0 - 0 . 0 8 6 2 0 . 0 3 2 4 0 . 6 1 7 5 3 . 0 0 0 0 0 - 0 . 0 8 5 1 0 . 0 2 9 6 0 . 62 3 7 3 . 0 0 0 0 0 - 0 . 0 8 4 3 0 . 0 2 67 0 . 62 7 8 3 . 0 0 0 0 0 - 0 . 0 8 3 8 0 . 02 4 5 0 . 6 3 6 6 3 . 0 0 0 0 0 - 0 . 0 8 3 5 0 . 02 3 9 0 . 6 4 4 5 3 . 0 0 0 0 0 - 0 . 0 8 3 4 0 . 02 2 5 0 . 6 4 8 8

POL . W3_1 9 5_3 0_9 ; 1

FFA TN 1 9 9 0- 1 5 5 9 POL . W3_1 95_3 0_TU1 ; 2

XFOIL Vers ion 5 . 0

Calculated polar for : 5 0 % NACA 6 3- 6 1 8 AND 5 0 % FFA-W3- 2

1 Reynolds number fixed

xt rf = 0 . 0 1 0 ( suct ion) 0 . 1 0 0 (pres sure ) Mach = 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re ( CL) CM S xt r P xt r --- ---- -------- - - -- - ---- --- - ----- -- - ----- ------- -------- 4 . 5 0 0 0 0 - 0 . 1 4 0 4 0 0 . 0 1 0 5 8 3 . 0 0 0 0 0 - 0 . 0 8 7 6 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 4 . 0 0 0 0 0 - 0 . 0 7 8 7 0 0 . 0 1 0 5 5 3 . 0 0 0 0 0 - 0 . 0 8 8 8 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 5 0 0 0 0 - 0 . 0 1 7 1 0 0 . 0 1 0 5 4 3 . 0 0 0 0 0 - 0 . 0 8 9 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 0 0 0 0 0 0 . 0 4 4 4 0 0 . 0 1 0 5 5 3 . 0 0 0 0 0 - 0 . 0 9 1 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 2 . 5 0 0 0 0 0 . 1 0 5 7 0 0 . 0 1 0 5 8 3 . 0 0 0 0 0 - 0 . 0 92 1 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 2 . 0 0 0 0 0 0 . 1 6 6 9 0 0 . 0 1 0 6 3 3 . 0 0 0 0 0 - 0 . 0 9 3 2 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 5 0 0 0 0 0 . 2 2 7 8 0 0 . 0 1 0 7 0 3 . 0 0 0 0 0 - 0 . 0 9 4 2 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 0 0 0 0 0 0 . 2 8 8 5 0 0 . 0 1 0 7 8 3 . 0 0 0 0 0 - 0 . 0 9 5 2 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 0 . 5 0 0 0 0 0 . 3 4 9 0 0 0 . 0 1 0 8 8 3 . 0 0 0 0 0 - 0 . 0 9 6 1 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0

0 . 0 0 0 0 . 4 0 9 3 0 . 0 1 1 0 0 3 . 0 0 0 0 0 - 0 . 0 9 7 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 5 0 0 0 . 4 6 9 3 0 . 0 1 1 1 4 3 . 0 0 0 0 0 - 0 . 0 97 9 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 . 52 8 9 0 . 0 1 1 3 1 3 . 0 0 0 0 0 - 0 . 0 9 8 7 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 5 8 8 2 0 . 0 1 1 4 9 3 . 0 0 0 0 0 - 0 . 0 9 9 4 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 6 4 7 1 0 . 0 1 1 7 0 3 . 0 0 0 0 0 - 0 . 1 0 0 1 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 7 0 5 5 0 . 0 1 1 9 3 3 . 0 0 0 0 0 - 0 . 1 0 0 7 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 7 6 3 5 0 . 0 1 2 1 8 3 . 0 0 0 0 0 - 0 . 1 0 1 3 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 8 2 0 9 0 . 0 1 2 4 6 3 . 0 0 0 0 0 - 0 . 1 0 1 7 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 8 7 7 7 0 . 0 1 2 7 7 3 . 0 0 0 0 0 - 0 . 1 0 2 1 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 9 3 3 8 0 . 0 1 3 1 1 3 . 0 0 0 0 0 - 0 . 1 0 2 3 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 9 8 9 0 0 . 0 1 3 4 9 3 . 0 0 0 0 0 - 0 . 1 0 2 4 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 1 . 0 4 3 3 0 . 0 1 3 9 0 3 . 0 0 0 0 0 - 0 . 1 0 2 4 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 1 . 0 9 6 5 0 . 0 1 4 3 6 3 . 0 0 0 0 0 - 0 . 1 0 2 2 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 1 4 8 3 0 . 0 1 4 8 6 3 . 0 0 0 0 0 - 0 . 1 0 1 8 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 1 9 8 4 0 . 0 1 5 42 3 . 0 0 0 0 0 - 0 . 1 0 1 1 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 2 4 6 0 0 . 0 1 6 0 4 3 . 0 0 0 0 0 - 0 . 1 0 0 1 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 2 8 0 9 0 . 0 1 6 7 4 3 . 0 0 0 0 0 - 0 . 0 9 6 8 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 3 1 7 8 0 . 0 1 7 7 0 3 . 0 0 0 0 0 - 0 . 0 9 4 5 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 3 5 0 9 0 . 0 1 8 9 4 3 . 0 0 0 0 0 - 0 . 0 92 0 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 3.8 0 1 0 . 0 2 0 5 5 3 . 0 0 0 0 0 - 0 . 0 8 9 6 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 4 0 63 0 . 0 2 2 5 6 3 . 0 0 0 0 0 - 0 . 0 8 7 4 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 4 3 0 0 0 . 02 5 0 3 3 . 0 0 0 0 0 - 0 . 0 8 5 6 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 4 5 2 7 0 . 02 7 8 4 3 . 0 0 0 0 0 - 0 . 0 8 4 0 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 4 7 1 5 0 . 0 3 1 2 0 3 . 0 0 0 0 0 - 0 . 0 8 2 7 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 4 9 0 0 0 . 0 3 4 8 3 3 . 0 0 0 0 0 - 0 . 0 8 1 7 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 5 0 6 4 0 . 0 3 8 9 1 3 . 0 0 0 0 0 - 0 . 0 8 0 9 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 52 0 0 0 . 0 4 3 4 6 3 . 0 0 0 0 0 - 0 . 0 8 0 3 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 5 32 8 0 . 0 4 8 2 9 3 . 0 0 0 0 0 - 0 . 0 7 9 9 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 5 4 4 9 0 . 0 5 3 4 1 3 . 0 0 0 0 0 - 0 . 0 7 97 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 5 5 6 0 0 . 0 5 8 8 2 3 . 0 0 0 0 0 - 0 . 0 7 9 7 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 5 6 5 7 0 . 0 6 4 4 8 3 . 0 0 0 0 0 - 0 . 0 7 9 9 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 5 0 0 1 . 57 4 9 0 . 0 7 0 2 8 3 . 0 0 0 0 0 - 0 . 0 8 0 1 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 0 0 0 1 . 5 8 3 3 0 . 0 7 6 4 4 3 . 0 0 0 0 0 - 0 . 0 8 0 6 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 5 0 0 1 . 5 8 9 8 0 . 0 8 3 1 1 3 . 0 0 0 0 0 - 0 . 0 8 1 4 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 6 0

XFOI L Ve rsion 5 . 0

Ca lculated polar for : FFA-W3-2 l l

1 Reynolds numbe r fixed

xt rf = 1 . 0 0 0 ( suct ion) 1 . 0 0 0 (pre s su re ) Mach =

a lpha -- ------ 6 . 0 0 0 0 0 - 5 . 5 0 0 0 0 - 5 . 0 0 0 0 0 - 4 . 5 0 0 0 0 - 4 . 0 0 0 0 0 - 3 . 5 0 0 0 0 - 3 . 0 0 0 0 0 -2 . 5 0 0 0 0 - 2 . 0 0 0 0 0 - 1 . 5 0 0 0 0 - 1 . 0 0 0 0 0 - 0 . 5 0 0 0 0

0 . 0 0 0 0 0 0 . 5 0 0 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0

0 . 1 5 0

CL --------

- 0 . 3 9 1 6 0 - 0 . 3 2 7 4 0 - 0 . 2 6 4 4 0 - 0 . 2 0 0 4 0 - 0 . 1 3 6 9 0 - 0 . 0 7 3 8 0 - 0 . 0 1 0 5 0

0 . 0 5 3 0 0 0 . 1 1 5 9 0 0 . 1 7 8 8 0 0 . 2 4 1 4 0 0 . 3 0 4 4 0 0 . 3 6 7 0 0 0 . 4 2 9 3 0

0 . 4 9 1 5 0 . 5 5 3 4 0 . 6 1 5 5 0 . 6 7 7 4 0 . 7 3 9 0 0 . 8 0 0 0 0 . 8 6 0 9 0 . 92 1 8 0 . 9 8 2 5 1 . 0 4 2 5 1 . 1 0 2 5 1 . 1 6 1 4 1 . 2 2 0 7 1 . 2 7 9 0 1 . 3 3 6 4 1 . 3 9 2 5 1 . 4 4 5 6 1 . 4 9 5 1 1 . 5 3 7 1 1 . 5 6 2 0 1 . 5 6 5 3 1 . 5 6 3 0 1 . 5 5 6 5 1 . 5 5 1 2 1 . 5 4 1 9 1 . 5 3 8 1 1 . 5 2 7 5 1 . 5 2 5 2 1 . 52 0 1

Re = 1 . 0 0 0 e 6 Ncr it

CD Re ( CL) CM --------- --------- --------

0 . 0 0 8 5 1 1 . 0 0 0 0 0 - 0 . 0 7 0 8 0 0 . 0 0 8 3 7 1 . 0 0 0 0 0 - 0 . 0 7 2 4 0 0 . 0 0 8 4 5 1 . 0 0 0 0 0 - 0 . 0 7 3 4 0 0 . 0 0 8 3 6 1 . 0 0 0 0 0 - 0 . 0 7 4 9 0 0 . 0 0 8 3 8 1 . 0 0 0 0 0 - 0 . 0 7 62 0 0 . 0 0 8 4 2 1 . 0 0 0 0 0 - 0 . 0 7 7 3 0 0 . 0 0 8 4 5 1 . 0 0 0 0 0 - 0 . 0 7 8 6 0 0 . 0 0 8 4 2 1 . 0 0 0 0 0 - 0 . 0 7 9 9 0 0 . 0 0 8 4 9 1 . 0 0 0 0 0 - 0 . 0 8 1 1 0 0 . 0 0 8 5 6 1 . 0 0 0 0 0 - 0 . 0 8 2 2 0 0 . 0 0 8 6 5 1 . 0 0 0 0 0 - 0 . 0 8 3 3 0 0 . 0 0 8 6 7 1 . 0 0 0 0 0 - 0 . 0 8 4 6 0 0 . 0 0 8 7 5 1 . 0 0 0 0 0 - 0 . 0 8 5 7 0 0 . 0 0 8 8 6 1 . 0 0 0 0 0 - 0 . 0 8 6 8 0

0 . 0 0 8 9 8 1 . 0 0 0 0 0 - 0 . 0 8 7 9 0 . 0 0 9 1 1 1 . 0 0 0 0 0 - 0 . 0 8 8 9 0 . 0 0 92 1 1 . 0 0 0 0 0 - 0 . 0 9 0 0 0 . 0 0 9 3 3 1 . 0 0 0 0 0 - 0 . 0 9 1 0 0 . 0 0 9 4 7 1 . 0 0 0 0 0 - 0 . 0 9 1 9 0 . 0 0 9 6 7 1 . 0 0 0 0 0 - 0 . 0 92 8 0 . 0 0 9 8 7 1 . 0 0 0 0 0 - 0 . 0 9 3 6 0 . 0 1 0 0 3 1 . 0 0 0 0 0 - 0 . 0 9 4 4 0 . 0 1 0 2 1 1 . 0 0 0 0 0 - 0 . 0 9 53 0 . 0 1 0 4 5 1 . 0 0 0 0 0 - 0 . 0 9 6 0 0 . 0 1 0 6 7 1 . 0 0 0 0 0 - 0 . 0 9 6 6 0 . 0 1 0 9 9 1 . 0 0 0 0 0 - 0 . 0 9 7 2 0 . 0 1 1 2 3 1 . 0 0 0 0 0 - 0 . 0 9 7 7 0 . 0 1 1 5 5 1 . 0 0 0 0 0 - 0 . 0 9 8 2 0 . 0 1 1 9 5 1 . 0 0 0 0 0 - 0 . 0 9 8 5 0 . 0 1 2 4 2 1 . 0 0 0 0 0 - 0 . 0 9 8 6 0 . 0 1 3 1 2 1 . 0 0 0 0 0 - 0 . 0 9 8 3 0 . 0 1 4 0 4 1 . 0 0 0 0 0 - 0 . 0 9 7 6 0 . 0 1 5 4 4 1 . 0 0 0 0 0 - 0 . 0 9 62 0 . 0 1 7 8 2 1 . 0 0 0 0 0 - 0 . 0 9 3 0 0 . 0 2 0 6 3 1 . 0 0 0 0 0 - 0 . 0 8 7 3 0 . 0 2 5 0 1 1 . 0 0 0 0 0 - 0 . 0 8 4 2 0 . 0 3 0 8 4 1 . 0 0 0 0 0 - 0 . 0 8 2 9 0 . 0 3 7 3 8 1 . 0 0 0 0 0 - 0 . 0 8 2 7 0 . 0 4 4 8 8 1 . 0 0 0 0 0 - 0 . 0 8 3 0 0 . 0 5 2 1 5 1 . 0 0 0 0 0 - 0 . 0 8 3 7 0 . 0 6 0 5 4 1 . 0 0 0 0 0 - 0 . 0 8 4 7 0 . 0 6 8 1 9 1 . 0 0 0 0 0 - 0 . 0 8 5 7 0 . 0 7 6 3 1 1 . 0 0 0 0 0 - 0 . 0 8 7 0

POL . W3_2 1 1_1 0_9 ; 1

9 . 0 0 0

S xt r P xt r ------- -------0 . 5 7 3 8 0 0 . 4 0 9 0 0 0 . 5 5 9 2 0 0 . 4 3 0 5 0 0 . 5 4 9 2 0 0 . 4 4 7 3 0 0 . 5 3 6 9 0 0 . 4 5 4 9 0 0 . 5 2 4 5 0 0 . 4 6 0 2 0 0 . 5 1 5 3 0 0 . 4 6 4 3 0 0 . 5 0 4 2 0 0 . 4 6 7 8 0 0 . 4 9 6 4 0 0 . 4 7 5 0 0 0 . 4 8 5 6 0 0 . 4 7 9 0 0 0 . 4 7 8 3 0 0 . 4 8 2 2 0 0 . 4 7 0 8 0 0 . 4 8 5 1 0 0 . 4 6 1 9 0 0 . 4 9 0 7 0 0 . 4 5 5 6 0 0 . 4 9 5 2 0 0 . 4 4 7 2 0 0 . 4 9 8 3 0 0 . 4 4 1 1 0 . 5 0 1 2 0 . 4352 0 . 5 0 3 9 0 . 42 6 9 0 . 5 0 8 6 0 . 42 1 8 0 . 5 1 3 0 0 . 4 1 6 5 0 . 5 1 6 2 0 . 4 0 8 1 0 . 5 1 9 2 0 . 4 0 2 9 0 . 5 2 1 8 0 . 3 9 7 9 0 . 52 4 4 0 . 3 9 0 0 0 . 5 3 0 2 0 . 3 8 3 5 0 . 5 3 4 0 0 . 3 7 7 9 0 . 5 3 6 9 0 . 3 6 6 8 0 . 5 3 9 7 0 . 3 5 7 9 0 . 5 4 2 2 0 . 3 4 5 5 0 . 5 4 8 1 0 . 3 3 2 0 0 . 5 52 1 0 . 3 2 0 2 0 . 5 5 5 3 0 . 2 97 4 0 . 5 5 8 3 0 . 2 6 9 6 0 . 5 6 1 0 0 . 2 3 2 2 0 . 5 6 7 2 0 . 1 8 4 6 0 . 5 7 1 2 0 . 1 5 1 7 0 . 5 7 4 2 0 . 1 2 3 2 0 . 5 7 7 0 0 . 1 0 2 2 0 . 5 7 9 5 0 . 0 8 7 3 0 . 5 8 4 0 0 . 0 7 8 1 0 . 5 8 8 9 0 . 0 6 6 7 0 . 5 9 2 0 0 . 0 5 9 5 0 . 5 9 4 7 0 . 0 5 1 3 0 . 5 9 7 3 0 . 0 4 8 8 0 . 6 0 0 1

FFA TN 1 9 9 0 - 1 5 6 1 POL . W3_2 1 1_1 0_TU1 ; 1

XFOI L Vers ion 5 . 0

Calculated polar for : FFA-W3 - 2 1 1

1 Reynolds number fixed

xtrf = 0 . 0 1 0 ( suct ion) 0 . 1 0 0 (pre ssure ) Mach = 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it 9 . 0 0 0

alpha CL CD Re (CL) CM S xt r P xt r - -- - - -- -------- --------- -------- - -------- ------- -------

0 . 0 0 0 0 . 3 32 9 0 . 0 1 3 9 5 1 . 0 0 0 0 0 - 0 . 0 7 8 7 0 . 0 1 0 0 0 . 1 0 0 0 0 . 5 0 0 0 . 3 9 4 5 0 . 0 1 4 0 6 1 . 0 0 0 0 0 - 0 . 0 8 0 0 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 . 4 5 5 7 0 . 0 1 4 2 0 1 . 0 0 0 0 0 - 0 . 0 8 12 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 5 1 6 5 0 . 0 1 4 3 8 1 . 0 0 0 0 0 - 0 . 0 82 4 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 5 7 6 8 0 . 0 1 4 6 0 1 . 0 0 0 0 0 - 0 . 0 8 3 4 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 6 3 6 6 0 . 0 1 4 8 5 1 . 0 0 0 0 0 - 0 . 0 8 4 4 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 9 5 8 0 . 0 1 5 1 3 1 . 0 0 0 0 0 - 0 . 0 8 5 3 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 7 5 4 3 0 . 0 1 5 4 6 1 . 0 0 0 0 0 - 0 . 0 8 6 0 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 8 1 2 1 0 . 0 1 5 82 1 . 0 0 0 0 0 - 0 . 0 8 6 7 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 8 6 9 1 0 . 0 1 62 4 1 . 0 0 0 0 0 - 0 . 0 8 7 3 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 92 5 1 0 . 0 1 6 7 0 1 . 0 0 0 0 0 - 0 . 0 8 7 7 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 9 8 0 0 0 . 0 1 7 2 2 1 . 0 0 0 0 0 - 0 . 0 8 8 0 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 1 . 0 3 3 6 0 . 0 1 7 8 1 1 . 0 0 0 0 0 - 0 . 0 8 8 1 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 0 8 5 5 0 . 0 1 8 4 7 1 . 0 0 0 0 0 - 0 . 0 8 8 0 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 1 3 5 5 0 . 0 1 92 2 1 . 0 0 0 0 0 - 0 . 0 8 7 7 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1 8 2 7 0 . 0 2 0 0 8 1 . 0 0 0 0 0 - 0 . 0 8 7 0 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 2 2 4 1 0 . 0 2 1 0 9 1 . 0 0 0 0 0 - 0 . 0 8 5 7 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 2 5 1 0 0 . 0 2 2 52 1 . 0 0 0 0 0 - 0 . 0 8 2 7 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 2 7 9 2 0 . 0 2 4 6 1 1 . 0 0 0 0 0 - 0 . 0 8 1 3 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 3 0 3 3 0 . 0 2 7 3 9 1 . 0 0 0 0 0 - 0 . 0 8 0 6 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 32 4 2 0 . 0 3 0 8 4 1 . 0 0 0 0 0 - 0 . 0 8 0 3 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 3 4 1 9 0 . 0 3 4 9 0 1 . 0 0 0 0 0 - 0 . 0 8 0 3 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 3 5 7 2 0 . 0 3 9 52 1 . 0 0 0 0 0 - 0 . 0 8 0 6 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 3 6 9 9 0 . 0 4 4 62 1 . 0 0 0 0 0 - 0 . 0 8 1 1 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 3 8 1 0 0 . 0 5 0 1 7 1 . 0 0 0 0 0 - 0 . 0 8 1 8 0 . 0 1 0 0 0 . 1 0 0 0 12 . 5 0 0 1 . 3 9 0 1 0 . 0 5 6 0 4 1 . 0 0 0 0 0 - 0 . 0 8 2 5 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 3 9 8 0 0 . 0 62 2 8 1 . 0 0 0 0 0 - 0 . 0 8 3 4 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 4 0 4 8 0 . 0 6 8 7 7 1 . 0 0 0 0 0 - 0 . 0 8 4 5 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 4 1 0 4 0 . 0 7 552 1 . 0 0 0 0 0 - 0 . 0 8 5 6 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 4.1 5 7 0 . 0 8 2 5 2 1 . 0 0 0 0 0 - 0 . 0 8 6 9 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 4

'2 0 6 0 . 0 8 9 7 5 1 . 0 0 0 0 0 - 0 . 0 8 8 4 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 6 2

XFO I L Version 5 . 0

Calculated pola r for : FFA-W3-2 1 1

1 Reynolds numbe r fixed

xtrf -= 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pre s sure ) Mach ""'

a lpha -------- 6 . 0 0 0 0 0 - 5 . 50 0 0 0 -5 . 0 0 0 0 0 - 4 . 5 0 0 0 0 - 4 . 0 0 0 0 0 - 3 . 5 0 0 0 0 - 3 . 0 0 0 0 0 - 2 . 5 0 0 0 0 - 2 . 0 0 0 0 0 - 1 . 5 0 0 0 0 - 1 . 0 0 0 0 0 - 0 . 5 0 0 0 0

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 50 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0 1 5 . 5 0 0 1 6 . 0 0 0 1 6 . 5 0 0

0 . 1 5 0

CL --------

- 0 . 3 8 4 8 0 - 0 . 32 0 0 0 - 0 . 2 5 5 5 0 - 0 . 1 9 1 8 0 - 0 . 1 2 8 3 0 - 0 . 0 6 4 9 0 - 0 . 0 0 1 3 0

0 . 0 62 0 0 0 . 1 2 5 2 0 0 . 1 8 8 1 0 0 . 2 5 1 3 0 0 . 3 1 4 4 0

0 . 3 7 7 2 0 . 4 3 9 8 0 . 5 0 2 2 0 . 5 6 4 5 0 . 62 7 3 0 . 6 8 9 5 0 . 7 5 1 5 0 . 8 1 32 0 . 8 7 4 8 0 . 9 3 5 9 0 . 9 9 7 5 1 . 0 5 8 6 1 . 11 9 0 1 . 1 7 8 7 1 . 2 3 7 8 1 . 2 9 6 4 1 . 3 5 2 5 1 . 4 0 7 5 1 . 4 5 7 2 1 . 4 9 6 8 1 . 5 3 4 9 1 . 5 6 5 9 1 . 5 7 7 7 1 . 5 8 6 7 1 . 5 8 9 9 1 . 5 9 5 1 1 . 6 0 0 7 1 . 5 9 9 4 1 . 5 9 5 7 1 . 5 9 6 7 1 . 5 9 8 8 1 . 5 9 9 6 1 . 5 9 6 3 1 . 5 9 4 5

Re = 2 . 0 0 0 e 6 Nc r it

CD Re ( CL) CM - - ------- --------- ------- -

0 . 0 0 7 3 4 2 . 0 0 0 0 0 - 0 . 0 7 2 4 0 0 . 0 0 7 0 6 2 . 0 0 0 0 0 - 0 . 0 7 42 0 0 . 0 0 6 8 4 2 . 0 0 0 0 0 - 0 . 0 7 5 9 0 0 . 0 0 6 7 2 2 . 0 0 0 0 0 - 0 . 0 7 7 3 0 0 . 0 0 6 7 2 2 . 0 0 0 0 0 - 0 . 0 7 8 5 0 0 . 0 0 6 7 2 2 . 0 0 0 0 0 - 0 . 0 7 97 0 0 . 0 0 6 7 1 2 . 0 0 0 0 0 - 0 . 0 8 1 1 0 0 . 0 0 6 7 4 2 . 0 0 0 0 0 - 0 . 0 8 2 3 0 0 . 0 0 6 7 8 2 . 0 0 0 0 0 - 0 . 0 8 3 4 0 0 . 0 0 6 8 5 2 . 0 0 0 0 0 - 0 . 0 8 4 6 0 0 . 0 0 6 8 8 2 . 0 0 0 0 0 - 0 . 0 8 5 8 0 0 . 0 0 6 9 1 2 . 0 0 0 0 0 - 0 . 0 8 7 0 0

0 . 0 0 6 9 9 2 . 0 0 0 0 0 - 0 . 0 8 8 1 0 . 0 0 7 0 8 2 . 0 0 0 0 0 - 0 . 0 8 92 0 . 0 0 7 1 8 2 . 0 0 0 0 0 - 0 . 0 9 0 3 0 . 0 0 7 2 9 2 . 0 0 0 0 0 - 0 . 0 9 1 3 0 . 0 0 7 3 4 2 . 0 0 0 0 0 - 0 . 0 92 5 0 . 0 0 7 4 7 2 . 0 0 0 0 0 - 0 . 0 9 3 5 0 . 0 0 7 5 8 2 . 0 0 0 0 0 - 0 . 0 9 4 5 0 . 0 0 7 7 2 2 . 0 0 0 0 0 - 0 . 0 9 5 5 0 . 0 0 7 8 7 2 . 0 0 0 0 0 - 0 . 0 9 6 4 0 . 0 0 8 0 8 2 . 0 0 0 0 0 - 0 . 0 9 7 2 0 . 0 0 8 1 9 2 . 0 0 0 0 0 - 0 . 0 9 8 1 0 . 0 0 8 3 7 2 . 0 0 0 0 0 - 0 . 0 9 9 0 0 . 0 0 8 6 1 2 . 0 0 0 0 0 - 0 . 0 9 9 7 0 . 0 0 8 8 9 2 . 0 0 0 0 0 - 0 . 1 0 0 3 0 . 0 0 922 2 . 0 0 0 0 0 - 0 . 1 0 0 8 0 . 0 0 9 5 8 2 . 0 0 0 0 0 - 0 . 1 0 1 3 0 . 0 1 0 1 6 2 . 0 0 0 0 0 - 0 . 1 0 1 4 0 . 0 1 0 8 0 2 . 0 0 0 0 0 - 0 . 1 0 1 5 0 . 0 1 1 8 8 2 . 0 0 0 0 0 - 0 . 1 0 0 9 0 . 0 1 3 6 9 2 . 0 0 0 0 0 - 0 . 0 9 92 0 . 0 1 5 3 7 2 . 0 0 0 0 0 - 0 . 0 9 7 3 0 . 0 1 7 2 7 2 . 0 0 0 0 0 - 0 . 0 9 4 5 0 . 0 1 9 3 8 2 . 0 0 0 0 0 - 0 . 0 8 9 3 0 . 0 2 2 5 6 2 . 0 0 0 0 0 - 0 . 0 8 6 1 0 . 0 2 7 0 7 2 . 0 0 0 0 0 - 0 . 0 8 4 3 0 . 0 3 2 1 0 2 . 0 0 0 0 0 - 0 . 0 8 3 6 0 . 0 3 7 4 5 2 . 0 0 0 0 0 - 0 . 0 8 32 0 . 0 4 3 9 9 2 . 0 0 0 0 0 - 0 . 0 8 3 3 0 . 0 5 1 1 3 2 . 0 0 0 0 0 - 0 . 0 8 3 7 0 . 0 5 7 8 4 2 . 0 0 0 0 0 - 0 . 0 8 4 2 0 . 0 6 4 6 9 2 . 0 0 0 0 0 - 0 . 0.8 4 9 0 . 0 7 1 9 0 2 . 0 0 0 0 0 - 0 . 0 8 5 8 0 . 0 7 9 7 0 2 . 0 0 0 0 0 - 0 . 0 8 6 8 0 . 0 8 7 5 7 2 . 0 0 0 0 0 - 0 . 0 8 8 2

POL . W3_2 1 1_2 0_9 ; 2

9 . 0 0 0

S xt r P xt r ------- -------0 . 5 3 5 5 0 0 . 3 5 7 2 0 0 . 52 7 7 0 0 . 3 8 8 1 0 0 . 5 1 1 8 0 0 . 4 1 6 3 0 0 . 5 0 5 3 0 0 . 4 3 9 9 0 0 . 4 9 3 5 0 0 . 4 4 3 9 0 0 . 4 8 5 8 0 0 . 4 4 8 4 0 0 . 4 7 8 3 0 0 . 4 5 6 2 0 0 . 4 6 5 9 0 0 . 4 62 0 0 0 . 4 6 1 1 0 0 . 4 6 5 3 0 0 . 4 5 3 3 0 0 . 4 6 8 0 0 0 . 4 4 3 6 0 0 . 4 7 4 6 0 0 . 4 3 9 8 0 0 . 4 8 0 3 0 0 . 4 3 2 9 0 . 4 8 4 1 0 . 42 3 7 0 . 4 8 7 1 0 . 4 1 9 2 0 . 4 8 9 2 0 . 4 1 4 5 0 . 4 9 0 9 0 . 4 0 8 1 0 . 4 9 7 8 0 . 3 9 9 4 0 . 5 0 3 1 0 . 3 9 5 7 0 . 5 0 62 0 . 3 9 0 9 0 . 5 0 8 6 0 . 3 8 4 1 0 . 5 1 0 6 0 . 3 7 5 3 0 . 5 1 2 6 0 . 37 1 5 0 . 5 1 7 3 0 . 3 6 4 6 0 . 52 2 7 0 . 3 5 2 3 0 . 52 6 4 0 . 3 4 2 4 0 . 52 9 1 0 . 3 2 7 4 0 . 5 3 1 6 0 . 3 1 52 0 . 5 3 3 6 0 . 2 9 0 3 0 . 5352 0 . 2 6 3 8 0 . 5 4 1 4 0 . 2 3 1 8 0 . 5 4 6 3 0 . 1 7 1 4 0 . 5 5 0 1 0 . 1 3 2 3 0 . 5 52 6 0 . 1 0 4 2 0 . 5 5 4 7 0 . 0 8 5 0 0 . 5 5 6 5 0 . 0 7 0 9 0 . 5 5 9 8 0 . 0 62 9 0 . 5 6 5 2 0 . 0 5 4 8 0 . 5 6 9 4 0 . 0 4 7 1 0 . 57 3 1 0 . 0 4 4 9 0 . 5 7 5 4 0 . 0 4 1 9 0 . 57 7 3 0 . 0 3 8 2 0 . 5 7 9 1 0 . 0 3 4 7 0 . 5 8 3 3 0 . 0 3 1 4 0 . 5 8 8 5 0 . 0 2 9 7 0 . 5 9 2 5 0 . 0 2 92 0 . 5 9 5 6

FFA TN 1 9 9 0 - 1 5 6 3 POL . W3_2 1 1_3 0_9 ; 1

XFOI L Version 5 . 0

Calculated polar for : FFA-W3-2 1 1

1 Reynolds number fixed

xt rf ... 1 . 0 0 0 ( suction) 1 . 0 0 0 (pre s sure ) Mach = 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xt r ------- -------- --------- -------- - -------- ------- -------- 6 . 0 0 0 0 0 - 0 . 3 8 5 2 0 0 . 0 0 7 3 8 3 . 0 0 0 0 0 - 0 . 0 7 1 9 0 0 . 5 1 8 1 0 0 . 2 9 3 1 0 - 5 . 5 0 0 0 0 - 0 . 3 1 7 9 0 0 . 0 0 6 6 5 3 . 0 0 0 0 0 - 0 . 0 7 4 8 0 0 . 5 0 4 1 0 0 . 3 6 2 0 0 - 5 . 0 0 0 0 0 - 0 . 2 5 3 3 0 0 . 0 0 6 4 3 3 . 0 0 0 0 0 - 0 . 0 7 6 4 0 0 . 4 9 6 8 0 0 . 3 8 5 4 0 - 4 . 5 0 0 0 0 - 0 . 1 8 8 6 0 0 . 0 0 6 1 3 3 . 0 0 0 0 0 - 0 . 0 7 8 2 0 0 . 4 8 4 9 0 0 . 42 6 5 0 - 4 . 0 0 0 0 0 - 0 . 12 5 1 0 0 . 0 0 6 12 3 . 0 0 0 0 0 - 0 . 0 7 9 4 0 0 . 4 7 8 4 0 0 . 4 3 2 0 0 - 3 . 5 0 0 0 0 - 0 . 0 6 1 5 0 0 . 0 0 6 1 2 3 . 0 0 0 0 0 - 0 . 0 8 0 7 0 0 . 4 6 6 8 0 0 . 4 3 9 8 0 - 3 . 0 0 0 0 0 0 . 0 0 1 9 0 0 . 0 0 6 1 2 3 . 0 0 0 0 0 - 0 . 0 8 1 9 0 0 . 4 6 0 3 0 0 . 4 4 5 0 0 - 2 . 5 0 0 0 0 0 . 0 6 5 2 0 0 . 0 0 6 1 5 3 . 0 0 0 0 0 - 0 . 0 8 3 1 0 0 . 4 5 3 3 0 0 . 4 4 7 7 0 -2 . 0 0 0 0 0 0 . 12 8 6 0 0 . 0 0 6 1 6 3 . 0 0 0 0 0 - 0 . 0 8 4 3 0 0 . 4 4 3 7 0 0 . 4 5 5 3 0 - 1 . 5 0 0 0 0 0 . 1 9 1 8 0 0 . 0 0 6 1 9 3 . 0 0 0 0 0 - 0 . 0 8 5 5 0 0 . 4 3 8 6 0 0 . 4 6 1 3 0 - 1 . 0 0 0 0 0 0 . 2 5 4 9 0 0 . 0 0 62 4 3 . 0 0 0 0 0 - 0 . 0 8 6 7 0 0 . 4 3 0 8 0 0 . 4 6 4 9 0 - 0 . 5 0 0 0 0 0 . 3 1 7 8 0 0 . 0 0 6 3 0 3 . 0 0 0 0 0 - 0 . 0 8 7 8 0 0 . 42 3 8 0 0 . 4 6 7 0 0

0 . 0 0 0 0 0 0 . 3 8 0 8 0 0 . 0 0 6 3 5 3 . 0 0 0 0 0 - 0 . 0 8 9 0 0 0 . 4 1 9 1 0 0 . 4 7 4 2 0 0 . 5 0 0 0 0 0 . 4 4 3 7 0 0 . 0 0 6 4 1 3 . 0 0 0 0 0 - 0 . 0 9 0 1 0 0 . 4 1 2 1 0 0 . 4 7 9 0 0 1 . 0 0 0 0 . 5 0 6 4 0 . 0 0 6 4 9 3 . 0 0 0 0 0 - 0 . 0 9 1 2 0 . 4 0 5 0 0 . 4 8 2 6 1 . 5 0 0 0 . 5 6 8 9 0 . 0 0 6 5 8 3 . 0 0 0 0 0 - 0 . 0 9 22 0 . 4 0 1 2 0 . 4 8 4 7 2 . 0 0 0 0 . 6 3 1 4 0 . 0 0 6 6 8 3 . 0 0 0 0 0 - 0 . 0 9 3 3 0 . 3 9 5 8 0 . 4 8 7 5 2 . 5 0 0 0 . 6 9 3 8 0 . 0 0 6 7 8 3 . 0 0 0 0 0 - 0 . 0 9 4 4 0 . 3 8 6 3 0 . 4 9 3 3 3 . 0 0 0 0 . 7 5 6 1 0 . 0 0 6 8 7 3 . 0 0 0 0 0 - 0 . 0 9 5 4 0 . 3 8 3 1 0 . 4 9 8 1 3 . 5 0 0 0 . 8 1 8 1 0 . 0 0 7 0 0 3 . 0 0 0 0 0 - 0 . 0 9 6 3 0 . 3 7 8 7 0 . 5 0 0 9 4 . 0 0 0 0 . 8 7 9 9 0 . 0 0 7 1 4 3 . 0 0 0 0 0 - 0 . 0 9 7 3 0 . 3 6 9 8 0 . 5 0 2 9 4 . 5 0 0 0 . 9 4 1 5 0 . 0 0 7 2 9 3 . 0 0 0 0 0 - 0 . 0 9 8 1 0 . 3 6 4 7 0 . 5 0 4 5 5 . 0 0 0 1 . 0 0 3 0 0 . 0 0 7 4 4 3 . 0 0 0 0 0 - 0 . 0 9 9 0 0 . 3 5 9 0 0 . 5 0 9 9 5 . 5 0 0 1 . 0 6 4 1 0 . 0 0 7 6 4 3 . 0 0 0 0 0 - 0 . 0 9 9 9 0 . 3 4 7 2 0 . 5 1 4 5 6 . 0 0 0 1 . 1 2 4 7 0 . 0 0 7 8 8 3 . 0 0 0 0 0 - 0 . 1 0 0 6 0 . 3 3 8 7 0 . 5 1 7 8 6 . 5 0 0 1 . 1 8 4 4 0 . 0 0 8 1 9 3 . 0 0 0 0 0 - 0 . 1 0 1 2 0 . 32 3 3 0 . 52 0 5 7 . 0 0 0 1 . 2 4 3 3 0 . 0 0 8 5 7 3 . 0 0 0 0 0 - 0 . 1 0 1 7 0 . 3 0 5 4 0 . 52 2 3 7 . 5 0 0 1 . 3 0 1 7 0 . 0 0 8 9 9 3 . 0 0 0 0 0 - 0 . 1 0 2 2 0 . 2 8 8 0 0 . 52 3 8 8 . 0 0 0 1 . 3 5 6 8 0 . 0 0 9 7 3 3 . 0 0 0 0 0 - 0 . 1 0 2 2 0 . 2 5 3 0 0 . 52 9 2 8 . 5 0 0 1 . 4 0 92 0 . 0 1 0 6 6 3 . 0 0 0 0 0 - 0 . 1 0 2 0 0 . 2 2 0 6 0 . 5 3 4 2 9 . 0 0 0 1 . 4 5 5 4 0 . 0 1 2 0 9 3 . 0 0 0 0 0 - 0 . 1 0 1 0 0 . 1 7 1 5 0 . 5 372 9 . 5 0 0 1 . 5 0 0 1 0 . 0 1 3 4 7 3 . 0 0 0 0 0 - 0 . 0 9 9 8 0 . 1 3 4 3 0 . 5 3 9 5

1 0 . 0 0 0 1 . 5 4 2 5 0 . 0 1 4 8 6 3 . 0 0 0 0 0 - 0 . 0 9 8 3 0 . 1 0 2 0 0 . 5 4 1 3 1 0 . 5 0 0 1 . 5 8 0 5 0 . 0 1 6 3 8 3 . 0 0 0 0 0 - 0 . 0 9 6 3 0 . 0 8 1 9 0 . 5 4 2 9 1 1 . 5 0 0 1 . 6 2 1 4 0 . 0 2 0 2 5 3 . 0 0 0 0 0 - 0 . 0 8 8 6 0 . 0 5 3 1 0 . 5 5 3 3 1 2 . 0 0 0 1 . 6 2 9 1 0 . 0 2 3 9 0 3 . 0 0 0 0 0 - 0 . 0 8 6 1 0 . 0 4 8 6 0 . 5 5 62 1 2 . 5 0 0 1 . 6 3 9 0 0 . 0 2 8 12 3 . 0 0 0 0 0 - 0 . 0 8 5 0 0 . 0 42 8 0 . 55 8 5 1 3 . 0 0 0 1 . 6 5 1 2 0 . 0 3 2 5 9 3 . 0 0 0 0 0 - 0 . 0 8 4 5 0 . 0 3 6 8 0 . 5 6 0 3 1 3 . 5 0 0 1 . 6 5 0 8 0 . 0 3 8 7 4 3 . 0 0 0 0 0 - 0 . 0 8 4 4 0 . 0 3 5 4 0 . 5 6 1 9 1 4 . 0 0 0 1 . 6 4 9 0 0 . 0 4 5 5 0 3 . 0 0 0 0 0 - 0 . 0 8 4 7 0 . 0 3 3 2 0 . 5 6 7 9 1 4 . 5 0 0 1 . 6 4 92 0 . 0 52 2 4 3 . 0 0 0 0 0 - 0 . 0 8 5 1 0 . 0 2 9 5 0 . 5 7 2 0 1 5 . 0 0 0 1 . 6 5 1 4 0 . 0 5 8 9 8 3 . 0 0 0 0 0 - 0 . 0 8 5 8 0 . 0 2 6 8 0 . 5 7 5 1

FFA TN 1 9 9 0 - 1 5 6 4

XFOI L Vers ion 5 . 0

Ca lculated polar for : FFA-W3- 2 1 1

1 Reynolds numbe r fixed

xt rf = 0 . 0 1 0 ( suct ion) 0 . 1 0 0 (pressure ) Mach =

a lpha --- - -- -

- 6 . 0 0 0 0 0 - 5 . 5 0 0 0 0 - 5 . 0 0 0 0 0 - 4 . 5 0 0 0 0 - 4 . 0 0 0 0 0 - 3 . 5 0 0 0 0 - 3 . 0 0 0 0 0 -2 . 5 0 0 0 0 -2 . 0 0 0 0 0 - 1 . 5 0 0 0 0 - 1 . 0 0 0 0 0 - 0 . 5 0 0 0 0

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0 1 5 . 5 0 0 1 6 . 0 0 0 1 6 . 5 0 0

0 . 1 5 0

CL --------

- 0 . 4 0 2 0 0 - 0 . 3 3 7 5 0 - 0 . 2 7 9 9 0 - 0 . 2 1 6 1 0 - 0 . 1 52 3 0 - 0 . 0 8 8 8 0 - 0 . 0 2 5 4 0

0 . 0 3 7 9 0 0 . 1 0 0 9 0 0 . 1 6 3 7 0 0 . 2 2 6 4 0 0 . 2 8 8 8 0

0 . 3 5 1 0 0 . 4 1 2 9 0 . 4 7 4 5 0 . 5 3 5 9 0 . 5 9 6 9 0 . 6 5 7 6 0 . 7 1 7 8 0 . 7 7 7 6 0 . 8 3 7 0 0 . 8 9 5 7 0 . 9 5 3 9 1 . 0 1 1 3 1 . 0 6 8 0 1 . 1 2 3 7 1 . 1 7 8 3 1 . 2 3 1 6 1 . 2 8 3 3 1 . 3 3 3 0 1 . 3 8 0 0 1 . 4 1 9 0 1 . 4 42 7 1 . 4 6 6 4 1 . 4 8 6 4 1 . 5 0 3 0 1 . 5 1 7 4 1 . 52 8 8 1 . 5 3 8 8 1 . 5 4 65 1 . 5 5 2 1 1 . 5 5 7 5 1 . 5 6 1 7 1 . 5 6 4 1 1 . 5 6 6 0 1. 5 6 9 3

Re = 3 . 0 0 0 e 6 Ncr it

CD Re ( CL ) CM --------- -------- - - - ------

0 . 0 1 0 1 0 3 . 0 0 0 0 0 - 0 . 0 6 4 3 0 0 . 0 0 9 8 5 3 . 0 0 0 0 0 - 0 . 0 6 6 2 0 0 . 0 1 1 5 8 3 . 0 0 0 0 0 - 0 . 0 6 7 8 0 0 . 0 1 1 4 5 3 . 0 0 0 0 0 - 0 . 0 6 9 5 0 0 . 0 1 1 3 6 3 . 0 0 0 0 0 - 0 . 0 7 1 1 0 0 . 0 1 12 9 3 . 0 0 0 0 0 - 0 . 0 7 2 7 0 0 . 0 1 1 2 4 3 . 0 0 0 0 0 - 0 . 0 7 4 3 0 0 . 0 1 1 2 1 3 . 0 0 0 0 0 - 0 . 0 7 5 7 0 0 . 0 1 1 2 1 3 . 0 0 0 0 0 - 0 . 0 7 7 2 0 0 . 0 1 1 2 3 3 . 0 0 0 0 0 - 0 . 0 7 8 6 0 0 . 0 1 1 2 7 3 . 0 0 0 0 0 - 0 . 0 8 0 0 0 0 . 0 1 1 3 4 3 . 0 0 0 0 0 - 0 . 0 8 1 3 0

0 . 0 1 1 4 2 3 . 0 0 0 0 0 - 0 . 0 8 2 5 0 . 0 1 1 5 3 3 . 0 0 0 0 0 - 0 . 0 8 3 7 0 . 0 1 1 6 6 3 . 0 0 0 0 0 - 0 . 0 8 4 9 0 . 0 1 1 8 1 3 . 0 0 0 0 0 - 0 . 0 8 6 0 0 . 0 1 1 9 9 3 . 0 0 0 0 0 - 0 . 0 8 7 1 0 . 0 1 2 1 9 3 . 0 0 0 0 0 - 0 . 0 8 8 0 0 . 0 12 4 1 3 . 0 0 0 0 0 - 0 . 0 8 9 0 0 . 0 1 2 6 7 3 . 0 0 0 0 0 - 0 . 0 8 9 8 0 . 0 12 9 5 3 . 0 0 0 0 0 - 0 . 0 9 0 6 0 . 0 1 3 2 6 3 . 0 0 0 0 0 - 0 . 0 9 1 3 0 . 0 1 3 6 1 3 . 0 0 0 0 0 - 0 . 0 9 1 9 0 . 0 1 3 9 9 3 . 0 0 0 0 0 - 0 . 0 92 4 0 . 0 1 4 4 0 3 . 0 0 0 0 0 - 0 . 0 92 7 0 . 0 1 4 8 6 3 . 0 0 0 0 0 - 0 . 0 9 3 0 0 . 0 1 5 3 7 3 . 0 0 0 0 0 - 0 . 0 9 3 1 0 . 0 1 5 9 3 3 . 0 0 0 0 0 - 0 . 0 9 3 0 0 . 0 1 6 5 6 3 . 0 0 0 0 0 - 0 . 0 92 7 0 . 0 1 7 2 6 3 . 0 0 0 0 0 - 0 . 0 92 2 0 . 0 1 8 0 7 3 . 0 0 0 0 0 - 0 . 0 9 1 3 0 . 0 1 9 0 0 3 . 0 0 0 0 0 - 0 . 0 8 92 0 . 0 2 0 4 4 3 . 0 0 0 0 0 - 0 . 0 8 5 5 0 . 0 2 2 5 9 3 . 0 0 0 0 0 - 0 . 0 8 3 5 0 . 0 2 5 5 0 3 . 0 0 0 0 0 - 0 . 0 8 2 1 0 . 02 9 1 6 3 . 0 0 0 0 0 - 0 . 0 8 1 4 0 . 0 3 3 4 2 3 . 0 0 0 0 0 - 0 . 0 8 1 1 0 . 0 3 8 2 3 3 . 0 0 0 0 0 - 0 . 0 8 1 0 0 . 0 4 3 5 4 3 . 0 0 0 0 0 - 0 . 0 8 1 2 0 . 0 4 92 8 3 . 0 0 0 0 0 - 0 . 0 8 1 6 0 . 0 5 5 4 6 3 . 0 0 0 0 0 - 0 . 0 8 2 1 0 . 0 6 1 8 4 3 . 0 0 0 0 0 - 0 . 0 8 2 8 0 . 0 6 8 5 4 3 . 0 0 0 0 0 - 0 . 0 8 3 7 0 . 0 7 5 5 4 3 . 0 0 0 0 0 - 0 . 0 8 4 7 0 . 0 8 2 7 9 3 . 0 0 0 0 0 - 0 . 0 8 5 8 0 . 0 8.9 9 8 3 . 0 0 0 0 0 - 0 . 0 8 7 0

POL . W3_2 1 1_3 0_TU1 ; 2

9 . 0 0 0

S xt r P xt r ---- - - - -------0 . 5 1 93 0 0 . 1 0 0 0 0 0 . 5 0 7 7 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 6 5 POL . W3_2 4 1_1 0_9 ; 1

XFOI L Vers ion 5 . 0

Calculated polar for : FFA-W3 -2 4 1

1 Reynolds numbe r fixed

xt r f - 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pre s sure ) Mach = 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM s xt r P xt r - ------ ------- - --------- -------- - -------- ------- -------- 3 . 5 0 0 0 0 - 0 . 0 9 6 3 0 0 . 0 0 9 4 0 1 . 0 0 0 0 0 - 0 . 0 8 1 7 0 0 . 5 1 9 0 0 0 . 4 3 9 4 0 - 3 . 0 0 0 0 0 - 0 . 0 3 0 4 0 0 . 0 0 9 4 1 1 . 0 0 0 0 0 - 0 . 0 8 3 6 0 0 . 5 0 2 7 0 0 . 4 4 3 9 0 - 2 . 5 0 0 0 0 0 . 0 3 4 9 0 0 . 0 0 9'4 5 1 . 0 0 0 0 0 - 0 . 0 8 5 2 0 0 . 4 9 4 4 0 0 . 4 4 7 8 0 -2 . 0 0 0 0 0 0 . 1 0 1 1 0 0 . 0 0 9 4 1 1 . 0 0 0 0 0 - 0 . 0 8 7 1 0 0 . 4 8 0 1 0 0 . 4 5 4 6 0 - 1 . 5 0 0 0 0 0 . 1 6 6 9 0 0 . 0 0 9 4 0 1 . 0 0 0 0 0 - 0 . 0 8 8 9 0 0 . 4 7 2 7 0 0 . 4 6 1 3 0 - 1 . 0 0 0 0 0 0 . 2 3 1 7 0 0 . 0 0 9 4 9 1 . 0 0 0 0 0 - 0 . 0 9 0 4 0 0 . 4 5 9 5 0 0 . 4 6 5 9 0 - 0 . 5 0 0 0 0 0 . 2 9 62 0 0 . 0 0 9 5 8 1 . 0 0 0 0 0 - 0 . 0 9 1 8 0 0 . 4 5 0 9 0 0 . 4 6 9 3 0

0 . 0 0 0 0 . 3 6 0 5 0 . 0 0 9 6 9 1 . 0 0 0 0 0 - 0 . 0 9 32 0 . 4 42 6 0 . 4 7 2 1 0 . 5 0 0 0 . 4 2 5 7 0 . 0 0 9 7 3 1 . 0 0 0 0 0 - 0 . 0 9 4 9 0 . 42 9 8 0 . 4 8 0 5 1 . 0 0 0 0 . 4 9 0 0 0 . 0 0 9 8 2 1 . 0 0 0 0 0 - 0 . 0 9 6 3 0 . 4 2 3 5 0 . 4 8 5 4 1 . 5 0 0 0 . 5 5 3 7 0 . 0 0 9 9 7 1 . 0 0 0 0 0 - 0 . 0 9 7 5 0 . 4 1 1 8 0 . 4 8 8 9 2 . 0 0 0 0 . 6 1 6 8 0 . 0 1 0 1 5 1 . 0 0 0 0 0 - 0 . 0 9 8 6 0 . 4 0 4 0 0 . 4 92 2 2 . 5 0 0 0 . 6 7 9 9 0 . 0 1 0 3 3 1 . 0 0 0 0 0 - 0 . 0 9 9 7 0 . 3 9 7 3 0 . 4 9 4 8 3 . 0 0 0 0 . 7 4 3 5 0 . 0 1 0 4 6 1 . 0 0 0 0 0 - 0 . 1 0 1 0 0 . 3 8 4 3 0 . 5 0 1 3 3 . 5 0 0 0 . 8 0 6 4 0 . 0 1 0 6 1 1 . 0 0 0 0 0 - 0 . 1 0 2 2 0 . 3 7 8 7 0 . 5 0 6 6 4 . 0 0 0 0 . 8 6 8 5 0 . 0 1 0 8 4 1 . 0 0 0 0 0 - 0 . 1 0 3 1 0 . 3 7 1 6 0 . 5 1 0 5 4 . 5 0 0 0 . 92 9 9 0 . 0 1 1 1 4 1 . 0 0 0 0 0 - 0 . 1 0 3 9 0 . 3 5 8 7 0 . 5 1 35 5 . 0 0 0 0 . 9 9 1 3 0 . 0 1 1 3 7 1 . 0 0 0 0 0 - 0 . 1 0 4 6 0 . 3 5 3 4 0 . 5 1 62 5 . 5 0 0 1 . 0 5 1 8 0 . 0 1 1 6 8 1 . 0 0 0 0 0 - 0 . 1 0 52 0 . 3 4 2 9 0 . 5 1 8 5 6 . 0 0 0 1 . 1 1 2 8 0 . 0 1 1 9 2 1 . 0 0 0 0 0 - 0 . 1 0 6 1 0 . 3 3 3 3 0 . 52 5 8 6 . 5 0 0 1 . 1 7 2 3 0 . 0 1 2 2 5 1 . 0 0 0 0 0 - 0 . 1 0 6 5 0 . 32 5 2 0 . 5 3 0 6 7 . 0 0 0 1 . 2 3 0 5 0 . 0 1 2 6 8 1 . 0 0 0 0 0 - 0 . 1 0 6 8 0 . 3 1 0 9 0 . 5 3 3 9 7 . 5 0 0 1 . 2 8 8 3 0 . 0 1 3 0 8 1 . 0 0 0 0 0 - 0 . 1 0 7 0 0 . 3 0 4 5 0 . 5 3 6 8 8 . 0 0 0 1 . 3 4 4 3 0 . 0 1 3 6 0 1 . 0 0 0 0 0 - 0 . 1 0 6 9 0 . 2 8 9 0 0 . 5 3 9 5 8 . 5 0 0 1 . 3 9 8 3 0 . 0 1 42 0 1 . 0 0 0 0 0 - 0 . 1 0 6 4 0 . 2 7 9 5 0 . 5 4 1 9 9 . 0 0 0 1 . 4 5 2 5 0 . 0 1 4 7 3 1 . 0 0 0 0 0 - 0 . 1 0 62 0 . 2 6 4 3 0 . 5 4 9 5 9 . 5 0 0 1 . 5 0 1 6 0 . 0 1 5 5 3 1 . 0 0 0 0 0 - 0 . 1 0 5 2 0 . 2 5 3 2 0 . 55 3 7

1 0 . 0 0 0 1 . 5 4 8 5 0 . 0 1 6 3 6 1 . 0 0 0 0 0 - 0 . 1 0 3 8 0 . 2 3 8 7 0 . 5 5 7 0 1 0 . 5 0 0 1 . 5 8 8 2 0 . 0 1 7 3 9 1 . 0 0 0 0 0 - 0 . 1 0 1 3 0 . 2 2 7 6 0 . 5 5 9 9 1 1 . 0 0 0 1 . 6 0 9 3 0 . 0 1 8 7 3 1 . 0 0 0 0 0 - 0 . 0 9 6 0 0 . 2 1 4 7 0 . 5 62 5 1 1 . 5 0 0 1 . 6 3 0 1 0 . 0 2 0 7 2 1 . 0 0 0 0 0 - 0 . 0 92 0 0 . 2 0 3 1 0 . 5 6 4 9 1 2 . 0 0 0 1 . 6 4 1 6 0 . 0 2 3 6 8 1 . 0 0 0 0 0 - 0 . 0 8 8 5 0 . 1 8 7 9 0 . 5 7 1 4 1 3 . 0 0 0 1 . 6 5 2 8 0 . 0 32 2 6 1 . 0 0 0 0 0 - 0 . 0 8 4 0 0 . 1 6 3 5 0 . 5 7 8 7 1 3 . 5 0 0 1. 6 5 4 4 0 . 0 3 7 8 2 1 . 0 0 0 0 0 - 0 . 0 8 3 0 0 . 1 4 8 4 0 . 5 8 1 4 1 4 . 0 0 0 1 . 6 4 8 4 0 . 0 4 4 5 8 1 . 0 0 0 0 0 - 0 . 0 8 2 6 0 . 1 4 0 7 0 . 5 8 3 7 1 5 . 0 0 0 1 . 6 2 8 8 0 . 0 6 0 5 4 1 . 0 0 0 0 0 - 0 . 0 8 3 6 0 . 1 1 8 1 0 . 5 8 7 8 1 5 . 5 0 0 1 . 62 2 9 0 . 0 6 8 6 3 1 . 0 0 0 0 0 - 0 . 0 8 4 8 0 . 1 0 5 6 0 . 5 92 7 1 6 . 0 0 0 1 . 6 1 3 3 0 . 0 7 7 4 6 1 . 0 0 0 0 0 - 0 . 0 8 6 2 0 . 1 0 1 4 0 . 5 9 7 1 1 6 . 5 0 0 1 . 6 0 2 8 0 . 0 8 6 7 6 1 . 0 0 0 0 0 - 0 . 0 8 8 0 0 . 0 9 4 4 0 . 6 0 0 1

FFA TN 1 9 9 0 - 1 5 6 6 POL . W3_2 4 1_1 0_TU1 ; 1

XFO IL Vers ion 5 . 0

Calculated polar for : FFA-W3-2 4 1

1 Reynolds numbe r fixed

xtrf = 0 . 0 1 0 ( suction ) 0 . 1 0 0 (pressure ) Mach = 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it 9 . 0 0 0

alpha CL CD Re (CL) CM S xt r P xt r ------- ------ - - ----- - --- --------- -------- ------- -------

0 . 0 0 0 0 . 2 9 4 0 0 . 0 1 6 0 6 1 . 0 0 0 0 0 - 0 . 0 7 7 1 0 . 0 1 0 0 0 . 1 0 0 0 0 . 50 0 0 . 3 6 0 0 0 . 0 1 6 0 5 1 . 0 0 0 0 0 - 0 . 0 7 9 6 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 . 4 2 52 0 . 0 1 6 1 0 1 . 0 0 0 0 0 - 0 . 0 8 1 8 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 4 8 9 4 0 . 0 1 6 2 0 1 . 0 0 0 0 0 - 0 . 0 8 3 8 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 5 5 2 8 0 . 0 1 6 3 5 1 . 0 0 0 0 0 - 0 . 0 8 5 6 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 6 1 5 3 0 . 0 1 6 5 5 1 . 0 0 0 0 0 - 0 . 0 8 7 1 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 7 6 8 0 . 0 1 6 8 0 1 . 0 0 0 0 0 - 0 . 0 8 8 5 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 7 3 7 2 0 . 0 1 7 0 9 1 . 0 0 0 0 0 - 0 . 0 8 9 7 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 7 9 6 5 0 . 0 1 7 4 4 1 . 0 0 0 0 0 - 0 . 0 9 0 6 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 8 5 4 5 0 . 0 1 7 8 5 1 . 0 0 0 0 0 - 0 . 0 9 1 3 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 9 1 1 0 0 . 0 1 8 3 1 1 . 0 0 0 0 0 - 0 . 0 9 1 8 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 9 6 5 8 0 . 0 1 8 8 4 1 . 0 0 0 0 0 - 0 . 0 9 2 0 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 1 . 0 1 8 6 0 . 0 1 9 4 4 1 . 0 0 0 0 0 - 0 . 0 9 2 0 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 0 6 8 8 0 . 0 2 0 1 4 1 . 0 0 0 0 0 - 0 . 0 9 1 5 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 1 1 53 0 . 0 2 0 9 5 1 . 0 0 0 0 0 - 0 . 0 9 0 6 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1 4 0 6 0 . 0 2 1 9 7 1 . 0 0 0 0 0 - 0 . 0 8 62 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1. 1 7 2 7 0 . 0 2 3 4 4 1 . 0 0 0 0 0 - 0 . 0 8 3 9 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 2 0 1 3 0 . 0 2 5 3 9 1 . 0 0 0 0 0 - 0 . 0 8 2 1 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 2 2 6 3 0 . 0 2 7 9 0 1 . 0 0 0 0 0 - 0 . 0 8 0 7 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 2 4 8 6 0 . 0 3 0 9 8 1 . 0 0 0 0 0 - 0 . 0 7 9 8 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 2 6 8 4 0 . 0 3 4 6 3 1 . 0 0 0 0 0 - 0 . 0 7 9 4 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 2 8 6 9 0 . 0 3 8 7 9 1 . 0 0 0 0 0 - 0 . 0 7 9 4 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 3 0 2 8 0 . 0 4 352 1 . 0 0 0 0 0 - 0 . 0 7 9 8 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 3 1 6 6 0 . 0 4 8 6 4 1 . 0 0 0 0 0 - 0 . 0 8 0 3 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 32 8 5 0 . 0 5 4 3 1 1 . 0 0 0 0 0 - 0 . 0 8 1 2 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 3 3 9 2 0 . 0 6 0 3 4 1 . 0 0 0 0 0 - 0 . 0 8 2 2 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 3 4 8 2 0 . 0 6 6 7 0 1 . 0 0 0 0 0 - 0 . 0 8 3 3 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 3 5 5 5 0 . 0 7 3 4 2 1 . 0 0 0 0 0 - 0 . 0 8 4 6 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 3 62 1 0 . 0 8 0 4 8 1 . 0 0 0 0 0 - 0 . 0 8 6 1 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 3 6 8 0 0 . 0 8 7 8 1 1 . 0 0 0 0 0 - 0 . 0 8 7 7 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 3 7 3 6 0 . 0 9 5 3 1 1 . 0 0 0 0 0 - 0 . 0 8 9 4 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 5 0 0 1 . 3 7 7 4 0 . 1 0 3 2 9 1 . 0 0 0 0 0 - 0 . 0 9 1 4 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 0 0 0 1 . 3 7 9 9 0 . 1 1 1 6 9 1 . 0 0 0 0 0 - 0 . 0 9 3 6 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 5 0 0 1 . 3 8 3 0 0 . 12 0 1 5 1 . 0 0 0 0 0 - 0 . 0 9 5 8 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 6 7 POL . W3_2 4 1_2 0_9 ; 1

XFOI L Ve rsion 5 . 0

Calculated po lar for : FFA-W3-2 4 1

1 Reynolds number fixed

xtrf ... 1 . 0 0 0 ( suction) 1 . 0 0 0 (pre ssure ) Mach c 0 . 1 5 0 Re = 2 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xt r - ------ -------- --------- --------- -------- ------- ---- - --- 4 . 0 0 0 0 0 - 0 . 1 4 8 1 0 0 . 0 0 7 8 2 2 . 0 0 0 0 0 - 0 . 0 8 3 8 0 0 . 4 9 6 8 0 0 . 4 1 5 2 0 - 3 . 5 0 0 0 0 - 0 . 0 8 2 0 0 0 . 0 0 7 7 8 2 . 0 0 0 0 0 - 0 . 0 8 5 6 0 0 . 4 7 9 8 0 0 . 42 1 0 0 - 3 . 0 0 0 0 0 - 0 . 0 1 6 6 0 0 . 0 0 7 7 8 2 . 0 0 0 0 0 - 0 . 0 8 7 2 0 0 . 4 7 3 1 0 0 . 42 5 1 0 - 2 . 5 0 0 0 0 0 . 0 4 9 4 0 0 . 0 0 7 7 6 2 . 0 0 0 0 0 - 0 . 0 8 9 0 0 0 . 4 6 1 0 0 0 . 4 3 2 0 0 - 2 . 0 0 0 0 0 0 . 1 1 5 0 0 0 . 0 0 7 7 6 2 . 0 0 0 0 0 - 0 . 0 9 0 7 0 0 . 4 5 0 9 0 0 . 4 3 9 5 0 - 1 . 5 0 0 0 0 0 . 1 8 0 2 0 0 . 0 0 7 7 8 2 . 0 0 0 0 0 - 0 . 0 92 2 0 0 . 4 4 1 6 0 0 . 4 4 5 0 0 - 1 . 0 0 0 0 0 0 . 2 4 5 1 0 0 . 0 0 7 8 4 2 . 0 0 0 0 0 - 0 . 0 9 3 7 0 0 . 4 3 0 2 0 0 . 4 4 8 0 0 - 0 . 5 0 0 0 0 0 . 3 1 0 1 0 0 . 0 0 7 8 9 2 . 0 0 0 0 0 - 0 . 0 9 5 2 0 0 . 42 3 0 0 0 . 4 5 3 0 0

0 . 0 0 0 0 . 3 7 52 0 . 0 0 7 9 3 2 . 0 0 0 0 0 - 0 . 0 9 6 8 0 . 4 1 1 8 0 . 4 6 1 5 0 . 5 0 0 0 . 4 3 9 8 0 . 0 0 8 0 0 2 . 0 0 0 0 0 - 0 . 0 9 8 2 0 . 4 0 4 6 0 . 4 6 6 1 1 . 0 0 0 0 . 5 0 3 9 0 . 0 0 8 1 1 2 . 0 0 0 0 0 - 0 . 0 9 9 5 0 . 3 9 6 7 0 . 4 6 9 5 1 . 5 0 0 0 . 5 6 7 9 0 . 0 0 8 2 4 2 . 0 0 0 0 0 - 0 . 1 0 0 7 0 . 3 8 5 1 0 . 4 7 2 1 2 . 0 0 0 0 . 6 3 2 3 0 . 0 0 8 3 1 2 . 0 0 0 0 0 - 0 . 1 0 2 1 0 . 3 7 9 9 0 . 4 7 8 9 2 . 5 0 0 0 . 6 9 6 0 0 . 0 0 8 4 5 2 . 0 0 0 0 0 - 0 . 1 0 3 3 0 . 3 7 1 4 0 . 4 8 5 0 3 . 0 0 0 0 . 7 5 9 6 0 . 0 0 8 5 9 2 . 0 0 0 0 0 - 0 . 1 0 4 4 0 . 3 5 9 8 0 . 4 8 9 7 3 . 5 0 0 0 . 8 2 2 6 0 . 0 0 8 7 7 2 . 0 0 0 0 0 - 0 . 1 0 5 5 0 . 3 5 42 0 . 4 9 2 5 4 . 0 0 0 0 . 8 8 5 3 0 . 0 0 8 9 7 2 . 0 0 0 0 0 - 0 . 1 0 6 5 0 . 3 4 5 9 0 . 4 9 4 7 4 . 5 0 0 0 . 9 4 8 1 0 . 0 0 9 1 6 2 . 0 0 0 0 0 - 0 . 1 0 7 5 0 . 3 3 5 0 0 . 4 9 9 2 5 . 0 0 0 1 . 0 1 0 4 0 . 0 0 9 3 6 2 . 0 0 0 0 0 - 0 . 1 0 8 4 0 . 32 8 6 0 . 5 0 6 5 5 . 5 0 0 1 . 0 7 2 1 0 . 0 0 9 62 2 . 0 0 0 0 0 - 0 . 1 0 92 0 . 3 1 4 9 0 . 5 1 0 8 6 . 0 0 0 1 . 1 3 3 3 0 . 0 0 9 8 9 2 . 0 0 0 0 0 - 0 . 1 0 9 9 0 . 3 0 8 2 0 . 5 1 3 8 6 . 5 0 0 1 . 1 9 3 5 0 . 0 1 0 2 3 2 . 0 0 0 0 0 - 0 . 1 1 0 5 0 . 2 9 6 4 0 . 5 1 62 7 . 0 0 0 1 . 2 52 9 0 . 0 1 0 6 1 2 . 0 0 0 0 0 - 0 . 1 1 0 9 0 . 2 8 4 4 0 . 5 1 8 4 7 . 5 0 0 1 . 3 1 2 2 0 . 0 1 0 9 8 2 . 0 0 0 0 0 - 0 . 1 1 1 3 0 . 2 7 4 3 0 . 52 4 4 8 . 0 0 0 1 . 3 7 0 0 0 . 0 1 1 4 3 2 . 0 0 0 0 0 - 0 . 1 1 1 5 0 . 2 6 0 3 0 . 5 3 0 1 8 . 5 0 0 1 . 4 2 6 0 0 . 0 1 1 9 8 2 . 0 0 0 0 0 - 0 . 1 1 1 4 0 . 2 4 1 5 0 . 5 3 4 1 9 . 0 0 0 1 . 4 8 0 1 0 . 0 1 2 6 1 2 . 0 0 0 0 0 - 0 . 1 1 1 0 0 . 2 3 2 8 0 . 5 3 7 2 9 . 5 0 0 1 . 5 3 3 4 0 . 0 1 3 2 4 2 . 0 0 0 0 0 - 0 . 1 1 0 4 0 . 2 1 6 7 0 . 5 3 9 5

1 0 . 0 0 0 1 . 5 8 2 7 0 . 0 1 4 0 6 2 . 0 0 0 0 0 - 0 . 1 0 9 3 0 . 2 0 5 4 0 . 5 4 1 4 1 0 . 5 0 0 1 . 6 3 0 4 0 . 0 1 4 8 9 2 . 0 0 0 0 0 - 0 . 1 0 8 0 0 . 1 9 1 0 0 . 5 4 6 8 1 1 . 0 0 0 1 . 6 6 7 3 0 . 0 1 6 1 2 2 . 0 0 0 0 0 - 0 . 1 0 5 1 0 . 17 02 0 . 5 5 2 5 1 1 . 5 0 0 1 . 6 8 3 9 0 . 0 1 7 6 3 2 . 0 0 0 0 0 - 0 . 0 9 9 1 0 . 1 5 8 9 0 . 5 5 6 3 1 2 . 0 0 0 1 . 7 0 1 7 0 . 0 1 9 6 8 2 . 0 0 0 0 0 - 0 . 0 9 4 6 0 . 1 4 6 1 0 . 5 5 9 5 1 2 . 5 0 0 1 . 7 1 12 0 . 0 2 2 6 8 2 . 0 0 0 0 0 - 0 . 0 9 0 5 0 . 1 3 3 6 0 . 5 6 1 7 1 3 . 0 0 0 1 . 7 0 6 8 0 . 0 2 7 4 1 2 . 0 0 0 0 0 - 0 . 0 8 7 2 0 . 1 2 1 1 0 . 5 6 3 4 1 3 . 5 0 0 1 . 7 1 35 0 . 0 3 1 9 8 2 . 0 0 0 0 0 - 0 . 0 8 5 5 0 . 1 0 8 4 0 . 5 6 5 0 1 4 . 0 0 0 1 . 7 1 0 8 0 . 0 3 8 0 5 2 . 0 0 0 0 0 - 0 . 0 8 4 7 0 . 1 0 2 3 0 . 5 7 0 1 1 4 . 5 0 0 1 . 7 0 62 0 . 0 4 4 7 8 2 . 0 0 0 0 0 - 0 . 0 8 4 4 0 . 0 9 4 6 0 . 5 7 4 8 1 5 . 0 0 0 1 . 7 0 6 6 0 . 0 5 1 4 4 2 . 0 0 0 0 0 - 0 . 0 8 4 6 0 . 0 8 5 0 0 . 5 7 8 4 1 5 . 5 0 0 1 . 7 0 0 4 0 . 0 5 9 12 2 . 0 0 0 0 0 - 0 . 0 8 5 2 0 . 0 8 2 0 0 . 5 8 1 6 1 6 . 0 0 0 1 . 6 8 9 8 0 . 0 67 7 1 2 . 0 0 0 0 0 - 0 . 0 8 62 0 . 0 7 7 3 0 . 5 8 3 6 1 6 . 5 0 0 1 . 6 8 8 0 0 . 0 7 5 3 8 2 . 0 0 0 0 0 - 0 . 0 8 7 2 0 . 0 7 0 8 0 . 5 8 5 4

FFA TN 1 9 9 0 - 1 5 6 8

XFOIL Ve rs ion 5 . 0

Ca lculated polar for : FFA-W3- 2 4 1

1 Reynolds number fixed

xt rf = 1 . 0 0 0 ( suction ) 1 . 0 0 0 (pre s sure ) Mach = 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncr it

a lpha CL CD Re (CL) CM ------- -------- --------- ---- - ---- ------- -

- 6 . 0 0 0 0 0 - 0 . 4 0 8 3 0 0 . 0 0 7 5 1 3 . 0 0 0 0 0 - 0 . 0 7 7 6 0 - 5 . 5 0 0 0 0 - 0 . 3 4 1 7 0 0 . 0 0 7 4 0 3 . 0 0 0 0 0 - 0 . 0 7 9 6 0 - 5 . 0 0 0 0 0 - 0 . 2 7 5 0 0 0 . 0 0 7 3 0 3 . 0 0 0 0 0 - 0 . 0 8 1 6 0 - 4 . 5 0 0 0 0 - 0 . 2 0 8 7 0 0 . 0 0 72 3 3 . 0 0 0 0 0 - 0 . 0 8 3 4 0 - 4 . 0 0 0 0 0 - 0 . 1 4 2 7 0 0 . 0 0 7 1 8 3 . 0 0 0 0 0 - 0 . 0 8 5 2 0 - 3 . 5 0 0 0 0 - 0 . 0 7 6 7 0 0 . 0 0 7 1 4 3 . 0 0 0 0 0 - 0 . 0 8 7 0 0 - 3 . 0 0 0 0 0 - 0 . 0 1 0 9 0 0 . 0 0 7 12 3 . 0 0 0 0 0 - 0 . 0 8 8 7 0 -2 . 5 0 0 0 0 0 . 0 5 4 7 0 0 . 0 0 7 1 1 3 . 0 0 0 0 0 - 0 . 0 9 0 3 0 - 2 . 0 0 0 0 0 0 . 1 1 9 9 0 0 . 0 0 7 1 4 3 . 0 0 0 0 0 - 0 . 0 9 1 9 0 - 1 . 5 0 0 0 0 0 . 1 8 5 4 0 0 . 0 0 7 1 4 3 . 0 0 0 0 0 - 0 . 0 9 3 5 0 - 1 . 0 0 0 0 0 0 . 2 5 0 5 0 0 . 0 0 7 1 8 3 . 0 0 0 0 0 - 0 . 0 9 5 0 0 - 0 . 5 0 0 0 0 0 . 3 1 5 5 0 0 . 0 0 7 2 2 3 . 0 0 0 0 0 - 0 . 0 9 6 5 0

0 . 0 0 0 0 . 3 8 0 2 0 . 0 0 7 2 9 3 . 0 0 0 0 0 - 0 . 0 9 7 9 0 . 5 0 0 0 . 4 4 4 9 0 . 0 0 7 3 5 3 . 0 0 0 0 0 - 0 . 0 9 9 3 1 . 0 0 0 0 . 5 0 9 5 0 . 0 0 7 4 2 3 . 0 0 0 0 0 - 0 . 1 0 0 7 1 . 5 0 0 0 . 5 7 3 9 0 . 0 0 7 52 3 . 0 0 0 0 0 - 0 . 1 0 2 0 2 . 0 0 0 0 . 6 3 7 9 0 . 0 0 7 6 3 3 . 0 0 0 0 0 - 0 . 1 0 3 3 2 . 5 0 0 0 . 7 0 1 6 0 . 0 0 7 7 6 3 . 0 0 0 0 0 - 0 . 1 0 4 4 3 . 0 0 0 0 . 7 6 5 3 0 . 0 0 7 9 1 3 . 0 0 0 0 0 - 0 . 1 0 5 7 3 . 5 0 0 0 . 8 2 9 1 0 . 0 0 8 0 3 3 . 0 0 0 0 0 - 0 . 1 0 6 8 4 . 0 0 0 0 . 8 92 3 0 . 0 0 8 1 9 3 . 0 0 0 0 0 - 0 . 1 0 7 9 4 . 5 0 0 0 . 9 5 4 8 0 . 0 0 8 4 1 3 . 0 0 0 0 0 - 0 . 1 0 8 8 5 . 0 0 0 1. 0 1 7 3 0 . 0 0 8 6 1 3 . 0 0 0 0 0 - 0 . 1 0 9 7 5 . 5 0 0 1 . 0 7 9 1 0 . 0 0 8 8 7 3 . 0 0 0 0 0 - 0 . 1 1 0 6 6 . 0 0 0 1 . 1 4 1 0 0 . 0 0 9 1 1 3 . 0 0 0 0 0 - 0 . 1 11 4 6 . 5 0 0 1 . 2 0 1 3 0 . 0 0 9 4 8 3 . 0 0 0 0 0 - 0 . 1 1 2 0 7 . 0 0 0 1 . 2 62 1 0 . 0 0 9 7 6 3 . 0 0 0 0 0 - 0 . 1 1 2 6 7 . 5 0 0 1 . 32 0 4 0 . 0 1 0 2 4 3 . 0 0 0 0 0 - 0 . 1 1 2 8 8 . 0 0 0 1 . 3 7 92 0 . 0 1 0 6 3 3 . 0 0 0 0 0 - 0 . 1 1 3 1 8 . 5 0 0 1 . 4 3 5 4 0 . 0 1 1 2 1 3 . 0 0 0 0 0 - 0 . 1 1 3 0 9 . 0 0 0 1 . 4 9 1 0 0 . 0 1 1 7 7 3 . 0 0 0 0 0 - 0 . 1 12 9 9 . 5 0 0 1 . 5 4 5 8 0 . 0 1 2 3 4 3 . 0 0 0 0 0 - 0 . 1 1 2 5

1 0 . 0 0 0 1 . 5 9 5 6 0 . 0 1 3 1 9 3 . 0 0 0 0 0 - 0 . 1 1 1 5 1 0 . 5 0 0 1 . 6 4 0 4 0 . 0 1 4 2 6 3 . 0 0 0 0 0 - 0 . 1 0 9 8 1 1 . 0 0 0 1 . 6 8 4 0 0 . 0 1 5 2 1 3 . 0 0 0 0 0 - 0 . 1 0 7 8 1 1 . 5 0 0 1 . 7 1 1 0 0 . 0 1 6 4 7 3 . 0 0 0 0 0 - 0 . 1 0 3 2 1 2 . 0 0 0 1 . 7 2 7 2 0 . 0 1 8 2 3 3 . 0 0 0 0 0 - 0 . 0 9 7 6 1 2 . 5 0 0 1 . 7 3 6 3 0 . 0 2 0 9 3 3 . 0 0 0 0 0 - 0 . 0 92 8 1 3 . 0 0 0 1 . 7 37 6 0 . 0 2 4 8 9 3 . 0 0 0 0 0 - 0 . 0 8 9 1 1 3 . 5 0 0 1 . 7 432 0 . 0 2 9 1 9 3 . 0 0 0 0 0 - 0 . 0 8 6 9 1 4 . 0 0 0 1 . 7 4 8 4 0 . 0 3 4 1 6 3 . 0 0 0 0 0 - 0 . 0 8 5 6 1 4 . 5 0 0 1 . 7 4 3 4 0 . 0 4 0 6 3 3 . 0 0 0 0 0 - 0 . 0 8 4 9 1 5 . 0 0 0 1 . 7 4 1 9 0 . 0 4 7 2 1 3 . 0 0 0 0 0 - 0 . 0 8 4 8 1 5 . 5 0 0 1 . 7 4 1 8 0 . 0 5 3 9 7 3 . 0 0 0 0 0 - 0 . 0 8 5 0 1 6 . 0 0 0 1 . 7 3 4 3 0 . 0 62 0 6 3 . 0 0 0 0 0 - 0 . 0 8 5 9 1 6 . 5 0 0 1 . 7 2 4 2 0 . 0 7 0 5 8 3 . 0 0 0 0 0 - 0 . 0 8 6 9

POL . W3_2 4 1_3 0_9 ; 1

9 . 0 0 0

S xt r P xt r ------- - - -----0 . 52 3 9 0 0 . 3 7 3 6 0 0 . 5 1 1 0 0 0 . 37 8 8 0 0 . 4 9 9 8 0 0 . 3 8 8 9 0 0 . 4 8 4 8 0 0 . 3 9 6 7 0 0 . 4 7 5 5 0 0 . 4 0 1 7 0 0 . 4 6 5 0 0 0 . 4 0 8 6 0 0 . 4 5 3 7 0 0 . 4 1 7 0 0 0 . 4 4 4 4 0 0 . 42 2 9 0 0 . 4 3 1 2 0 0 . 42 5 6 0 0 . 42 6 4 0 0 . 4 3 3 0 0 0 . 4 1 4 4 0 0 . 4 4 1 5 0 0 . 4 0 5 8 0 0 . 4 4 5 6 0 0 . 4 0 0 3 0 . 4 4 8 3 0 . 3 8 7 7 0 . 4 5 4 7 0 . 3 8 12 0 . 4 6 1 7 0 . 3 7 5 5 0 . 4 6 7 3 0 . 3 6 3 0 0 . 4 7 0 3 0 . 3 5 7 0 0 . 4 7 2 2 0 . 3 4 8 8 0 . 4 7 8 4 0 . 3 3 7 6 0 . 4 8 5 8 0 . 3 32 4 0 . 4 8 9 9 0 . 32 2 2 0 . 4 92 9 0 . 3 1 1 2 0 . 4 9 4 8 0 . 3 0 3 9 0 . 4 9 9 9 0 . 2 8 8 0 0 . 5 0 6 0 0 . 2 7 9 5 0 . 5 1 0 7 0 . 2 6 5 8 0 . 5 1 4 0 0 . 2 5 4 6 0 . 5 1 6 8 0 . 2 4 0 3 0 . 5 1 8 4 0 . 2 2 3 9 0 . 52 3 5 0 . 2 1 2 6 0 . 52 92 0 . 1 9 57 0 . 5 3 4 4 0 . 1 8 4 4 0 . 5 3 7 4 0 . 1 6 4 1 0 . 5 3 9 6 0 . 1 4 7 6 0 . 5 4 1 2 0 . 1 3 4 7 0 . 5 4 4 7 0 . 1 2 4 1 0 . 5 5 0 2 0 . 1 0 6 7 0 . 5 555 0 . 1 0 1 1 0 . 5 5 8 5 0 . 0 9 2 0 0 . 5 6 0 9 0 . 0 8 4 3 0 . 5 6 2 8 0 . 0 8 0 5 0 . 5 6 4 2 0 . 0 7 4 5 0 . 5 6 5 6 0 . 0 6 5 5 0 . 5 7 0 8 0 . 0 6 3 6 0 . 5 7 62 0 . 0 6 0 7 0 . 5 7 9 4

FFA TN 1 9 9 0 - 1 5 6 9 POL . W3_2 4 1_30_TU1 ; 2

XFOI L Version 5 . 0

Calculated pola r for : FFA-W3-2 4 1

1 Reynolds number fixed

xt rf = 0 . 0 1 0 ( suct ion) 0 . 1 0 0 (pre s sure ) Mach = 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xt r -- -- - - - -------- --------- --------- -------- ------- -------- 5 . 0 0 0 0 0 - 0 . 3 5 7 9 0 0 . 0 1 5 7 7 3 . 0 0 0 0 0 - 0 . 0 5 3 7 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 4 . 5 0 0 0 0 - 0 . 2 8 7 5 0 0 . 0 1 5 1 0 3 . 0 0 0 0 0 - 0 . 0 5 8 1 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 4 . 0 0 0 0 0 - 0 . 2 1 6 6 0 0 . 0 1 4 5 4 3 . 0 0 0 0 0 - 0 . 0 62 3 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 5 0 0 0 0 - 0 . 1 4 5 7 0 0 . 0 1 4 0 6 3 . 0 0 0 0 0 - 0 . 0 6 6 3 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 0 0 0 0 0 - 0 . 0 7 5 0 0 0 . 0 1 3 6 6 3 . 0 0 0 0 0 - 0 . 0 7 0 1 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 2 . 5 0 0 0 0 - 0 . 0 0 4 9 0 0 . 0 1 3 3 4 3 . 0 0 0 0 0 - 0 . 0 7 3 7 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 2 . 0 0 0 0 0 0 . 0 6 3 5 0 0 . 0 1 3 1 6 3 . 0 0 0 0 0 - 0 . 0 7 6 6 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 5 0 0 0 0 0 . 1 3 0 7 0 0 . 0 1 3 0 7 3 . 0 0 0 0 0 - 0 . 0 7 9 1 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 0 0 0 0 0 0 . 1 9 7 4 0 0 . 0 1 3 02 3 . 0 0 0 0 0 - 0 . 0 8 1 5 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 0 . 5 0 0 0 0 0 . 2 6 3 5 0 0 . 0 1 3 0 0 3 . 0 0 0 0 0 - 0 . 0 8 3 6 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0

0 . 0 0 0 0 . 3 2 9 1 0 . 0 1 3 0 2 3 . 0 0 0 0 0 - 0 . 0 8 5 7 0 . 0 1 0 0 0 . 1 0 0 0 0 . 5 0 0 0 . 3 9 4 2 0 . 0 1 3 0 7 3 . 0 0 0 0 0 - 0 . 0 8 7 6 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 . 4 5 8 8 0 . 0 1 3 1 6 3 . 0 0 0 0 0 - 0 . 0 8 9 3 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 5 2 2 8 0 . 0 1 3 2 7 3 . 0 0 0 0 0 - 0 . 0 9 1 0 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 5 8 6 3 0 . 0 1 3 4 1 3 . 0 0 0 0 0 - 0 . 0 92 5 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 6 4 92 0 . 0 1 3 5 9 3 . 0 0 0 0 0 - 0 . 0 9 3 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 7 1 1 5 0 . 0 1 3 7 9 3 . 0 0 0 0 0 - 0 . 0 9 5 1 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 7 7 32 0 . 0 1 4 0 3 3 . 0 0 0 0 0 - 0 . 0 9 63 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 8 3 4 1 0 . 0 1 4 3 0 3 . 0 0 0 0 0 - 0 . 0 9 7 3 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 8 9 4 1 0 . 0 1 4 6 1 3 . 0 0 0 0 0 - 0 . 0 9 8 1 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 9 5 3 3 0 . 0 1 4 9 5 3 . 0 0 0 0 0 - 0 . 0 9 8 8 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 1 . 0 1 1 5 0 . 0 1 5 3 4 3 . 0 0 0 0 0 - 0 . 0 9 9 3 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 1 . 0 6 8 5 0 . 0 1 5 7 7 3 . 0 0 0 0 0 - 0 . 0 9 9 6 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 1 2 4 1 0 . 0 1 62 5 3 . 0 0 0 0 0 - 0 . 0 9 9 7 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 1 7 8 2 0 . 0 1 6 7 9 3 . 0 0 0 0 0 - 0 . 0 9 9 5 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 2 3 0 3 0 . 0 1 7 3 9 3 . 0 0 0 0 0 - 0 . 0 9 9 1 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 2 7 9 8 0 . 0 1 8 0 7 3 . 0 0 0 0 0 - 0 . 0 9 8 3 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 3 2 5 0 0 . 0 1 8 8 6 3 . 0 0 0 0 0 - 0 . 0 9 6 8 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 3 4 5 7 0 . 0 1 9 9 0 3 . 0 0 0 0 0 - 0 . 0 9 1 4 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 37 5 4 0 . 02 1 4 0 3 . 0 0 0 0 0 - 0 . 0 8 8 5 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 4 0 0 0 0 . 0 2 3 4 2 3 . 0 0 0 0 0 - 0 . 0 8 5 9 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 4 2 1 7 0 . 02 6 0 4 3 . 0 0 0 0 0 - 0 . 0 8 4 0 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 4 3 9 7 0 . 0 2 9 3 4 3 . 0 0 0 0 0 - 0 . 0 8 2 6 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 4 5 6 4 0 . 0 3 3 2 1 3 . 0 0 0 0 0 - 0 . 0 8 1 9 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 4 7 1 3 0 . 0 3 7 6 7 3 . 0 0 0 0 0 - 0 . 0 8 1 6 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 4 8 32 0 . 0 4 2 7 1 3 . 0 0 0 0 0 - 0 . 0 8 1 8 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 4 9 4 3 0 . 0 4 8 1 0 3 . 0 0 0 0 0 - 0 . 0 8 2 1 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 5 0 4 0 0 . 0 5 3 9 4 3 . 0 0 0 0 0 - 0 . 0 8 2 7 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 5 1 1 3 0 . 0 6 0 3 5 3 . 0 0 0 0 0 - 0 . 0 8 3 7 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 5 1 7 0 0 . 0 6 7 0 4 3 . 0 0 0 0 0 - 0 . 0 8 4 7 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 5 2 1 1 0 . 0 7 4 1 1 3 . 0 0 0 0 0 - 0 . 0 8 5 9 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 5 0 0 1 . 52 4 5 0 . 0 8 1 4 9 3 . 0 0 0 0 0 - 0 . 0 8 7 2 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 0 0 0 1 . 5 2 7 8 0 . 0 8 9 0 4 3 . 0 0 0 0 0 - 0 . 0 8 8 8 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 5 0 0 1 . 5 3 0 4 0 . 0 9 6 8 7 3 . 0 0 0 0 0 - 0 . 0 9 0 5 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 7 0

XFOIL Ve rs ion 5 . 0

Calculated polar for : FFA-W3-2 7 0

1 Reynolds number fixed

xt rf = 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pres sure ) Mach = 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it

a lpha CL CD Re ( CL) CM - - - - - -- -------- --------- -------- - ------ - -

0 . 0 0 0 0 . 3 4 3 9 0 . 0 1 0 4 9 1 . 0 0 0 0 0 - 0 . 0 9 3 0 0 . 5 0 0 0 . 4 0 9 8 0 . 0 1 0 6 0 1. 0 0 0 0 0 - 0 . 0 9 47 1 . 0 0 0 0 . 4 7 4 9 0 . 0 1 0 7 5 1 . 0 0 0 0 0 - 0 . 0 9 6 3 1 . 5 0 0 0 . 5 4 1 5 0 . 0 1 0 8 1 1 . 0 0 0 0 0 - 0 . 0 9 8 3 2 . 0 0 0 0 . 6 0 7 0 0 . 0 1 0 9 1 1 . 0 0 0 0 0 - 0 . 0 9 9 9 2 . 5 0 0 0 . 6 7 1 4 0 . 0 1 1 0 9 1 . 0 0 0 0 0 - 0 . 1 0 1 3 3 . 0 0 0 0 . 7 3 4 8 0 . 0 1 1 33 1 . 0 0 0 0 0 - 0 . 1 0 2 5 3 . 50 0 0 . 7 9 8 3 0 . 0 1 1 5 4 1 . 0 0 0 0 0 - 0 . 1 0 37 4 . 0 0 0 0 . 8 6 2 1 0 . 0 1 1 7 2 1 . 0 0 0 0 0 - 0 . 1 0 5 1 4 . 5 0 0 0 . 92 4 9 0 . 0 1 1 9 6 1 . 0 0 0 0 0 - 0 . 1 0 62 5 . 0 0 0 0 . 9 8 6 7 0 . 0 12 2 4 1 . 0 0 0 0 0 - 0 . 1 0 7 1 5 . 5 0 0 1 . 0 4 7 5 0 . 0 1 2 5 8 1 . 0 0 0 0 0 - 0 . 1 0 7 8 6 . 0 0 0 1 . 1 0 7 3 0 . 0 1 2 9 5 1 . 0 0 0 0 0 - 0 . 1 0 8 3 6 . 5 0 0 1 . 1 6 6 5 0 . 0 1 3 3 3 1 . 0 0 0 0 0 - 0 . 1 0 8 7 7 . 0 0 0 1 . 2 2 5 6 0 . 0 1 3 6 9 1 . 0 0 0 0 0 - 0 . 1 0 92 7 . 5 0 0 1 . 2 8 2 3 0 . 0 1 4 1 5 1 . 0 0 0 0 0 - 0 . 1 0 9 3 8 . 0 0 0 1 . 3 3 7 5 0 . 0 1 4 6 6 1 . 0 0 0 0 0 - 0 . 1 0 9 1 8 . 5 0 0 1 . 3 9 0 5 0 . 0 1 525 1 . 0 0 0 0 0 - 0 . 1 0 8 5 9 . 0 0 0 1 . 4 4 0 2 0 . 0 1 5 9 3 1 . 0 0 0 0 0 - 0 . 1 0 7 5 9 . 5 0 0 1 . 4 8 5 6 0 . 0 1 6 6 8 1 . 0 0 0 0 0 - 0 . 1 0 5 7

1 0 . 0 0 0 1 . 5 1 4 3 0 . 0 1 7 5 9 1 . 0 0 0 0 0 - 0 . 1 0 1 4 1 0 . 5 0 0 1 . 5 4 4 0 0 . 0 1 8 9 9 1 . 0 0 0 0 0 - 0 . 0 9 8 0 1 1 . 0 0 0 1 . 5 6 9 9 0 . 02 0 8 0 1 . 0 0 0 0 0 - 0 . 0 9 4 8 1 1 . 5 0 0 1 . 5 9 1 6 0 . 0 2 3 1 7 1 . 0 0 0 0 0 - 0 . 0 9 2 1 1 2 . 0 0 0 1 . 6 0 7 1 0 . 0 2 6 3 1 1 . 0 0 0 0 0 - 0 . 0 8 9 6 1 2 . 5 0 0 1 . 6 1 9 9 0 . 0 3 0 0 7 1 . 0 0 0 0 0 - 0 . 0 8 7 7 1 3 . 0 0 0 1 . 6 3 2 8 0 . 0 3 4 3 1 1 . 0 0 0 0 0 - 0 . 0 8 6 7 1 3 . 5 0 0 1 . 6 4 1 6 0 . 0 3 92 1 1 . 0 0 0 0 0 - 0 . 0 8 6 0 1 4 . 0 0 0 1 . 6 4 4 6 0 . 0 4 4 9 6 1 . 0 0 0 0 0 - 0 . 0 8 5 5

POL . W3_2 7 0_1 0_9 ; 2

9 . 0 0 0

S xt r P xt r - - ----- -- -- - - -0 . 4 2 6 5 0 . 4 5 9 6 0 . 4 1 55 0 . 4 6 3 0 0 . 4 0 7 9 0 . 4 6 62 0 . 3 9 4 9 0 . 4 7 3 5 0 . 3 8 9 5 0 . 4 7 92 0 . 3 7 9 7 0 . 4 8 2 9 0 . 3 6 9 1 0 . 4 8 6 4 0 . 3 6 3 6 0 . 4 8 9 1 0 . 3 5 3 1 0 . 4 9 5 1 0 . 3 4 4 1 0 . 5 0 1 1 0 . 3 3 8 5 0 . 5 0 52 0 . 32 7 7 0 . 5 0 8 3 0 . 3 1 9 6 0 . 5 1 1 1 0 . 3 1 4 1 0 . 5 1 3 4 0 . 3 0 3 0 0 . 52 1 6 0 . 2 9 5 4 0 . 52 5 9 0 . 2 8 8 6 0 . 52 9 2 0 . 2 7 8 7 0 . 5 3 2 1 0 . 2 7 0 4 0 . 5 3 4 7 0 . 2 6 4 4 0 . 5 3 7 4 0 . 2 553 0 . 5 4 4 8 0 . 2 4 6 7 0 . 5 4 8 8 0 . 2 4 1 0 0 . 5 5 1 8 0 . 2 3 1 5 0 . 5 5 4 5 0 . 2 2 2 8 0 . 5 5 6 9 0 . 2 1 6 5 0 . 5 5 9 2 0 . 2 0 5 8 0 . 5 6 3 9 0 . 1 9 9 6 0 . 5 6 9 0 0 . 1 9 3 0 0 . 5 7 2 2

FFA TN 1 9 9 0 - 1 5 7 1

XFOI L Ve rs ion 5 . 0

Calculated polar for : FFA-W3-2 7 0

1 Reynolds number fixed

xtrf = 0 . 0 1 0 ( suct ion ) 0 . 1 0 0 (pre s sure ) Mach =

a lpha - - - -- - -

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 50 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 50 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0

0 . 1 5 0

CL - - --- - - -

0 . 2 1 5 2 0 . 2 8 5 7 0 . 3 5 5 8 0 . 42 5 5 0 . 4 9 4 2 0 . 5 6 1 8 0 . 6 2 7 7 0 . 6 9 1 3 0 . 7 5 2 1 0 . 8 1 0 4 0 . 8 6 6 0 0 . 9 1 8 0 0 . 9 5 3 9 0 . 9 8 4 4 1 . 0 1 9 6 1 . 0 5 0 2 1 . 0 7 8 1 1 . 1 0 2 9 1 . 1 2 6 0 1 . 1 4 7 8 1 . 1 6 6 9 1 . 1 8 4 2 1 . 2 0 0 3 1 . 2 1 4 7 1 . 2 2 7 2 1 . 23 7 8 1 . 2 4 7 3 1 . 2 5 6 0 1 . 2 6 4 3

Re = 1 . 0 0 0 e 6 Ncr it

CD Re (CL) CM ------ - - - - - - ------ --------

0 . 0 1 9 5 6 1 . 0 0 0 0 0 - 0 . 0 5 8 5 0 . 0 1 9 1 9 1 . 0 0 0 0 0 - 0 . 0 62 9 0 . 0 1 8 9 4 1 . 0 0 0 0 0 - 0 . 0 6 7 0 0 . 0 1 8 7 6 1 . 0 0 0 0 0 - 0 . 0 7 0 9 0 . 0 1 8 6 8 1 . 0 0 0 0 0 - 0 . 0 7 4 5 0 . 0 1 8 6 8 1 . 0 0 0 0 0 - 0 . 0 7 7 7 0 . 0 1 8 7 7 1 . 0 0 0 0 0 - 0 . 0 8 0 6 0 . 0 1 8 9 6 1 . 0 0 0 0 0 - 0 . 0 8 2 9 0 . 0 1 9 2 8 1 . 0 0 0 0 0 - 0 . 0 8 4 6 0 . 0 1 9 6 8 1 . 0 0 0 0 0 - 0 . 0 8 5 7 0 . 0 2 0 1 8 1 . 0 0 0 0 0 - 0 . 0 8 6 4 0 . 0 2 0 7 8 1 . 0 0 0 0 0 - 0 . 0 8 6 6 0 . 0 2 1 52 1 . 0 0 0 0 0 - 0 . 0 8 4 0 0 . 0 2 2 6 7 1 . 0 0 0 0 0 - 0 . 0 8 1 2 0 . 0 2 4 2 1 1 . 0 0 0 0 0 - 0 . 0 8 0 0 0 . 0 2 6 1 9 1 . 0 0 0 0 0 - 0 . 0 7 8 9 0 . 0 2 8 6 9 1 . 0 0 0 0 0 - 0 . 0 7 8 3 0 . 0 3 1 6 9 1 . 0 0 0 0 0 - 0 . 0 7 7 9 0 . 0 3 5 1 8 1 . 0 0 0 0 0 - 0 . 0 7 7 9 0 . 0 3 9 0 8 1 . 0 0 0 0 0 - 0 . 0 7 8 2 0 . 0 4 3 4 7 1 . 0 0 0 0 0 - 0 . 0 7 8 8 0 . 0 4 82 7 1 . 0 0 0 0 0 - 0 . 0 7 9 5 0 . 0 5 3 4 1 1 . 0 0 0 0 0 - 0 . 0 8 0 4 0 . 0 5 8 9 5 1 . 0 0 0 0 0 - 0 . 0 8 1 4 0 . 0 6 4 8 7 1 . 0 0 0 0 0 - 0 . 0 8 2 6 0 . 0 7 1 1 5 1 . 0 0 0 0 0 - 0 . 0 8 3 9 0 . 0 7 7 7 9 1 . 0 0 0 0 0 - 0 . 0 8 5 3 0 . 0 8 4 7 6 1 . 0 0 0 0 0 - 0 . 0 8 7 0 0 . 0 9 1 9 1 1 . 0 0 0 0 0 - 0 . 0 8 8 7

POL . W3_2 7 0_1 0_TU1 ; 2

9 . 0 0 0

S xt r P xt r ------- -------0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 7 2

XFOIL Ve rs ion 5 . 0

Calculated polar for : FFA-W3- 2 7 0

1 Reyno lds number f ixed

xt r f = 1 . 0 0 0 ( suct ion) 1 . 0 0 0 (pres sure ) Mach =

a lpha ------ -- 6 . 0 0 0 0 0 -5 . 5 0 0 0 0 - 5 . 0 0 0 0 0 - 4 . 5 0 0 0 0 - 4 . 0 0 0 0 0 - 3 . 50 0 0 0 - 3 . 0 0 0 0 0 -2 . 5 0 0 0 0 -2 . 0 0 0 0 0 - 1 . 5 0 0 0 0 - 1 . 0 0 0 0 0 - 0 . 5 0 0 0 0

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0 1 5 . 5 0 0 1 6 . 0 0 0 1 6 . 5 0 0

0 . 1 5 0

CL --------

- 0 . 4 6 5 1 0 - 0 . 3 9 0 7 0 - 0 . 3 1 8 9 0 - 0 . 2 4 8 5 0 - 0 . 1 7 9 8 0 - 0 . 1 0 9 9 0 - 0 . 0 4 1 3 0

0 . 0 2 6 8 0 0 . 0 9 3 9 0 0 . 1 62 0 0 0 . 2 2 9 3 0 0 . 2 9 5 9 0

0 . 3 6 2 1 0 . 4 2 8 5 0 . 4 9 4 8 0 . 5 6 0 5 0 . 6 2 5 7 0 . 6 9 0 4 0 . 7 5 5 5 0 . 8 2 0 0 0 . 8 8 3 9 0 . 9 4 7 4 1 . 0 1 0 0 1 . 0 7 2 7 1 . 1 3 4 8 1 . 1 9 5 9 1 . 2 5 6 4 1 . 3 1 5 5 1 . 3 7 3 5 1 . 4 3 1 0 1 . 4 8 6 8 1 . 5 3 8 6 1 . 5 8 9 1 1 . 6322 1 . 6 5 9 4 1 . 6 8 8 1 1 . 7 0 7 6 1 . 7 2 5 2 1 . 7 3 1 5 1 . 7 3 5 3 1 . 7 4 7 0 1 . 7 4 3 1 1 . 7 3 9 9 1 . 7 4 0 2 1 . 7 32 9 1 . 7 2 3 2

Re = 2 . 0 0 0 e 6 Ncr it

CD Re (CL) CM --------- --------- --------

0 . 0 1 0 0 2 2 . 0 0 0 0 0 - 0 . 0 6 6 2 0 0 . 0 0 9 5 4 2 . 0 0 0 0 0 - 0 . 0 7 0 7 0 0 . 0 0 9 2 5 2 . 0 0 0 0 0 - 0 . 0 7 4 2 0 0 . 0 0 9 0 5 2 . 0 0 0 0 0 - 0 . 0 7 7 2 0 0 . 0 0 8 9 6 2 . 0 0 0 0 0 - 0 . 0 7 9 7 0 0 . 0 0 8 8 0 2 . 0 0 0 0 0 - 0 . 0 8 2 5 0 0 . 0 0 8 7 1 2 . 0 0 0 0 0 - 0 . 0 8 5 0 0 0 . 0 0 8 6 6 2 . 0 0 0 0 0 - 0 . 0 8 7 3 0 0 . 0 0 8 6 8 2 . 0 0 0 0 0 - 0 . 0 8 9 3 0 0 . 0 0 8 6 3 2 . 0 0 0 0 0 - 0 . 0 9 1 6 0 0 . 0 0 8 6 3 2 . 0 0 0 0 0 - 0 . 0 9 3 6 0 0 . 0 0 8 6 8 2 . 0 0 0 0 0 - 0 . 0 9 5 5 0

0 . 0 0 8 7 5 2 . 0 0 0 0 0 - 0 . 0 9 7 3 0 . 0 0 8 7 9 2 . 0 0 0 0 0 - 0 . 0 9 9 1 0 . 0 0 8 8 6 2 . 0 0 0 0 0 - 0 . 1 0 0 9 0 . 0 0 8 9 6 2 . 0 0 0 0 0 - 0 . 1 0 2 5 0 . 0 0 9 0 8 2 . 0 0 0 0 0 - 0 . 1 0 4 0 0 . 0 0 92 4 2 . 0 0 0 0 0 - 0 . 1 0 5 4 0 . 0 0 9 37 2 . 0 0 0 0 0 - 0 . 1 0 6 9 0 . 0 0 9 53 2 . 0 0 0 0 0 - 0 . 1 0 8 3 0 . 0 0 9 7 2 2 . 0 0 0 0 0 - 0 . 1 0 9 5 0 . 0 0 9 9 3 2 . 0 0 0 0 0 - 0 . 1 1 0 6 0 . 0 1 0 1 9 2 . 0 0 0 0 0 - 0 . 1 1 1 6 0 . 0 1 0 4 3 2 . 0 0 0 0 0 - 0 . 1 1 2 6 0 . 0 1 0 7 0 2 . 0 0 0 0 0 - 0 . 1 1 3 5 0 . 0 1 1 0 0 2 . 0 0 0 0 0 - 0 . 1 1 4 2 0 . 0 1 1 3 3 2 . 0 0 0 0 0 - 0 . 1 1 4 7 0 . 0 1 1 7 2 2 . 0 0 0 0 0 - 0 . 1 1 5 0 0 . 0 1 2 1 5 2 . 0 0 0 0 0 - 0 . 1 1 52 0 . 0 1 2 5 9 2 . 0 0 0 0 0 - 0 . 1 1 5 3 0 . 0 1 3 0 7 2 . 0 0 0 0 0 - 0 . 1 1 5 1 0 . 0 1 3 7 3 2 . 0 0 0 0 0 - 0 . 1 1 4 3 0 . 0 1 4 3 6 2 . 0 0 0 0 0 - 0 . 1 1 32 0 . 0 1 5 2 1 2 . 0 0 0 0 0 - 0 . 1 1 1 1 0 . 0 1 6 1 9 2 . 0 0 0 0 0 - 0 . 1 0 62 0 . 0 1 7 5 2 2 . 0 0 0 0 0 - 0 . 1 0 2 4 0 . 0 1 9 5 5 2 . 0 0 0 0 0 - 0 . 0 9 8 3 0 . 0 2 2 1 1 2 . 0 0 0 0 0 - 0 . 0 9 5 1 0 . 0 2 5 8 8 2 . 0 0 0 0 0 - 0 . 0 92 0 0 . 0 3 0 4 8 2 . 0 0 0 0 0 - 0 . 0 8 9 9 0 . 0 3 4 8 3 2 . 0 0 0 0 0 - 0 . 0 8 8 7 0 . 0 4 1 0 0 2 . 0 0 0 0 0 - 0 . 0 8 7 6 0 . 0 4 7 5 8 2 . 0 0 0 0 0 - 0 . 0 8 7 3 0 . 0 5 4 1 8 2 . 0 0 0 0 0 - 0 . 0 8 7 4 0 . 0 6 1 8 3 2 . 0 0 0 0 0 - 0 . 0 8 7 7 0 . 0 7 0 0 0 2 . 0 0 0 0 0 - 0 . 0 8 8 4

POL . W3_2 7 0_2 0_9 ; 3

9 . 0 0 0

s xt r P xt r ------- --- - ---0 . 5 3 3 8 0 0 . 37 0 6 0 0 . 5 1 6 0 0 0 . 3 7 8 2 0 0 . 5 0 7 1 0 0 . 3 8 7 1 0 0 . 4 9 1 8 0 0 . 3 9 2 3 0 0 . 4 8 1 9 0 0 . 3 9 6 1 0 0 . 4 6 7 3 0 0 . 4 0 4 8 0 0 . 4 6 0 1 0 0 . 4 1 1 9 0 0 . 4 4 6 3 0 0 . 4 1 6 3 0 0 . 4 3 7 4 0 0 . 4 1 9 6 0 0 . 4 2 6 0 0 0 . 4 2 7 5 0 0 . 4 1 6 7 0 0 . 4 3 4 4 0 0 . 4 0 7 4 0 0 . 4 3 8 8 0 0 . 3 9 4 6 0 . 4 42 2 0 . 3 8 9 8 0 . 4 4 7 2 0 . 3 8 12 0 . 4 5 4 5 0 . 3 6 9 2 0 . 4 6 0 4 0 . 3 6 3 9 0 . 4 6 3 7 0 . 3 5 4 6 0 . 4 6 6 1 0 . 3 4 5 1 0 . 4 7 1 7 0 . 3 3 8 8 0 . 4 7 9 4 0 . 32 9 1 0 . 4 8 3 6 0 . 32 0 6 0 . 4 8 6 8 0 . 3 1 4 2 0 . 4 8 9 1 0 . 3 0 4 4 0 . 4 9 4 5 0 . 2 9 5 5 0 . 5 0 1 0 0 . 2 9 0 0 0 . 5 0 5 6 0 . 2 8 0 5 0 . 5 0 8 9 0 . 2 7 1 5 0 . 5 1 1 6 0 . 2 6 5 9 0 . 5 1 3 5 0 . 2 527 0 . 52 0 7 0 . 2 4 7 1 0 . 52 6 1 0 . 2 3 7 4 0 . 52 9 9 0 . 2 2 6 1 0 . 5 3 3 0 0 . 2 1 9 4 0 . 5 3 5 1 0 . 2 1 0 0 0 . 5 3 6 8 0 . 2 0 1 6 0 . 5 4 3 4 0 . 1 9 6 3 0 . 5 4 8 4 0 . 1 8 6 6 0 . 5 52 0 0 . 1 7 6 6 0 . 5 5 4 9 0 . 1 6 92 0 . 5 5 6 9 0 . 1 5 7 6 0 . 5 5 8 7 0 . 1 5 3 2 0 . 5 6 0 0 0 . 1 4 52 0 . 5 6 5 1 0 . 1 3 4 8 0 . 5 6 9 7 0 . 1 3 0 8 0 . 5 7 3 1 0 . 1 2 3 3 0 . 5 7 62

FFA TN 1 9 9 0 - 1 5 7 3

XFOIL Ve rs ion 5 . 0

Calculated pola r for : FFA-W3 - 2 7 0

1 Reynolds number fixed

xt r f • 1 . 0 0 0 ( suct ion) 1 . 0 0 0 (pre s sure ) Mach =

a lpha ---- - --

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 50 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0

0 . 1 5 0

CL --------

0 . 3 6 9 5 0 . 4 3 6 0 0 . 5 0 1 6 0 . 5 6 7 3 0 . 6 3 3 1 0 . 6 9 8 4 0 . 7 6 3 0 0 . 82 7 5 0 . 8 92 0 0 . 9 5 5 7 1 . 0 1 9 4 1 . 0 8 2 4 1 . 1 4 42 1 . 2 0 6 5 1 . 2 6 7 4 1 . 32 7 9 1 . 3 8 7 2 1 . 4 4 5 0 1 . 5 0 1 6 1 . 5 5 7 0 1 . 6 0 8 0 1 . 6 5 8 0 1 . 7 0 0 2 1 . 7 2 6 6 1 . 7 42 6 1 . 7 5 8 4 1 . 7 7 42 1 . 7 7 7 1 1 . 7 8 3 0

Re = 3 . 0 0 0 e 6 Ncr it

CD Re (CL) CM --------- -- - - ----- --------

0 . 0 0 8 0 2 3 . 0 0 0 0 0 - 0 . 0 9 9 0 0 . 0 0 8 0 5 3 . 0 0 0 0 0 - 0 . 1 0 0 8 0 . 0 0 8 1 6 3 . 0 0 0 0 0 - 0 . 1 0 2 4 0 . 0 0 8 2 6 3 . 0 0 0 0 0 - 0 . 1 0 4 0 0 . 0 0 8 3 5 3 . 0 0 0 0 0 - 0 . 1 0 5 6 0 . 0 0 8 4 5 3 . 0 0 0 0 0 - 0 . 1 0 7 1 0 . 0 0 8 62 3 . 0 0 0 0 0 - 0 . 1 0 8 5 0 . 0 0 8 7 8 3 . 0 0 0 0 0 - 0 . 1 0 9 7 0 . 0 0 8 9 3 3 . 0 0 0 0 0 - 0 . 1 1 1 1 0 . 0 0 9 1 5 3 . 0 0 0 0 0 - 0 . 1 1 2 2 0 . 0 0 9 3 4 3 . 0 0 0 0 0 - 0 . 1 1 3 4 0 . 0 0 9 5 6 3 . 0 0 0 0 0 - 0 . 1 1 4 4 0 . 0 0 9 8 7 3 . 0 0 0 0 0 - 0 . 1 1 52 0 . 0 1 0 1 2 3 . 0 0 0 0 0 - 0 . 1 1 6 0 0 . 0 1 0 4 5 3 . 0 0 0 0 0 - 0 . 1 1 6 7 0 . 0 1 0 7 8 3 . 0 0 0 0 0 - 0 . 1 1 7 2 0 . 0 1 1 1 6 3 . 0 0 0 0 0 - 0 . 1 1 7 6 0 . 0 1 1 6 0 3 . 0 0 0 0 0 - 0 . 1 1 7 6 0 . 0 1 2 0 8 3 . 0 0 0 0 0 - 0 . 1 1 7 5 0 . 0 1 2 5 8 3 . 0 0 0 0 0 - 0 . 1 1 7 2 0 . 0 1 3 2 8 3 . 0 0 0 0 0 - 0 . 1 1 6 3 0 . 0 1 3 9 0 3 . 0 0 0 0 0 - 0 . 1 1 5 1 0 . 0 1 4 7 8 3 . 0 0 0 0 0 - 0 . 1 1 2 8 0 . 0 1 5 7 5 3 . 0 0 0 0 0 - 0 . 1 0 7 7 0 . 0 1 7 62 3 . 0 0 0 0 0 - 0 . 1 0 2 3 0 . 0 1 9 9 3 3 . 0 0 0 0 0 - 0 . 0 9 8 1 0 . 0 2 2 7 3 3 . 0 0 0 0 0 - 0 . 0 9 5 0 0 . 0 2 6 9 1 3 . 0 0 0 0 0 - 0 . 0 92 0 0 . 0 3 1 4 9 3 . 0 0 0 0 0 - 0 . 0 9 0 2

POL . W3_2 7 0_3 0_9 ; 2

9 . 0 0 0

S xt r P xt r ------- - - -----0 . 3 8 3 9 0 . 4 3 5 1 0 . 3 7 2 1 0 . 4 4 0 1 0 . 3 6 5 7 0 . 4 4 2 6 0 . 3 5 7 4 0 . 4 4 7 5 0 . 3 4 6 0 0 . 4 5 6 1 0 . 3 4 22 0 . 4 6 0 9 0 . 3 3 2 0 0 . 4 6 42 0 . 32 1 5 0 . 4 6 6 3 0 . 3 1 7 6 0 . 4 7 3 0 0 . 3 0 7 2 0 . 4 7 9 4 0 . 2 9 7 3 0 . 4 8 4 0 0 . 2 9 35 0 . 4 8 7 2 0 . 2 8 3 2 0 . 4 8 9 6 0 . 2 7 3 4 0 . 4 9 4 3 0 . 2 6 7 9 0 . 5 0 0 7 0 . 2 5 9 1 0 . 5 0 5 8 0 . 2 4 8 4 0 . 5 0 9 8 0 . 2 4 3 0 0 . 5 1 2 0 0 . 2 2 9 0 0 . 5 1 3 6 0 . 2 2 3 3 0 . 52 0 1 0 . 2 1 1 0 0 . 52 5 8 0 . 2 0 1 8 0 . 5 3 0 6 0 . 1 9 55 0 . 5 3 3 4 0 . 1 8 5 4 0 . 5 3 5 3 0 . 1 7 5 6 0 . 5 3 6 7 0 . 1 6 6 6 0 . 5 4 1 7 0 . 1 5 6 7 0 . 5 4 6 9 0 . 1 5 1 9 0 . 5 5 1 7 0 . 1 4 2 6 0 . 5 5 4 5

F.FA TN 1 9 9 0 - 1 5 7 4 POL . W3_2 7 0_3 0_TU 1 ; 2

XFO IL Ve rs ion 5 . 0

Ca lculated polar for : FFA-W3 - 2 7 0

1 Reynolds numbe r fixed

xt r f = 0 . 0 1 0 ( suct ion ) 0 . 1 0 0 (pres sure ) Mach = 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xt r ------- -------- -------- - --------- -------- ------- -------- 6 . 0 0 0 0 0 - 0 . 5 0 9 0 0 0 . 0 2 4 9 9 3 . 0 0 0 0 0 - 0 . 0 2 7 2 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 5 . 5 0 0 0 0 - 0 . 4 6 0 3 0 0 . 0 2 3 4 9 3 . 0 0 0 0 0 - 0 . 0 2 9 5 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 5 . 0 0 0 0 0 - 0 . 4 0 6 8 0 0 . 0 2 2 0 5 3 . 0 0 0 0 0 - 0 . 0 32 7 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 4 . 5 0 0 0 0 - 0 . 3 4 9 0 0 0 . 0 2 0 9 3 3 . 0 0 0 0 0 - 0 . 0 3 5 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 4 . 0 0 0 0 0 - 0 . 2 8 6 9 0 0 . 0 1 97 6 3 . 0 0 0 0 0 - 0 . 0 4 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 5 0 0 0 0 - 0 . 2 2 1 9 0 0 . 0 1 8 9 0 3 . 0 0 0 0 0 - 0 . 0 4 4 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 0 0 0 0 0 - 0 . 1 5 4 1 0 0 . 0 1 8 1 1 3 . 0 0 0 0 0 - 0 . 0 4 8 4 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 2 . 5 0 0 0 0 - 0 . 0 8 3 8 0 0 . 0 1 7 3 7 3 . 0 0 0 0 0 - 0 . 0 5 3 1 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 -2 . 0 0 0 0 0 - 0 . 0 1 3 0 0 0 . 0 1 6 8 2 3 . 0 0 0 0 0 - 0 . 0 5 7 5 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 5 0 0 0 0 0 . 0 5 9 3 0 0 . 0 1 6 2 9 3 . 0 0 0 0 0 - 0 . 0 62 2 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 0 0 0 0 0 0 . 1 3 1 5 0 0 . 0 1 5 8 9 3 . 0 0 0 0 0 - 0 . 0 6 6 6 0 0 . 0 1 0 0 0 0 . 10 0 0 0 - 0 . 5 0 0 0 0 0 . 2 0 3 9 0 0 . 0 1 5 5 4 3 . 0 0 0 0 0 - 0 . 0 7 0 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0

0 . 0 0 0 0 . 2 7 5 8 0 . 0 1 5 2 8 3 . 0 0 0 0 0 - 0 . 0 7 5 0 0 . 0 1 0 0 0 . 1 0 0 0 0 . 5 0 0 0 . 3 4 7 3 0 . 0 1 5 0 6 3 . 0 0 0 0 0 - 0 . 0 7 8 9 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 . 4 1 7 7 0 . 0 1 4 9 3 3 . 0 0 0 0 0 - 0 . 0 8 2 4 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 4 8 7 0 0 . 0 1 4 8 6 3 . 0 0 0 0 0 - 0 . 0 8 5 6 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 5 5 4 3 0 . 0 1 4 9 0 3 . 0 0 0 0 0 - 0 . 0 8 8 2 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 6 1 9 9 0 . 0 1 5 0 2 3 . 0 0 0 0 0 - 0 . 0 9 0 4 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 8 4 4 0 . 0 1 5 1 9 3 . 0 0 0 0 0 - 0 . 0 9 2 3 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 7 4 7 7 0 . 0 1 5 4 0 3 . 0 0 0 0 0 - 0 . 0 9 3 9 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 8 0 9 9 0 . 0 1 5 6 6 3 . 0 0 0 0 0 - 0 . 0 9 53 0 . 0 1 0 0 0 . 1 0 0 0 4 . 50 0 0 . 8 7 0 7 0 . 0 1 5 9 7 3 . 0 0 0 0 0 - 0 . 0 9 65 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 9 3 0 1 0 . 0 1 6 3 3 3 . 0 0 0 0 0 - 0 . 0 9 7 3 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 9 8 7 8 0 . 0 1 6 7 4 3 . 0 0 0 0 0 - 0 . 0 9 7 9 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 1 . 0 4 3 7 0 . 0 1 7 2 1 3 . 0 0 0 0 0 - 0 . 0 9 8 2 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 0 9 7 1 0 . 0 1 7 7 6 3 . 0 0 0 0 0 - 0 . 0 9 8 1 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 1 4 7 2 0 . 0 1 8 3 9 3 . 0 0 0 0 0 - 0 . 0 9 7 5 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1 7 9 9 0 . 0 1 9 1 5 3 . 0 0 0 0 0 - 0 . 0 9 3 9 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 2 0 5 6 0 . 0 2 0 3 6 3 . 0 0 0 0 0 - 0 . 0 8 9 8 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 2 3 5 3 0 . 0 2 1 9 7 3 . 0 0 0 0 0 - 0 . 0 8 7 5 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 2 6 0 9 0 . 0 2 4 1 1 3 . 0 0 0 0 0 - 0 . 0 8 5 4 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 2 8 4 1 0 . 0 2 6 7 9 3 . 0 0 0 0 0 - 0 . 0 8 4 0 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 3 0 4 5 0 . 0 3 0 0 3 3 . 0 0 0 0 0 - 0 . 0 8 3 0 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 32 4 0 0 . 0 3 3 7 6 3 . 0 0 0 0 0 - 0 . 0 8 2 6 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 3 4 1 6 0 . 0 3 7 9 8 3 . 0 0 0 0 0 - 0 . 0 8 2 5 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 3 5 6 8 0 . 0 4 2 6 3 3 . 0 0 0 0 0 - 0 . 0 8 2 7 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 3 6 9 9 0 . 0 4 7 8 6 3 . 0 0 0 0 0 - 0 . 0 8 3 1 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 3 8 2 5 0 . 0 5 3 3 5 3 . 0 0 0 0 0 - 0 . 0 8 3 8 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1. 3 9 3 6 0 . 0 5 9 2 0 3 . 0 0 0 0 0 - 0 . 0 8 4 6 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 4 0 2 7 0 . 0 6 5 4 2 3 . 0 0 0 0 0 - 0 . 0 8 5 5 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 4 1 0 1 0 . 0 7 2 0 3 3 . 0 0 0 0 0 - 0 . 0 8 6 6 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 4 1 6 6 0 . 0 7 9 0 1 3 . 0 0 0 0 0 - 0 . 0 8 8 0 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 42 2 0 0 . 0 8 6 3 1 3 . 0 0 0 0 0 - 0 . 0 8 9 5 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 50 0 1 . 42 8 0 0 . 0 9 3 5 7 3 . 0 0 0 0 0 - 0 . 0 9 1 0 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 0 0 0 1 . 4 3 0 7 0 . 1 0 1 57 3 . 0 0 0 0 0 - 0 . 0 9 2 8 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 50 0 1 . 4 32 0 0 . 1 1 0 0 4 3 . 0 0 0 0 0 - 0 . 0 9 4 9 0 . 0 1 0 0 0 . 1 0 0 0 17 . 0 0 0 1 . 4 3 4 9 0 . 1 1 8 3 5 3 . 0 0 0 0 0 - 0 . 0 9 7 0 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 7 5 POL . W3_3 0 1_1 0_9 ; 2

XFOI L Version 5 . 0

Calculat ed pol a r for : FFA-W3-3 0 1

1 Reynolds numbe r fixed

xt r f = 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pre s su re ) Mach .. 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a l pha CL CD Re (CL) CM S xtr P xt r - - ----- -------- --------- --------- ------- - ------- --- - ---- 4 . 0 0 0 0 0 - 0 . 2 4 4 3 0 0 . 0 1 3 6 8 1 . 0 0 0 0 0 - 0 . 0 6 3 9 0 0 . 4 7 8 8 0 0 . 3 92 6 0 - 3 . 5 0 0 0 0 - 0 . 1 6 4 7 0 0 . 0 1 32 0 1 . 0 0 0 0 0 - 0 . 0 6 9 8 0 0 . 4 62 6 0 0 . 3 9 9 0 0 - 3 . 0 0 0 0 0 - 0 . 0 8 7 6 0 0 . 0 1 2 9 0 1 . 0 0 0 0 0 - 0 . 0 7 4 7 0 0 . 4 52 8 0 0 . 4 0 3 3 0 - 2 . 5 0 0 0 0 - 0 . 0 0 7 2 0 0 . 0 1 2 5 2 1 . 0 0 0 0 0 - 0 . 0 8 0 5 0 0 . 4 3 6 3 0 0 . 4 12 4 0 - 2 . 0 0 0 0 0 0 . 0 7 0 4 0 0 . 0 1 2 2 8 1 . 0 0 0 0 0 - 0 . 0 8 5 4 0 0 . 42 6 8 0 0 . 42 0 0 0 - 1 . 5 0 0 0 0 0 . 1 4 3 6 0 0 . 0 1 2 2 3 1 . 0 0 0 0 0 - 0 . 0 8 9 0 0 0 . 4 1 2 5 0 0 . 4 2 4 7 0 - 1 . 0 0 0 0 0 0 . 2 1 5 0 0 0 . 0 1 2 2 3 1 . 0 0 0 0 0 - 0 . 0 92 1 0 0 . 4 0 5 3 0 0 . 42 8 3 0 - 0 . 5 0 0 0 0 0 . 2 8 8 7 0 0 . 0 1 2 1 7 1 . 0 0 0 0 0 - 0 . 0 9 5 8 0 0 . 3 92 9 0 0 . 4 3 7 5 0

0 . 0 0 0 0 . 3 5 9 8 0 . 0 1 2 2 0 1 . 0 0 0 0 0 - 0 . 0 9 8 8 0 . 3 8 3 3 0 . 4 4 4 0 0 . 5 0 0 0 . 4 2 92 0 . 0 1 2 3 0 1. 0 0 0 0 0 - 0 . 1 0 1 3 0 . 3 7 5 1 0 . 4 4 8 2 1 . 5 0 0 0 . 5 6 7 1 0 . 0 12 5 3 1 . 0 0 0 0 0 - 0 . 1 0 62 0 . 3 5 7 6 0 . 4 5 9 0 2 . 0 0 0 0 . 6 3 5 7 0 . 0 12 6 6 1 . 0 0 0 0 0 - 0 . 1 0 8 5 0 . 3 5 0 2 0 . 4 6 6 0 2 . 5 0 0 0 . 7 02 1 0 . 0 12 9 0 1 . 0 0 0 0 0 - 0 . 1 1 0 4 0 . 3 3 7 4 0 . 4 7 0 3 3 . 0 0 0 0 . 7 6 8 0 0 . 0 1 3 1 1 1 . 0 0 0 0 0 - 0 . 1 1 2 0 0 . 3332 0 . 4 7 42 3 . 5 0 0 0 . 8 3 3 0 0 . 0 1 3 3 7 1 . 0 0 0 0 0 - 0 . 1 1 3 5 0 . 32 7 2 0 . 4 7 7 0 4 . 0 0 0 0 . 8 9 9 4 0 . 0 1 3 5 8 1 . 0 0 0 0 0 - 0 . 1 1 55 0 . 3 1 7 6 0 . 4 8 5 4 4 . 5 0 0 0 . 9 6 35 0 . 0 1 3 8 7 1 . 0 0 0 0 0 - 0 . 11 6 8 0 . 3 1 0 4 0 . 4 9 0 9 5 . 0 0 0 1 . 0 2 6 3 0 . 0 1 4 2 0 1 . 0 0 0 0 0 - 0 . 1 1 7 8 0 . 3 0 6 0 0 . 4 9 5 0 5 . 5 0 0 1 . 0 8 7 8 0 . 0 1 4 5 7 1 . 0 0 0 0 0 - 0 . 1 1 8 7 0 . 2 9 9 7 0 . 4 9 8 2 6 . 0 0 0 1 . 1 4 7 0 0 . 0 1 5 0 6 1 . 0 0 0 0 0 - o . 1 1 9 1 0 . 2 9 0 4 0 . 50 0 9 6 . 5 0 0 1 . 2 0 7 7 0 . 0 1 5 4 1 1 . 0 0 0 0 0 - 0 . 1 1 9 9 0 . 2 8 6 0 0 . 5 0 8 8 7 . 0 0 0 1 . 2 6 5 7 0 . 0 1 5 8 4 1 . 0 0 0 0 0 - 0 . 1 2 0 1 0 . 2 8 1 5 0 . 5 1 4 5 7 . 5 0 0 1 . 32 0 6 0 . 0 1 6 4 0 1 . 0 0 0 0 0 - 0 . 1 1 9 8 0 . 2 7 6 1 0 . 5 1 8 0 8 . 0 0 0 1 . 3 7 1 1 0 . 0 1 7 0 9 1 . 0 0 0 0 0 - 0 . 1 1 8 8 0 . 2 6 8 3 0 . 52 1 1 8 . 5 0 0 1 . 4 1 6 0 0 . 0 1 7 92 1 . 0 0 0 0 0 - 0 . 1 1 7 0 0 . 2 62 5 0 . 52 3 8 9 . 0 0 0 1 . 4 4 6 5 0 . 0 1 8 8 4 1 . 0 0 0 0 0 - 0 . 1 1 2 7 0 . 2 6 0 0 0 . 52 8 5 9 . 5 0 0 1 . 4 8 2 4 0 . 0 2 0 0 7 1 . 0 0 0 0 0 - 0 . 1 1 0 0 0 . 2 5 5 7 0 . 53 5 6

1 0 . 0 0 0 1 . 51 2 4 0 . 0 2 1 7 6 1 . 0 0 0 0 0 - 0 . 1 0 7 1 0 . 2 5 0 5 0 . 53 9 4 1 0 . 5 0 0 1 . 53 5 4 0 . 02 4 0 9 1 . 0 0 0 0 0 - 0 . 1 0 4 0 0 . 2 4 3 5 0 . 5 4 2 4 1 1 . 0 0 0 1 . 55 4 3 0 . 0 2 6 9 5 1 . 0 0 0 0 0 - 0 . 1 0 12 0 . 2 3 8 5 0 . 5 4 52 1 1 . 5 0 0 1 . 5 8 1 5 0 . 0 2 9 5 5 1 . 0 0 0 0 0 - 0 . 0 9 9 6 0 . 2 3 5 4 0 . 5 4 7 6 1 2 . 0 0 0 1 . 6 0 2 6 0 . 0 3 2 9 2 1 . 0 0 0 0 0 - 0 . 0 9 8 3 0 . 2 3 1 9 0 . 5 52 0 1 2 . 5 0 0 1 . 62 0 0 0 . 0 3 7 0 1 1 . 0 0 0 0 0 - 0 . 0 9 7 4 0 . 2 2 6 8 0 . 5 5 8 3 1 3 . 0 0 0 1 . 62 8 4 0 . 0 4 2 1 6 1 . 0 0 0 0 0 - 0 . 0 9 6 6 0 . 2 1 9 7 0 . 5 6 1 9 1 3 . 5 0 0 1 . 6 3 7 4 0 . 0 4 7 6 1 1 . 0 0 0 0 0 - 0 . 0 9 6 3 0 . 2 1 4 1 0 . 5 6 4 8 1 4 . 0 0 0 1 . 6 5 2 1 0 . 0 5 2 7 1 1 . 0 0 0 0 0 - 0 . 0 9 6 4 0 . 2 1 1 3 0 . 5 6 7 5 1 4 . 5 0 0 1 . 6 6 0 6 0 . 0 5 8 7 3 1 . 0 0 0 0 0 - 0 . 0 9 6 7 0 . 2 0 7 4 0 . 5 6 9 9 1 5 . 0 0 0 1 . 6 6 4 1 0 . 0 6 5 5 0 1 . 0 0 0 0 0 - 0 . 0 9 7 1 0 . 2 0 1 5 0 . 5 7 2 0 1 5 . 5 0 0 1 . 6 5 3 5 0 . 0 7 4 1 8 1 . 0 0 0 0 0 - 0 . 0 9 8 0 0 . 1 9 2 2 0 . 57 4 9 1 6 . 0 0 0 1 . 6 6 3 0 0 . 0 8 0 7 8 1 . 0 0 0 0 0 - 0 . 0 9 92 0 . 1 8 9 7 0 . 5 8 1 3 1 6 . 5 0 0 1 . 6 6 4 3 0 . 0 8 8 5 6 1 . 0 0 0 0 0 - 0 . 1 0 0 5 0 . 1 8 6 1 0 . 5 8 4 9

FFA TN 1 9 9 0 - 1 5 7 6 POL . W3_3 0 1_1 0_TU1 ; 2

XFOI L Ve rs ion 5 . 0

Calculated polar for : FFA-W3-3 0 1

1 Reynolds numbe r fixed

xt rf = 0 . 0 1 0 ( s uction ) 0 . 1 0 0 (pres sure ) Mach = 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it 9 . 0 0 0

alpha CL CD Re ( CL ) CM S xt r P xt r ------- -------- --------- -------- - -------- ------- -------

4 . 0 0 0 0 . 7 3 2 0 0 . 0 2 1 9 5 1 . 0 0 0 0 0 - 0 . 0 82 2 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 7 92 2 0 . 0 2 2 3 5 1 . 0 0 0 0 0 - 0 . 0 8 4 3 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 8 2 8 7 0 . 0 2 2 9 9 1 . 0 0 0 0 0 - 0 . 0 8 2 3 0 . 0 1 0 0 0 . 1 0 0 0 5 . 50 0 0 . 8 6 8 0 0 . 0 2 4 0 8 1 . 0 0 0 0 0 - 0 . 0 8 1 3 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 9 0 8 9 0 . 0 2 5 5 0 1 . 0 0 0 0 0 - 0 . 0 8 1 0 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 0 . 9 4 5 7 0 . 0 2 7 3 0 1 . 0 0 0 0 0 - 0 . 0 8 0 6 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 0 . 9 7 9 0 0 . 0 2 9 5 4 1 . 0 0 0 0 0 - 0 . 0 8 0 4 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 0 0 8 0 0 . 0 3 2 3 0 1 . 0 0 0 0 0 - 0 . 0 8 0 3 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 0 3 52 0 . 0 3 5 5 6 1 . 0 0 0 0 0 - 0 . 0 8 0 6 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 0 6 0 1 0 . 0 3 9 3 6 1 . 0 0 0 0 0 - 0 . 0 8 1 3 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 0 8 2 8 0 . 0 4 3 6 8 1 . 0 0 0 0 0 - 0 . 0 8 2 3 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 1 0 3 1 0 . 0 4 8 5 0 1 . 0 0 0 0 0 - 0 . 0 8 3 5 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 1 2 2 0 0 . 0 5 3 7 4 1 . 0 0 0 0 0 - 0 . 0 8 4 9 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 1 3 8 7 0 . 0 5 9 52 1 . 0 0 0 0 0 - 0 . 0 8 6 5 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 1 5 3 1 0 . 0 6 5 7 7 1 . 0 0 0 0 0 - 0 . 0 8 8 3 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 1 6 5 1 0 . 0 7 2 4 3 1 . 0 0 0 0 0 - 0 . 0 9 0 2 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 1 7 5 1 0 . 0 7 9 5 0 1 . 0 0 0 0 0 - 0 . 0 92 1 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 1 8 4 1 0 . 0 8 6 92 1 . 0 0 0 0 0 - 0 . 0 9 4 1 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 1 9 1 9 0 . 0 9 4 6 9 1 . 0 0 0 0 0 - 0 . 0 9 6 3 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 1 9 7 8 0 . 1 0 3 0 2 1 . 0 0 0 0 0 - 0 . 0 9 8 7 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 2 0 2 3 0 . 1 1 1 7 0 1 . 0 0 0 0 0 - 0 . 1 0 1 3 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 2 0 6 6 0 . 1 2 0 5 1 1 . 0 0 0 0 0 - 0 . 1 0 3 8 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 2 1 0 5 0 . 1 2 9 7 1 1 . 0 0 0 0 0 - 0 . 1 0 6 5 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 5 0 0 1 . 2 1 2 6 0 . 1 3 9 5 8 1 . 0 0 0 0 0 - 0 . 1 0 9 5 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 0 0 0 1 . 2 1 6 6 0 . 1 4 92 2 1 . 0 0 0 0 0 - 0 . 1 1 2 5 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 7 7

XFOIL Vers ion 5 . 0

Calculated polar for : FFA-W3-3 0 1

1 Reynolds number fixed

xt rf = 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pre s sure ) Mach =

a lpha -- ------ 6 . 0 0 0 0 0 - 5 . 5 0 0 0 0 - 5 . 0 0 0 0 0 - 4 . 5 0 0 0 0 - 4 . 0 0 0 0 0 - 3 . 5 0 0 0 0 - 3 . 0 0 0 0 0 - 2 . 5 0 0 0 0 - 2 . 0 0 0 0 0 - 1 . 5 0 0 0 0 - 1 . 0 0 0 0 0 - 0 . 5 0 0 0 0

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0 1 5 . 5 0 0 1 6 . 0 0 0 1 6 . 5 0 0 1 7 . 0 0 0

0 . 1 5 0

CL --------

- 0 . 5 1 5 6 0 - 0 . 4 3 5 3 0 - 0 . 3 5 3 5 0 - 0 . 2 7 3 1 0 - 0 . 1 9 3 8 0 - 0 . 1 1 5 3 0 - 0 . 0 3 9 5 0

0 . 0 32 9 0 0 . 1 0 6 1 0 0 . 1 7 7 9 0 0 . 2 4 9 1 0 0 . 3 1 8 7 0

0 . 3 8 9 0 0 . 4 5 8 7 0 . 52 7 5 0 . 5 9 52 0 . 6 6 3 2 0 . 7 3 1 1 0 . 7 9 8 2 0 . 8 6 4 1 0 . 92 9 6 0 . 9 9 5 5 1 . 0 6 0 3 1 . 12 4 1 1 . 1 8 7 0 1 . 2 4 8 8 1 . 3 1 0 9 1 . 3 7 1 0 1 . 4 2 92 1 . 5 4 0 7 1 . 5 9 3 0 1 . 6 3 9 9 1 . 6 6 7 2 1 . 6 9 5 3 1 . 7 2 6 9 1 . 7 4 8 8 1 . 7 6 6 6 1 . 7 8 7 7 1 . 7 9 8 9 1 . 8 1 4 7 1 . 82 2 6 1 . 8 2 7 5 1 . 8 3 5 1 1 . 8 3 4 7 1 . 8 3 4 9 1 . 8 2 6 5

Re = 2 . 0 0 0 e 6 Ncr it

CD Re (CL) CM --------- --------- --------

0 . 0 1 3 3 7 2 . 0 0 0 0 0 - 0 . 0 5 3 9 0 0 . 0 1 2 6 6 2 . 0 0 0 0 0 - 0 . 0 6 0 3 0 0 . 0 1 1 9 8 2 . 0 0 0 0 0 - 0 . 0 6 6 9 0 0 . 0 1 1 4 6 2 . 0 0 0 0 0 - 0 . 0 7 2 8 0 0 . 0 1 1 0 6 2 . 0 0 0 0 0 - 0 . 0 7 8 2 0 0 . 0 1 0 7 3 2 . 0 0 0 0 0 - 0 . 0 8 3 3 0 0 . 0 1 0 5 2 2 . 0 0 0 0 0 - 0 . 0 8 7 6 0 0 . 0 1 0 4 5 2 . 0 0 0 0 0 - 0 . 0 9 0 9 0 0 . 0 1 0 3 6 2 . 0 0 0 0 0 - 0 . 0 9 4 4 0 0 . 0 1 0 32 2 . 0 0 0 0 0 - 0 . 0 9 7 5 0 0 . 0 1 0 3 0 2 . 0 0 0 0 0 - 0 . 1 0 0 4 0 0 . 0 1 0 3 5 2 . 0 0 0 0 0 - 0 . 1 0 2 9 0

0 . 0 1 0 3 8 2 . 0 0 0 0 0 - 0 . 1 0 5 6 0 . 0 1 0 4 2 2 . 0 0 0 0 0 - 0 . 1 0 8 1 0 . 0 1 0 5 1 2 . 0 0 0 0 0 - 0 . 1 1 0 4 0 . 0 1 0 6 4 2 . 0 0 0 0 0 - 0 . 1 1 2 4 0 . 0 1 0 7 6 2 . 0 0 0 0 0 - 0 . 1 1 4 4 0 . 0 1 0 8 8 2 . 0 0 0 0 0 - 0 . 1 1 6 5 0 . 0 1 1 0 3 2 . 0 0 0 0 0 - 0 . 1 1 8 3 0 . 0 1 1 2 5 2 . 0 0 0 0 0 - 0 . 1 1 9 9 0 . 0 1 1 4 6 2 . 0 0 0 0 0 · - 0 . 12 1 4 0 . 0 1 1 6 5 2 . 0 0 0 0 0 - 0 . 1 2 3 0 0 . 0 1 1 8 9 2 . 0 0 0 0 0 - 0 . 12 4 3 0 . 0 12 1 7 2 . 0 0 0 0 0 - 0 . 1 2 5 5 0 . 0 12 4 8 2 . 0 0 0 0 0 - 0 . 1 2 6 4 0 . 0 1 2 8 2 2 . 0 0 0 0 0 - 0 . 1 2 7 2 0 . 0 1 3 1 3 2 . 0 0 0 0 0 - 0 . 1 2 8 0 0 . 0 1 3 5 2 2 . 0 0 0 0 0 - 0 . 12 8 5 0 . 0 1 3 9 6 2 . 0 0 0 0 0 - 0 . 1 2 8 6 0 . 0 1 4 9 4 2 . 0 0 0 0 0 - 0 . 1 2 7 9 0 . 0 1 5 5 2 2 . 0 0 0 0 0 - 0 . 12 7 1 0 . 0 1 62 8 2 . 0 0 0 0 0 - 0 . 1 2 5 4 0 . 0 1 7 3 0 2 . 0 0 0 0 0 - 0 . 12 0 4 0 . 0 1 8 7 9 2 . 0 0 0 0 0 - 0 . 1 1 6 3 0 . 0 2 0 3 0 2 . 0 0 0 0 0 - 0 . 1 1 3 2 0 . 02 2 4 9 2 . 0 0 0 0 0 - 0 . 1 0 9 7 0 . 0 2 5 3 0 2 . 0 0 0 0 0 - 0 . 1 0 6 5 0 . 0 2 8 3 1 2 . 0 0 0 0 0 - 0 . 1 0 4 3 0 . 0 3 2 4 3 2 . 0 0 0 0 0 - 0 . 1 02 2 0 . 0 3 6 4 0 2 . 0 0 0 0 0 - 0 . 1 0 0 9 0 . 0 4 1 5 4 2 . 0 0 0 0 0 ... 0 . 0 9 9 8 0 . 0 4 7 3 5 2 . 0 0 0 0 0 - 0 . 0 9 92 0 . 0 5 3 1 4 2 . 0 0 0 0 0 - 0 . 0 9 9 0 0 . 0 6 0 0 0 2 . 0 0 0 0 0 - 0 . 0 9 9 0 0 . 0 6 7 1 5 2 . 0 0 0 0 0 - 0 . 0 9 9 6 0 . 0 7 5 7 3 2 . 0 0 0 0 0 - 0 . 1 0 0 5

POL . W3_3 0 1_2 0_9 ; 4

9 . 0 0 0

S xtr P xt r - ------ -------0 . 4 97 5 0 0 . 3 4 3 5 0 0 . 4 8 0 8 0 0 . 3 5 1 5 0 0 . 4 6 8 6 0 0 . 3 6 2 2 0 0 . 4 5 3 6 0 0 . 3 6 7 2 0 0 . 4 4 2 8 0 0 . 3 7 2 4 0 0 . 42 6 0 0 0 . 3 8 2 5 0 0 . 4 1 6 8 0 0 . 3 8 9 8 0 0 . 4 0 5 8 0 0 . 3 9 3 3 0 0 . 3 9 3 8 0 0 . 4 0 0 6 0 0 . 3 8 7 0 0 0 . 4 0 9 1 0 0 . 3 7 1 8 0 0 . 4 1 5 1 0 0 . 3 6 5 8 0 0 . 4 1 8 2 0 0 . 3 5 8 4 0 . 42 5 2 0 . 3 4 6 7 0 . 4 3 3 2 0 . 3 3 9 9 0 . 4 3 9 1 0 . 3 3 3 5 0 . 4 4 2 2 0 . 32 3 5 0 . 4 4 6 8 0 . 3 1 6 5 0 . 4 5 4 9 0 . 3 1 2 4 0 . 4 6 1 5 0 . 3 0 3 8 0 . 4 6 52 0 . 2 9 42 0 . 4 6 7 6 0 . 2 9 0 3 0 . 4 7 5 3 0 . 2 8 6 4 0 . 4 8 2 0 0 . 2 8 0 4 0 . 4 8 6 6 0 . 2 7 0 1 0 . 4 8 9 9 0 . 2 6 5 9 0 . 4 92 5 0 . 2 62 8 0 . 4 9 9 0 0 . 2 5 8 3 0 . 5 0 5 6 0 . 2 4 9 6 0 . 5 1 0 3 0 . 2 4 0 4 0 . 5 1 6 3 0 . 2 3 7 3 0 . 5 1 9 6 0 . 2 3 0 9 0 . 52 7 0 0 . 2 2 4 8 0 . 5 3 2 1 0 . 2 1 8 1 0 . 5 3 6 3 0 . 2 1 6 5 0 . 5 3 8 9 0 . 2 12 8 0 . 5 4 0 9 0 . 2 0 8 3 0 . 5 4 2 6 0 . 2 0 2 0 0 . 5 4 9 5 0 . 1 9 4 2 0 . 5 5 4 7 0 . 1 92 2 0 . 5 5 92 0 . 1 8 8 9 0 . 5 6 1 9 0 . 1 8 4 0 0 . 5 6 4 0 0 . 1 7 7 5 0 . 5 6 5 8 0 . 1 7 0 7 0 . 5 6 7 2 0 . 1 6 8 2 0 . 5 7 2 2 0 . 1 6 4 1 0 . 5 7 7 0

FFA TN 1 9 9 0 - 1 5 7 8

XFOI L Ve rs ion 5 . 0

Calculated polar for : FFA-W3-3 0 1

1 Reynolds numbe r fixed

xt rf = 1 . 0 0 0 ( suction) 1 . 0 0 0 (pres sure ) Mach =

a lpha -------- 4 . 0 0 0 0 0 - 3 . 5 0 0 0 0 - 3 . 0 0 0 0 0 -2 . 5 0 0 0 0 -2 . 0 0 0 0 0 - 1 . 5 0 0 0 0 - 1 . 0 0 0 0 0 - 0 . 5 0 0 0 0

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 5 0 0 1 6 . 0 0 0 1 6 . 5 0 0

0 . 1 5 0

CL --------

- 0 . 1 7 0 7 0 - 0 . 0 9 6 6 0 - 0 . 02 3 6 0

0 . 0 4 8 3 0 0 . 1 1 9 6 0 0 . 1 9 0 9 0 0 . 2 6 1 0 0 0 . 3 3 0 6 0

0 . 4 0 0 2 0 . 4 6 9 5 0 . 5 3 7 7 0 . 6 0 5 9 0 . 6 7 3 9 0 . 7 4 1 5 0 . 8 0 8 3 0 . 8 7 4 8 0 . 9 4 1 1 1 . 0 0 6 8 1 . 0 7 2 0 1 . 1 3 6 6 1 . 2 0 0 3 1 . 2 6 3 7 1 . 32 6 0 1 . 3 8 7 6 1 . 4 4 7 9 1 . 5 0 7 0 1 . 5 6 42 1 . 6 1 9 1 1 . 6 7 32 1 . 7 2 3 1 1 . 7 5 4 1 1 . 7 7 8 9 1 . 8 0 7 8 1 . 8 3 4 8 1 . 8 5 1 3 1 . 8 6 4 1 1 . 8 7 5 2 1 . 8 9 0 4 1 . 9 0 1 5 1 . 9 0 0 2 1 . 9 0 0 0

Re = 3 . 0 0 0 e 6 Ncr it

CD Re (CL) CM --------- --------- --------

0 . 0 0 9 9 1 3 . 0 0 0 0 0 - 0 . 0 8 4 6 0 0 . 0.0 9 7 6 3 . 0 0 0 0 0 - 0 . 0 8 8 3 0 0 . 0 0 9 6 5 3 . 0 0 0 0 0 - 0 . 0 9 1 8 0 0 . 0 0 9 5 8 3 . 0 0 0 0 0 - 0 . 0 9 4 8 0 0 . 0 0 9 5 5 3 . 0 0 0 0 0 - 0 . 0 9 7 7 0 0 . 0 0 9 5 1 3 . 0 0 0 0 0 - 0 . 1 0 0 7 0 0 . 0 0 952 3 . 0 0 0 0 0 - 0 . 1 0 3 3 0 0 . 0 0 9 5 7 3 . 0 0 0 0 0 - 0 . 1 0 5 8 0

0 . 0 0 9 5 9 3 . 0 0 0 0 0 - 0 . 1 0 8 2 0 . 0 0 9 6 4 3 . 0 0 0 0 0 - 0 . 1 1 0 5 0 . 0 0 9 7 5 3 . 0 0 0 0 0 - 0 . 1 1 2 7 0 . 0 0 9 8 4 3 . 0 0 0 0 0 - 0 . 1 1 4 7 0 . 0 0 9 9 4 3 . 0 0 0 0 0 - 0 . 1 1 6 7 0 . 0 1 0 0 7 3 . 0 0 0 0 0 - 0 . 1 1 8 7 0 . 0 1 0 2 4 3 . 0 0 0 0 0 - 0 . 12 0 4 0 . 0 1 0 4 0 3 . 0 0 0 0 0 - 0 . 1 2 2 0 0 . 0 1 0 5 7 3 . 0 0 0 0 0 - 0 . 1 2 37 0 . 0 1 0 7 8 3 . 0 0 0 0 0 - 0 . 1252 0 . 0 1 0 9 9 3 . 0 0 0 0 0 - 0 . 1 2 6 5 0 . 0 1 1 2 3 3 . 0 0 0 0 0 - 0 . 1 2 78 0 . 0 1 1 4 9 3 . 0 0 0 0 0 - 0 . 1 2 8 8 0 . 0 1 1 7 7 3 . 0 0 0 0 0 - 0 . 1 2 9 9 0 . 0 1 2 0 9 3 . 0 0 0 0 0 - 0 . 1 3 0 7 0 . 0 1 2 4 2 3 . 0 0 0 0 0 - 0 . 1 3 1 3 0 . 0 1 2 78 3 . 0 0 0 0 0 - 0 . 1 3 1 7 0 . 0 1 3 1 7 3 . 0 0 0 0 0 - 0 . 1 3 1 9 0 . 0 1 3 6 4 3 . 0 0 0 0 0 - 0 . 1 3 1 8 0 . 0 1 4 1 6 3 . 0 0 0 0 0 - 0 . 1 3 1 4 0 . 0 1 4 6 7 3 . 0 0 0 0 0 - 0 . 1 3 0 7 0 . 0 1 5 3 0 3 . 0 0 0 0 0 - 0 . 1 2 9 3 0 . 0 1 6 2 7 3 . 0 0 0 0 0 - 0 . 12 4 9 0 . 0 1 7 6 8 3 . 0 0 0 0 0 - 0 . 1 1 9 9 0 . 0 1 92 2 3 . 0 0 0 0 0 - 0 . 1 1 62 0 . 0 2 1 0 9 3 . 0 0 0 0 0 - 0 . 1 1 2 9 0 . 0 2 3 7 8 3 . 0 0 0 0 0 - 0 . 1 0 9 3 0 . 0 2 7 1 4 3 . 0 0 0 0 0 - 0 . 1 0 6 1 0 . 0 3 1 1 1 3 . 0 0 0 0 0 - 0 . 1 0 3 7 0 . 0 3 5 1 1 3 . 0 0 0 0 0 - 0 . 1 0 2 1 0 . 0 4 5 9 4 3 . 0 0 0 0 0 - 0 . 1 0 0 2 0 . 0 5 2 6 1 3 . 0 0 0 0 0 - 0 . 0 9 9 8 0 . 0 5 9 6 3 3 . 0 0 0 0 0 - 0 . 1 0 0 0

POL . W3_3 0 1_3 0_9 ; 3

9 . 0 0 0

S xt r P xtr ------- -------0 . 4 1 8 1 0 0 . 3 62 6 0 0 . 4 0 9 3 0 0 . 3 7 3 3 0 0 . 3 9 8 3 0 0 . 37 8 3 0 0 . 3 8 6 9 0 0 . 3 8 1 3 0 0 . 3 8 0 3 0 0 . 3 9 0 6 0 0 . 3 6 5 1 0 0 . 3 9 9 4 0 0 . 3 5 9 5 0 0 . 4 0 3 4 0 0 . 3 5 1 8 0 0 . 4 0 7 3 0 0 . 3 4 0 5 0 . 4 1 6 0 0 . 3 3 5 4 0 . 4 2 3 8 0 . 32 7 2 0 . 4 2 7 4 0 . 3 1 7 3 0 . 4 3 0 4 0 . 3 1 1 5 0 . 4 3 8 7 0 . 3 0 71 0 . 4 4 6 6 0 . 2 97 4 0 . 4 5 0 4 0 . 2 8 8 3 0 . 4 5 2 8 0 . 2 8 5 7 0 . 4 5 9 0 0 . 2 8 1 2 0 . 4 6 7 6 0 . 2 7 4 3 0 . 4722 0 . 2 6 42 0 . 4 7 5 3 0 . 2 6 1 8 0 . 4 7 8 5 0 . 2 5 8 2 0 . 4 8 6 0 0 . 2 52 6 0 . 4 92 2 0 . 2 4 3 6 0 . 4 9 6 4 0 . 2 3 8 9 0 . 4 9 9 7 0 . 2 3 6 5 0 . 5 0 1 5 0 . 2 3 2 5 0 . 5 0 8 9 0 . 2 2 4 4 0 . 5 1 5 0 0 . 2 1 7 6 0 . 5 1 9 3 0 . 2 1 4 6 0 . 52 2 8 0 . 2 1 0 8 0 . 52 4 6 0 . 2 0 62 0 . 52 8 5 0 . 2 0 0 1 0 . 5 3 4 7 0 . 1 9 3 9 0 . 5 3 9 8 0 . 1 9 0 4 0 . 5 4 4 0 0 . 1 8 7 1 0 . 5 4 6 4 0 . 1 8 2 2 0 . 5 4 8 1 0 . 1 7 6 1 0 . 5 4 9 6 0 . 1 6 6 9 0 . 5 6 0 3 0 . 1 62 9 0 . 5 6 52 0 . 1 5 7 0 0 . 5 6 7 8

FFA TN 1 9 9 0 - 1 5 7 9 POL . W3_3 0 1_3 0_TU 1 ; 2

XFO IL Vers ion 5 . 0

Calculated pola r for : FFA-W3 - 3 0 1

1 Reynolds number fixed

xt rf = 0 . 0 1 0 ( suct ion ) 0 . 1 0 0 ( pres sure ) Mach = 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM s xt r P xt r - - -- --- -------- -------- - ------ - -- -------- ------- -------- 6 . 0 0 0 0 0 - 0 . 4 2 8 7 0 0 . 0 3 1 4 9 3 . 0 0 0 0 0 - 0 . 0 3 1 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 5 . 5 0 0 0 0 - 0 . 3 9 6 9 0 0 . 0 2 9 6 5 3 . 0 0 0 0 0 - 0 . 0 3 0 7 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 5 . 0 0 0 0 0 - 0 . 3 8 2 5 0 0 . 0 2 7 5 0 3 . 0 0 0 0 0 - 0 . 0 2 8 3 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 4 . 50 0 0 0 - 0 . 3 4 0 0 0 0 . 0 2 6 0 0 3 . 0 0 0 0 0 - 0 . 0 2 9 7 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 4 . 0 0 0 0 0 - 0 . 2 9 2 2 0 0 . 0 2 4 52 3 . 0 0 0 0 0 - 0 . 0 32 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 5 0 0 0 0 - 0 . 2 3 9 6 0 0 . 0 2 3 1 0 3 . 0 0 0 0 0 - 0 . 0 3 5 0 0 0 . 0 1 0 0 0 0 ; 1 0 0 0 0 - 3 . 0 0 0 0 0 - 0 . 1 8 0 1 0 0 . 0 2 2 0 4 3 . 0 0 0 0 0 - 0 . 0 3 8 5 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 2 . 5 0 0 0 0 - 0 . 1 1 6 3 0 0 . 0 2 0 9 3 3 . 0 0 0 0 0 - 0 . 0 4 3 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 -2 . 0 0 0 0 0 - 0 . 0 4 8 6 0 0 . 0 2 0 1 6 3 . 0 0 0 0 0 - 0 . 0 4 7 5 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 5 0 0 0 0 0 . 0 2 2 3 0 0 . 0 1 9 4 8 3 . 0 0 0 0 0 - 0 . 0 52 4 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 0 0 0 0 0 0 . 0 9 5 6 0 0 . 0 1 8 8 4 3 . 0 0 0 0 0 - 0 . 0 5 7 7 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 0 . 5 0 0 0 0 0 . 1 6 9 5 0 0 . 0 1 8 4 0 3 . 0 0 0 0 0 - 0 . 0 62 6 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0

0 . 0 0 0 0 . 2 4 4 9 0 . 0 1 7 9 9 3 . 0 0 0 0 0 - 0 . 0 6 7 9 0 . 0 1 0 0 0 . 1 0 0 0 0 . 5 0 0 0 . 32 0 2 0 . 0 1 7 7 0 3 . 0 0 0 0 0 - 0 . 0 7 2 9 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 . 3 9 5 3 0 . 0 1 7 4 8 3 . 0 0 0 0 0 - 0 . 0 7 7 7 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 4 7 0 3 0 . 0 1 7 3 2 3 . 0 0 0 0 0 - 0 . 0 8 2 5 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 5 4 4 2 0 . 0 1 7 2 5 3 . 0 0 0 0 0 - 0 . 0 8 6 8 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 6 1 7 0 0 . 0 1 7 2 4 3 . 0 0 0 0 0 - 0 . 0 9 0 9 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 8 8 5 0 . 0 1 7 3 0 3 . 0 0 0 0 0 - 0 . 0 9 4 6 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 7 5 7 2 0 . 0 1 7 4 6 3 . 0 0 0 0 0 - 0 . 0 9 7 6 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 8 2 2 7 0 . 0 1 7 7 4 3 . 0 0 0 0 0 - 0 . 0 9 9 9 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 8 8 6 0 0 . 0 1 8 0 8 3 . 0 0 0 0 0 - 0 . 1 0 1 6 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 9 4 6 9 0 . 0 1 8 4 9 3 . 0 0 0 0 0 - 0 . 1 0 3 0 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 1 . 0 0 4 6 0 . 0 1 8 9 8 3 . 0 0 0 0 0 - 0 . 1 0 3 7 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 1 . 0 5 8 1 0 . 0 1 9 5 5 3 . 0 0 0 0 0 - 0 . 1 0 3 8 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 1 0 1 9 0 . 0 2 0 2 7 3 . 0 0 0 0 0 - 0 . 1 0 2 1 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 12 0 1 0 . 0 2 1 52 3 . 0 0 0 0 0 - 0 . 0 9 6 6 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1.53 9 0 . 0 2 3 0 7 3 . 0 0 0 0 0 - 0 . 0 9 4 6 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 1 8 2 9 0 . 02 5 0 6 3 . 0 0 0 0 0 - 0 . 0 9 2 6 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 2 0 7 5 0 . 0 2 7 5 8 3 . 0 0 0 0 0 - 0 . 0 9 0 9 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 2 3 0 9 0 . 0 3 0 6 0 3 . 0 0 0 0 0 - 0 . 0 8 9 8 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 2 5 2 2 0 . 0 3 4 1 9 3 . 0 0 0 0 0 - 0 . 0 8 92 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 2 7 0 1 0 . 0 3 8 42 3 . 0 0 0 0 0 - 0 . 0 8 9 1 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 2 8 7 8 0 . 0 4 3 0 8 3 . 0 0 0 0 0 - 0 . 0 8 9 4 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 3 0 3 8 0 . 0 4 8 2 8 3 . 0 0 0 0 0 - 0 . 0 9 0 2 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 3 1 7 3 0 . 0 5 4 1 4 3 . 0 0 0 0 0 - 0 . 0 9 1 3 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 3 2 9 4 0 . 0 6 0 3 1 3 . 0 0 0 0 0 - 0 . 0 92 5 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 3 3 8 8 0 . 0 6 6 92 3 . 0 0 0 0 0 - 0 . 0 9 3 9 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 3 4 6 5 0 . 0 7 4 0 2 3 . 0 0 0 0 0 - 0 . 0 9 5 4 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 3 5 2 4 0 . 0 8 1 6 0 3 . 0 0 0 0 0 - 0 . 0 9 7 1 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 3 5 6 7 0 . 0 8 9 6 1 3 . 0 0 0 0 0 - 0 . 0 9 9 1 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 3 6 0 1 0 . 0 9 7 92 3 . 0 0 0 0 0 - 0 . 1 0 1 1 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1. 3 6 3 4 0 . 1 0 6 1 5 3 . 0 0 0 0 0 - 0 . 1 0 3 1 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 5 0 0 1 . 3 6 3 0 0 . 1 1 5 4 8 3 . 0 0 0 0 0 - 0 . 1 0 55 0 . 0 1 0 0 0 . 1 0 0 0 1 6 . 0 0 0 1 . 3 6 1 7 0 . 1 2 5 2 8 3 . 0 0 0 0 0 - 0 . 1 0 8 2 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 8 0

XFOI L Ve rs ion 5 . 0

Calculated polar for : FFA-W3- 3 32

1 Reynolds number fixed

xt rf .. 1 . 0 0 0 ( suction) 1 . 0 0 0 ( pre s su re ) Mach =

a lpha ------ -- 4 . 0 0 0 - 3 . 5 0 0 - 3 . 0 0 0 - 2 . 5 0 0 -2 . 0 0 0 - 1 . 5 0 0 - 1 . 0 0 0 - 0 . 5 0 0

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0 1 5 . 5 0 0 1 6 . 0 0 0

0 . 1 5 0

CL --------- 0 . 3 1 4 3 - 0 . 2 3 5 3 - 0 . 1 5 5 6 - 0 . 0 7 1 4

0 . 0 1 1 1 0 . 0 9 3 3 0 . 1 7 7 0 0 . 2 5 6 5 0 . 3 3 7 2 0 . 4 1 5 5 0 . 4 8 9 4 0 . 5 6 3 0 0 . 6 3 6 3 0 . 7 0 6 9 0 . 7 7 5 8 0 . 8 4 62 0 . 9 1 4 1 0 . 9 1 4 1 0 . 9 7 9 4 1 . 0 4 4 5 1 . 1 0 9 7 1 . 1 7 1 4 1 . 1 7 1 4 1 . 2 3 1 0 1 . 2 8 8 7 1 . 3 4 42 1 . 3 9 2 0 1 . 3 92 0 1 . 4 2 2 6 1 . 4 5 4 9 1 . 4 8 2 1 1 . 5 0 2 7 1 . 5 2 4 1 1 . 5 4 3 3 1 . 5 5 7 5 1 . 5 6 5 5 1 . 5 7 2 3 1 . 5 8 3 2 1 . 5 8 8 8 1 . 5 8 8 0 1 . 5 7 5 4 1 . 5 8 1 6 1 . 5 8 1 7 1 . 5 7 6 7

Re = 1 . 0 0 0 e 6 Ncr it

CD Re (CL) CM --------- --------- --------

0 . 0 1 7 1 1 1 . 0 0 0 0 0 - 0 . 0 4 4 6 0 . 0 1 6 3 0 1 . 0 0 0 0 0 - 0 . 0 5 1 0 0 . 0 1 5 7 4 1 . 0 0 0 0 0 - 0 . 0 5 6 9 0 . 0 1 5 1 6 1 . 0 0 0 0 0 - 0 . 0 6 3 9 0 . 0 1 4 7 9 1 . 0 0 0 0 0 - 0 . 0 7 0 0 0 . 0 1 452 1 . 0 0 0 0 0 - 0 . 0 7 5 8 0 . 0 1 42 7 1 . 0 0 0 0 0 - 0 . 0 8 1 9 0 . 0 1 4 1 8 1 . 0 0 0 0 0 - 0 . 0 8 6 8 0 . 0 1 4 0 9 1 . 0 0 0 0 0 - 0 . 0 9 1 9 0 . 0 1 4 0 9 1 . 0 0 0 0 0 - 0 . 0 9 6 4 0 . 0 1 4 2 1 1 . 0 0 0 0 0 - 0 . 0 9 9 7 0 . 0 1 435 1 . 0 0 0 0 0 - 0 . 1 0 3 0 0 . 0 1 4 5 0 1 . 0 0 0 0 0 - 0 . 1 0 6 1 0 . 0 1 4 72 1 . 0 0 0 0 0 - 0 . 1 0 8 6 0 . 0 1 5 0 1 1 . 0 0 0 0 0 - 0 . 1 1 0 7 0 . 0 1 523 1 . 0 0 0 0 0 - 0 . 1 1 32 0 . 0 1 5 5 4 1 . 0 0 0 0 0 - 0 . 1 1 52 0 . 0 1 554 1 . 0 0 0 0 0 - 0 . 1 1 52 0 . 0 1 5 9 6 1 . 0 0 0 0 0 - 0 . 1 1 6 6 0 . 0 1 6 3 0 1 . 0 0 0 0 0 - 0 . 1 1 7 9 0 . 0 1 6 6 8 1 . 0 0 0 0 0 - 0 . 1 1 9 3 0 . 0 1 7 1 9 1 . 0 0 0 0 0 - 0 . 12 0 1 0 . 0 1 7 1 9 1 . 0 0 0 0 0 - 0 . 1 2 0 1 0 . 0 1 7 7 3 1 . 0 0 0 0 0 - 0 . 1 2 0 5 0 . 0 1 8 3 1 1 . 0 0 0 0 0 - 0 . 1 2 0 5 0 . 0 1 8 9 8 1 . 0 0 0 0 0 - 0 . 1 2 0 3 0 . 0 1 9 9 3 1 . 0 0 0 0 0 - 0 . 1 1 8 9 0 . 0 1 9 9 3 1 . 0 0 0 0 0 - 0 . 1 1 8 9 0 . 0 2 1 0 2 1 . 0 0 0 0 0 - 0 . 1 1 4 5 0 . 0 2 2 5 5 1 . 0 0 0 0 0 - 0 . 1 1 1 1 0 . 0 2 4 5 8 1 . 0 0 0 0 0 - 0 . 1 0 7 8 0 . 0 2 7 4 1 1 . 0 0 0 0 0 - 0 . 1 0 5 0 0 . 0 3 0 5 3 1 . 0 0 0 0 0 - 0 . 1 0 3 0 0 . 0 3 4 2 6 1 . 0 0 0 0 0 - 0 . 1 0 1 6 0 . 0 3 8 8 9 1 . 0 0 0 0 0 - 0 . 1 0 0 8 0 . 0 4 4 5 6 1 . 0 0 0 0 0 - 0 . 1 0 0 6 0 . 0 5 0 9 2 1 . 0 0 0 0 0 - 0 . 1 0 12 0 . 0 5 7 0 3 1 . 0 0 0 0 0 - 0 . 1 0 1 9 0 . 0 6 3 8 9 1 . 0 0 0 0 0 - 0 . 1 0 2 8 0 . 0 7 1 8 0 1 . 0 0 0 0 0 - 0 . 1 0 4 0 0 . 0 8 1 5 3 1 . 0 0 0 0 0 - 0 . 1 0 5 6 0 . 0 8 9 1 3 1 . 0 0 0 0 0 - 0 . 1 0 7 3 0 . 0 9 7 62 1 . 0 0 0 0 0 - 0 . 1 0 9 1 0 . 1 0 7 0 9 1 . 0 0 0 0 0 - 0 . 1 1 12

POL . W3_3 32_1 0_9 ; 2

9 . 0 0 0

S xt r P xt r ------- -------0 . 4 4 1 1 0 . 37 4 2 0 . 4 2 8 0 0 . 3 8 2 7 0 . 4 1 3 9 0 . 3 8 8 0 0 . 4 0 2 6 0 . 3 9 8 2 0 . 3 8 9 4 0 . 4 0 5 1 0 . 3 7 9 0 0 . 4 1 1 2 0 . 3 6 6 7 0 . 4 2 0 4 0 . 3552 0 . 4 2 5 3 0 . 3 4 6 4 0 . 4 3 3 0 0 . 3 3 62 0 . 4 3 9 8 0 . 32 6 9 0 . 4 4 4 1 0 . 3 1 8 6 0 . 4 4 9 9 0 . 3 0 9 4 0 . 4 5 7 1 0 . 3 0 2 7 0 . 4 6 1 4 0 . 2 92 6 0 . 4 6 5 3 0 . 2 8 7 6 0 . 4 7 2 1 0 . 2 8 0 7 0 . 4 7 7 5 0 . 2 8 0 7 0 . 4 7 7 5 0 . 2 7 1 3 0 . 4 8 1 6 0 . 2 6 7 7 0 . 4 8 4 8 0 . 2 62 7 0 . 4 9 1 4 0 . 2 5 4 9 0 . 4 9 6 9 0 . 2 5 4 9 0 . 4 9 6 9 0 . 2 4 9 3 0 . 5 0 0 5 0 . 2 4 5 3 0 . 5 0 3 6 0 . 2 3 9 6 0 . 5 0 9 1 0 . 2 32 1 0 . 5 1 5 0 0 . 2 3 2 1 0 . 5 1 5 0 0 . 2 2 9 7 0 . 5 1 8 5 0 . 2 2 5 7 0 . 5 2 1 6 0 . 2 2 0 8 0 . 52 4 5 0 . 2 1 4 0 0 . 5 3 1 4 0 . 2 1 1 2 0 . 5 3 5 5 0 . 2 0 8 4 0 . 5 3 8 7 0 . 2 0 4 7 0 . 5 4 1 6 0 . 1 97 6 0 . 5 4 5 1 0 . 1 9 32 0 . 55 1 0 0 . 1 9 0 7 0 . 5 5 4 8 0 . 1 8 7 3 0 . 55 7 8 0 . 1 8 2 3 0 . 5 6 0 8 0 . 1 7 57 0 . 5 62 9 0 . 1 7 3 6 0 . 5 6 8 8 0 . 1 7 0 9 0 . 5 7 2 9 0 . 1 6 7 1 0 . 5 7 5 8

FFA TN 1 9 9 0 - 1 5 8 1 POL . W3_332_1 0_TU1 ; 2

XFO I L Vers ion 5 . 0

Calculated polar for : FFA-W3- 3 3 2

1 Reynolds numbe r f ixed

xt rf = 0 . 0 1 0 ( suct ion ) 0 . 1 0 0 (pre s sure ) Mach -= 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xt r ------- -------- --------- --------- -------- ------ - ------ -

- 4 . 0 0 0 - 0 . 1 3 2 8 0 . 0 3 9 1 1 1 . 0 0 0 0 0 - 0 . 0 3 4 9 0 . 0 1 0 0 0 . 1 0 0 0 - 3 . 5 0 0 - 0 . 1 0 3 0 0 . 0 3 7 0 6 1 . 0 0 0 0 0 - 0 . 0 3 4 5 0 . 0 1 0 0 0 . 1 0 0 0 - 3 . 0 0 0 - 0 . 0 7 4 2 0 . 0 3 5 1 5 1 . 0 0 0 0 0 - 0 . 0 3 3 7 0 . 0 1 0 0 0 . 1 0 0 0 - 2 . 5 0 0 - 0 . 0 4 9 9 0 . 0 3 3 2 7 1 . 0 0 0 0 0 - 0 . 0 3 2 1 0 . 0 1 0 0 0 . 1 0 0 0 - 2 . 0 0 0 - 0 . 0 4 1 7 0 . 0 3 1 5 0 1 . 0 0 0 0 0 - 0 . 0 2 8 2 0 . 0 1 0 0 0 . 1 0 0 0 - 1 . 5 0 0 - 0 . 0 0 7 3 0 . 0 3 0 0 5 1 . 0 0 0 0 0 - 0 . 02 8 1 0 . 0 1 0 0 0 . 1 0 0 0 - 1 . 0 0 0 0 . 0 3 42 0 . 02 8 6 8 1 . 0 0 0 0 0 - 0 . 0 2 92 0 . 0 1 0 0 0 . 1 0 0 0 - 0 . 5 0 0 0 . 0 8 3 5 0 . 02 7 5 6 1 . 0 0 0 0 0 - 0 . 0 3 1 4 0 . 0 1 0 0 0 . 1 0 0 0

0 . 0 0 0 0 . 1 3 8 9 0 . 02 6 6 0 1 . 0 0 0 0 0 - 0 . 0 3 4 2 0 . 0 1 0 0 0 . 1 0 0 0 0 . 5 0 0 0 . 2 0 0 2 0 . 0 2 5 8 2 1 . 0 0 0 0 0 . - 0 . 0 3 7 9 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 . 2 6 52 0 . 0 2 5 2 5 1 . 0 0 0 0 0 - 0 . 0 4 1 9 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 3 3 3 2 0 . 0 2 4 8 1 1 . 0 0 0 0 0 - 0 . 0 4 6 3 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 4 0 2 3 0 . 0 2 4 5 6 1 . 0 0 0 0 0 - 0 . 0 5 0 6 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 4 7 2 2 0 . 0 2 4 4 1 1 . 0 0 0 0 0 - 0 . 0 5 5 0 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 5 4 1 1 0 . 02 4 4 4 1 . 0 0 0 0 0 - 0 . 0 5 9 1 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 6 0 8 5 0 . 0 2 4 5 9 1 . 0 0 0 0 0 - 0 . 0 62 9 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 6 6 7 2 0 . 0 2 4 9 1 1 . 0 0 0 0 0 - 0 . 0 6 5 1 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 7 0 5 4 0 . 0 2 5 5 7 1 . 0 0 0 0 0 - 0 . 0 6 4 1 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 7 5 6 8 0 . 0 2 6 6 4 1 . 0 0 0 0 0 - 0 . 0 6 5 8 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 8 0 6 0 0 . 02 8 1 0 1 . 0 0 0 0 0 - 0 . 0 6 7 6 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 8 4 9 5 0 . 0 3 0 0 6 1 . 0 0 0 0 0 - 0 . 0 6 9 3 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 0 . 8 8 8 0 0 . 0 32 6 1 1 . 0 0 0 0 0 - 0 . 0 7 1 0 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 0 . 92 0 4 0 . 0 3 5 8 6 1 . 0 0 0 0 0 - 0 . 0 7 2 5 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 0 . 9 4 9 6 0 . 0 3 9 7 5 1 . 0 0 0 0 0 - 0 . 0 7 4 3 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 0 . 9 7 6 4 0 . 0 4 42 5 1 . 0 0 0 0 0 - 0 . 0 7 6 5 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 0 0 0 2 0 . 0 4 9 3 4 1 . 0 0 0 0 0 - 0 . 0 7 8 9 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 0 2 1 5 0 . 0 5 5 0 0 1 . 0 0 0 0 0 - 0 . 0 8 1 4 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 0 4 0 4 0 . 0 6 1 1 5 1 . 0 0 0 0 0 - 0 . 0 8 4 1 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 0 5 6 8 0 . 0 6 7 7 6 1 . 0 0 0 0 0 - 0 . 0 8 6 8 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 0 7 0 6 0 . 0 7 4 8 3 1 . 0 0 0 0 0 - 0 . 0 8 9 5 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 0 8 2 2 0 . 0 8 2 4 4 1 . 0 0 0 0 0 - 0 . 0 92 3 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 0 92 4 0 . 0 9 0 4 1 1 . 0 0 0 0 0 - 0 . 0 9 52 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 1 0 0 7 0 . 0 9 8 7 6 1 . 0 0 0 0 0 - 0 . 0 9 8 1 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 1 0 7 4 0 . 1 0 7 5 6 1 . 0 0 0 0 0 - 0 . 1 0 1 1 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 1 1 3 1 0 . 1 1 6 7 8 1 . 0 0 0 0 0 - 0 . 1 0 42 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 1 1 7 9 0 . 12 6 4 0 1 . 0 0 0 0 0 - 0 . 1 0 7 5 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 1 2 1 9 0 . 1 3 6 2 9 1 . 0 0 0 0 0 - 0 . 1 1 0 8 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 12 5 9 0 . 1 4 6 4 4 1 . 0 0 0 0 0 - 0 . 1 1 42 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 1 2 8 4 0 . 1 5 7 2 9 1 . 0 0 0 0 0 - 0 . 1 1 7 8 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 8 2

XFO IL Ve rs ion 5 . 0

Calculated polar for : FFA-W3 -332

1 Reynolds numbe r fixed

xt rf "" 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pres sure ) Mach = 0 . 1 5 0 Re = 2 . 0 0 0 e 6 Ncr it

a lpha CL CD Re (CL) CM - - - - - - - -------- -------- - ---- - - --- --------- 4 . 0 0 0 - 0 . 2 6 5 1 0 . 0 1 4 0 0 2 . 0 0 0 0 0 - 0 . 0 6 0 3 - 3 . 5 0 0 - 0 . 1 8 1 2 0 . 0 1 3 5 0 2 . 0 0 0 0 0 - 0 . 0 6 6 8 - 3 . 0 0 0 - 0 . 0 9 8 6 0 . 0 1 3 1 3 2 . 0 0 0 0 0 - 0 . 0 7 2 7 - 2 . 5 0 0 - 0 . 0 1 3 6 0 . 0 1 2 7 4 2 . 0 0 0 0 0 - 0 . 0 7 92 - 2 . 0 0 0 0 . 0 6 9 5 0 . 0 1 2 4 8 2 . 0 0 0 0 0 - 0 . 0 8 5 0 - 1 . 5 0 0 0 . 1 5 1 9 0 . 0 1 2 2 6 2 . 0 0 0 0 0 - 0 . 0 9 0 5 - 1 . 0 0 0 0 . 2 3 2 3 0 . 0 1 2 12 2 . 0 0 0 0 0 - 0 . 0 9 54 - 0 . 5 0 0 0 . 3 0 9 4 0 . 0 1 2 0 8 2 . 0 0 0 0 0 - 0 . 0 9 9 5

0 . 0 0 0 0 . 3 8 5 3 0 . 0 1 2 1 0 2 . 0 0 0 0 0 - 0 . 1 0 32 0 . 5 0 0 0 . 4 5 9 7 0 . 0 1 2 1 5 2 . 0 0 0 0 0 - 0 . 1 0 6 5 1 . 0 0 0 0 . 5 32 1 0 . 0 1 2 2 6 2 . 0 0 0 0 0 - 0 . 1 0 9 3 1 . 5 0 0 0 . 6 0 5 0 0 . 0 12 3 7 2 . 0 0 0 0 0 - 0 . 1 12 2 2 . 0 0 0 0 . 6 7 6 6 0 . 0 1 2 4 9 2 . 0 0 0 0 0 - 0 . 1 1 4 8 2 . 5 0 0 0 . 7 4 6 7 0 . 0 1 2 6 8 2 . 0 0 0 0 0 - 0 . 1 1 7 0 3 . 0 0 0 0 . 8 1 6 6 0 . 0 12 8 7 2 . 0 0 0 0 0 - 0 . 1 1 92 3 . 5 0 0 0 . 8 8 6 2 0 . 0 1 3 0 7 2 . 0 0 0 0 0 - 0 . 1 2 1 4 4 . 0 0 0 0 . 9 5 4 4 0 . 0 1 332 2 . 0 0 0 0 0 - 0 . 1 2 3 1 4 . 0 0 0 0 . 9 5 4 4 0 . 0 1 332 2 . 0 0 0 0 0 - 0 . 1 2 3 1 4 . 5 0 0 1. 0 2 1 3 0 . 0 1 3 6 1 2 . 0 0 0 0 0 - 0 . 1 2 4 6 5 . 0 0 0 1 . 0 8 8 9 0 . 0 1 3 8 6 2 . 0 0 0 0 0 - 0 . 1 2 6 3 5 . 5 0 0 1 . 1 5 4 4 0 . 0 1 42 2 2 . 0 0 0 0 0 - 0 . 12 7 6 6 . 0 0 0 1 . 2 1 92 0 . 0 1 4 5 6 2 . 0 0 0 0 0 - 0 . 12 8 7 6 . 0 0 0 1 . 2 1 92 0 . 0 1 4 5 6 2 . 0 0 0 0 0 - 0 . 12 8 7 6 . 5 0 0 1 . 2 8 2 4 0 . 0 1 4 9 6 2 . 0 0 0 0 0 - 0 . 1 2 9 5 7 . 0 0 0 1 . 3 4 5 1 0 . 0 1 5 3 7 2 . 0 0 0 0 0 - 0 . 1 3 0 2 7 . 5 0 0 1 . 4 0 5 4 0 . 0 1 5 8 8 2 . 0 0 0 0 0 - 0 . 1 3 0 6 8 . 0 0 0 1 . 4 6 3 8 0 . 0 1 6 4 5 2 . 0 0 0 0 0 - 0 . 1 3 0 5 8 . 0 0 0 1 . 4 6 3 8 0 . 0 1 6 4 5 2 . 0 0 0 0 0 - 0 . 1 3 0 5 8 . 5 0 0 1 . 5 2 0 7 0 . 0 1 7 0 0 2 . 0 0 0 0 0 - 0 . 1 3 0 3 9 . 0 0 0 1 . 5 7 3 7 0 . 0 1 7 7 0 2 . 0 0 0 0 0 - 0 . 12 9 4 9 . 5 0 0 1. 6 2 2 8 0 . 0 1 8 5 2 2 . 0 0 0 0 0 - 0 . 1 2 7 9

1 0 . 0 0 0 1 . 6 4 7 2 0 . 0 1 9 8 2 2 . 0 0 0 0 0 - 0 . 1 2 2 3 1 0 . 5 0 0 1 . 6 7 3 5 0 . 0 2 1 5 5 2 . 0 0 0 0 0 - 0 . 1 1 8 0 1 1 . 0 0 0 1 . 6 9 7 0 0 . 0 2 3 7 1 2 . 0 0 0 0 0 - 0 . 11 4 1 1 1 . 5 0 0 1 . 7 1 4 4 0 . 0 2 6 5 9 2 . 0 0 0 0 0 - 0 . 1 1 0 6 1 2 . 0 0 0 1 . 7 3 1 6 0 . 0 2 9 9 8 2 . 0 0 0 0 0 - 0 . 1 0 8 1 1 2 . 5 0 0 1 . 7 4 2 3 0 . 0 3 4 4 2 2 . 0 0 0 0 0 - 0 . 1 0 62 1 3 . 0 0 0 1 . 7 5 5 9 0 . 0 3 9 0 5 2 . 0 0 0 0 0 - 0 . 1 0 52 1 3 . 5 0 0 1 . 7 6 3 6 0 . 0 4 4 6 7 2 . 0 0 0 0 0 - 0 . 1 0 4 7 1 4 . 0 0 0 1 . 7 6 7 8 0 . 0 5 1 1 4 2 . 0 0 0 0 0 - 0 . 1 0 4 9 1 4 . 5 0 0 1 . 7 7 2 5 0 . 0 5 7 9 1 2 . 0 0 0 0 0 - 0 . 1 0 5 4 1 5 . 0 0 0 1 . 7 7 0 3 0 . 0 6 5 62 2 . 0 0 0 0 0 - 0 . 1 0 62 1 5 . 5 0 0 1 . 7 7 1 4 0 . 0 7 3 2 6 2 . 0 0 0 0 0 - 0 . 1 0 7 2 1 6 . 0 0 0 1 . 7 6 8 4 0 . 0 8 1 5 7 2 . 0 0 0 0 0 - 0 . 1 0 8 4

POL . W3_332_2 0_9 ; 2

9 . 0 0 0

S xt r P xt r ------- -------0 . 4 0 7 3 0 . 3 5 5 7 0 . 3 9 1 2 0 . 3 6 4 4 0 . 3 8 2 2 0 . 3 6 9 6 0 . 3 6 9 5 0 . 3 8 0 0 0 . 3 57 1 0 . 3 8 6 8 0 . 3 4 7 6 0 . 3 9 4 7 0 . 3 3 7 0 0 . 4 0 2 6 0 . 32 8 3 0 . 4 0 7 7 0 . 3 1 7 9 0 . 4 1 5 7 0 . 3 0 92 0 . 42 3 2 0 . 3 0 3 1 0 . 42 7 0 0 . 2 9 1 0 0 . 4 3 4 5 0 . 2 8 6 9 0 . 4 4 1 7 0 . 2 7 9 7 0 . 4 4 5 4 0 . 2 7 0 4 0 . 4 5 0 6 0 . 2 6 6 4 0 . 4 5 8 5 0 . 2 5 9 8 0 . 4 6 2 6 0 . 2 5 9 8 0 . 4 6 2 6 0 . 2 5 1 6 0 . 4 6 5 5 0 . 2 4 8 7 0 . 4 7 2 4 0 . 2 4 2 6 0 . 4 7 8 1 0 . 2 34 9 0 . 4 8 1 8 0 . 2 3 4 9 0 . 4 8 1 8 0 . 2 3 0 8 0 . 4 8 4 5 0 . 2 2 7 5 0 . 4 9 0 2 0 . 2 2 0 5 0 . 4 9 6 1 0 . 2 1 3 1 0 . 5 0 0 1 0 . 2 1 3 1 0 . 5 0 0 1 0 . 2 1 1 0 0 . 5 0 3 3 0 . 2 0 7 6 0 . 5 0 6 5 0 . 2 0 2 3 0 . 5 1 32 0 . 1 9 6 3 0 . 5 1 8 1 0 . 1 92 7 0 . 52 1 1 0 . 1 9 0 1 0 . 52 3 4 0 . 1 8 6 4 0 . 52 7 7 0 . 1 8 1 1 0 . 5 3 3 4 0 . 1 7 5 8 0 . 5 3 7 9 0 . 1 7 4 2 0 . 5 4 0 7 0 . 1 7 1 8 0 . 5 4 3 0 0 . 1 6 8 3 0 . 5 4 7 1 0 . 1 6 3 3 0 . 5 5 3 3 0 . 1 5 7 5 0 . 5 5 6 8 0 . 1 5 6 0 0 . 5 5 9 7 0 . 1 5 3 7 0 . 5 6 1 8

FFA TN 1 9 9 0 - 1 5 8 3 POL . W3_332_30_9 ; 2

XFOI L Version 5 . 0

Calculated polar for : FFA-W3-332

1 Reynolds number fixed

xt rf • 1 . 0 0 0 ( suct ion ) 1 . 0 0 0 (pressure ) Mach • 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM s xt r P xt r - ------ -------- --- - - - --- --------- -------- ------- -------- 4 . 0 0 0 - 0 . 2 3 3 0 0 . 0 1 2 5 1 3 . 0 0 0 0 0 - 0 . 0 6 9 4 0 . 3 8 6 8 0 . 3 4 6 4 - 3 . 5 0 0 - 0 . 1 4 8 0 0 . 0 1 2 0 9 3 . 0 0 0 0 0 - 0 . 0 7 5 8 0 . 37 1 8 0 . 3 5 0 9 - 3 . 0 0 0 - 0 . 0 6 3 6 0 . 0 1 1 7 6 3 . 0 0 0 0 0 - 0 . 0 8 2 0 0 . 3 6 4 6 0 . 3 6 3 0 - 2 . 5 0 0 0 . 0 1 9 5 0 . 0 1 1 5 1 3 . 0 0 0 0 0 - 0 . 0 8 7 7 0 . 3 5 0 0 0 . 3 6 8 2 - 2 . 0 0 0 0 . 1 0 1 0 0 . 0 1 1 3 2 3 . 0 0 0 0 0 - 0 . 0 92 9 0 . 3 4 1 6 0 . 3 7 5 2 - 1 . 5 0 0 0 . 1 7 9 9 0 . 0 1 1 2 1 3 . 0 0 0 0 0 - 0 . 0 9 7 4 0 . 3 3 0 2 0 . 3 8 4 6 - 1 . 0 0 0 0 . 2 5 5 6 0 . 0 1 12 0 3 . 0 0 0 0 0 - 0 . 1 0 1 0 0 . 32 3 5 0 . 3 8 9 0 - 0 . 5 0 0 0 . 3 3 0 7 0 . 0 1 1 2 0 3 . 0 0 0 0 0 - 0 . 1 0 4 5 0 . 3 1 0 5 0 . 3 9 8 3

0 . 0 0 0 0 . 4 0 5 2 0 . 0 1 1 2 3 3 . 0 0 0 0 0 - 0 . 1 0 7 8 0 . 3 0 5 2 0 . 4 0 5 4 0 . 5 0 0 0 . 4 7 8 2 0 . 0 1 1 2 9 3 . 0 0 0 0 0 - 0 . 1 1 0 7 0 . 2 9 5 1 0 . 4 0 8 8 1 . 0 0 0 0 . 5 5 0 7 0 . 0 1 1 3 8 3 . 0 0 0 0 0 - 0 . 11 3 5 0 . 2 8 8 1 0 . 4 1 9 5 1 . 5 0 0 0 . 6 2 2 4 0 . 0 1 1 5 0 3 . 0 0 0 0 0 - 0 . 1 1 6 0 0 . 2 8 1 3 0 . 42 4 7 2 . 0 0 0 0 . 6 9 3 1 0 . 0 1 1 62 3 . 0 0 0 0 0 - 0 . 1 1 8 3 0 . 2 7 1 5 0 . 4 2 7 8 2 . 5 0 0 0 . 7 6 3 8 0 . 0 1 1 7 8 3 . 0 0 0 0 0 - 0 . 1 2 0 7 0 . 2 6 7 2 0 . 4 37 9 3 . 0 0 0 0 . 8 3 3 5 0 . 0 1 1 9 6 3 . 0 0 0 0 0 - 0 . 1 2 2 8 0 . 2 6 0 6 0 . 4 4 3 1 3 . 5 0 0 0 . 9 0 2 6 0 . 0 1 2 1 4 3 . 0 0 0 0 0 - 0 . 12 4 6 0 . 2 52 0 0 . 4 4 6 3 4 . 0 0 0 0 . 9 7 1 3 0 . 0 1 2 3 5 3 . 0 0 0 0 0 - 0 . 12 6 5 0 . 2 4 92 0 . 4 5 3 4 4 . 0 0 0 0 . 9 7 1 3 0 . 0 12 3 5 3 . 0 0 0 0 0 - 0 . 1 2 6 5 0 . 2 4 9 2 0 . 4 5 3 4 4 . 5 0 0 1 . 0 3 8 8 0 . 0 1 2 6 3 3 . 0 0 0 0 0 - 0 . 1 2 8 1 0 . 2 42 9 0 . 4 5 9 6 5 . 0 0 0 1 . 1 0 62 0 . 0 12 8 7 3 . 0 0 0 0 0 - 0 . 1 2 9 6 0 . 2 3 5 4 0 . 4 6 3 4 5 . 5 0 0 1 . 1 7 2 1 0 . 0 1 3 1 7 3 . 0 0 0 0 0 - 0 . 1 3 0 9 0 . 2 3 1 1 0 . 4 6 6 2 6 . 0 0 0 1 . 2 3 8 0 0 . 0 1 3 4 8 3 . 0 0 0 0 0 - 0 . 1 3 2 2 0 . 2 2 7 8 0 . 4 7 2 8 6 . 0 0 0 1 . 2 3 8 0 0 . 0 1 3 4 8 3 . 0 0 0 0 0 - 0 . 1 3 2 2 0 . 2 2 7 8 0 . 4 7 2 8 6 . 5 0 0 1 . 3 0 2 6 0 . 0 1 3 8 4 3 . 0 0 0 0 0 - 0 . 1 3 3 2 0 . 2 2 2 2 0 . 4 7 8 5 7 . 0 0 0 1 . 3 6 6 3 0 . 0 1 4 2 0 3 . 0 0 0 0 0 - 0 . 1 3 4 0 0 . 2 1 32 0 . 4 8 2 7 7 . 5 0 0 1 . 4 2 8 2 0 . 0 1 4 6 3 3 . 0 0 0 0 0 - 0 . 1 3 4 4 0 . 2 1 1 1 0 . 4 8 5 0 8 . 0 0 0 1 . 4 8 8 8 0 . 0 1 5 1 1 3 . 0 0 0 0 0 - 0 . 1 3 4 7 0 . 2 0 7 3 0 . 4 8 9 8 8 . 0 0 0 1 . 4 8 8 8 0 . 0 1 5 1 1 3 . 0 0 0 0 0 - 0 . 1 3 4 7 0 . 2 0 7 3 0 . 4 8 9 8 8 . 5 0 0 1 . 5 4 8 1 0 . 0 1 5 6 1 3 . 0 0 0 0 0 - 0 . 1 3 4 8 0 . 2 0 1 4 0 . 4 9 5 9 9 . 0 0 0 1 . 6 0 6 1 0 . 0 1 6 1 3 3 . 0 0 0 0 0 - 0 . 1 3 4 6 0 . 1 9 4 7 0 . 5 0 0 6 9 . 5 0 0 1 . 6 5 9 1 0 . 0 1 6 8 4 3 . 0 0 0 0 0 - 0 . 1 3 3 6 0 . 1 9 1 8 0 . 5 0 3 4

1 0 . 0 0 0 1 . 7 0 8 0 0 . 0 1 7 6 6 3 . 0 0 0 0 0 - 0 . 1 3 2 0 0 . 1 8 8 1 0 . 5 0 5 6 1 0 . 5 0 0 1 . 7 3 8 0 0 . 0 1 8 7 8 3 . 0 0 0 0 0 - 0 . 1 2 7 2 0 . 1 8 3 0 0 . 5 1 3 0 1 1 . 0 0 0 1 . 7 65 2 0 . 0 2 0 2 9 3 . 0 0 0 0 0 - 0 . 1 2 2 5 0 . 1 7 7 5 0 . 5 1 7 7 1 1 . 5 0 0 1 . 7 8 8 2 0 . 02 2 3 1 3 . 0 0 0 0 0 -o . 1 1 8 1 0 . 1 7 5 0 0 . 52 0 8 1 2 . 0 0 0 1 . 8 0 6 0 0 . 0 2 4 9 3 3 . 0 0 0 0 0 - 0 . 1 1 4 1 0 . 1 7 2 9 0 . 52 32 1 2 . 5 0 0 1 . 8 1 7 9 0 . 02 8 4 3 3 . 0 0 0 0 0 - 0 . 1 1 0 7 0 . 1 6 9 8 0 . 52 5 9 1 3 . 0 0 0 1 . 8 3 0 3 0 . 0 3 2 5 0 3 . 0 0 0 0 0 - 0 . 1 0 8 4 0 . 1 6 54 0 . 5 3 3 0 1 3 . 5 0 0 1 . 8 4 3 3 0 . 0 3 7 0 1 3 . 0 0 0 0 0 - 0 . 1 0 7 0 0 . 1 6 0 5 0 . 5 3 7 3 1 4 . 0 0 0 1 . 8 4 8 1 0 . 0 4 2 6 8 3 . 0 0 0 0 0 - 0 . 1 0 62 0 . 1 5 6 9 0 . 5 4 0 3 1 4 . 5 0 0 1 . 8 5 2 8 0 . 0 4 8 8 7 3 . 0 0 0 0 0 - 0 . 1 0 6 0 0 . 1 5 5 1 0 . 5 4 2 6 1 5 . 0 0 0 1 . 8 5 2 4 0 . 0 5 6 0 3 3 . 0 0 0 0 0 - 0 . 1 0 6 3 0 . 1 5 2 4 0 . 5 4 62 1 5 . 5 0 0 1 . 8 5 2 4 0 . 0 6 3 4 5 3 . 0 0 0 0 0 - 0 . 1 0 6 9 0 . 1 4 8 5 0 . 55 1 7 1 6 . 0 0 0 1 . 8 5 5 0 0 . 0 7 0 6 6 3 . 0 0 0 0 0 - 0 . 1 0 7 7 0 . 1 4 42 0 . 5 5 6 1

FFA TN 1 9 9 0 - 1 5 8 4 POL . W3_3 32_3 0_TU 1 ; 2

XFOI L Ve rsion 5 . 0

Calculated polar for : FFA-W3 -332

1 Reynolds numbe r fixed

xt rf = 0 . 0 1 0 ( suct ion ) 0 . 1 0 0 (pres sure ) Mach • 0 . 1 5 0 Re = 3 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xt r - - - - --- -------- --------- --------- -------- ------- -------- 6 . 0 0 0 0 0 - 0 . 3 4 1 7 0 0 . 0 3 9 0 5 3 . 0 0 0 0 0 - 0 . 0 3 3 6 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 5 . 5 0 0 0 0 - 0 . 3 11 3 0 0 . 0 3 6 6 5 3 . 0 0 0 0 0 - 0 . 0 3 3 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 5 . 0 0 0 0 0 - 0 . 2 8 0 1 0 0 . 0 3 4 5 5 3 . 0 0 0 0 0 - 0 . 0 3 3 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 4 . 50 0 0 0 - 0 . 2 4 8 5 0 0 . 0 3 2 6 0 3 . 0 0 0 0 0 - 0 . 0 3 3 7 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 4 . 0 0 0 0 0 - 0 . 2 2 2 2 0 0 . 0 3 0 3 8 3 . 0 0 0 0 0 - 0 . 0 3 3 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 5 0 0 0 0 - 0 . 2 1 2 0 0 0 . 0 2 8 5 6 3 . 0 0 0 0 0 - 0 . 0 2 9 3 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 0 0 0 0 0 - 0 . 1 7 6 3 0 0 . 0 2 6 7 8 3 . 0 0 0 0 0 - 0 . 0 3 0 0 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 2 . 5 0 0 0 0 - o . 1 3 0 1 0 0 . 0 2 5 4 5 3 . 0 0 0 0 0 - 0 . 0 3 1 8 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 2 . 0 0 0 0 0 - 0 . 0 7 7 0 0 0 . 0 2 4 0 8 3 . 0 0 0 0 0 - 0 . 0 3 4 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 5 0 0 0 0 - 0 . 0 1 7 5 0 0 . 0 2 3 1 3 3 . 0 0 0 0 0 - 0 . 0 3 8 4 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 0 0 0 0 0 0 . 0 4 8 1 0 0 . 0 2 2 2 0 3 . 0 0 0 0 0 - 0 . 0 4 2 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 0 . 5 0 0 0 0 0 . 1 1 7 3 0 0 . 0 2 1 5 1 3 . 0 0 0 0 0 - 0 . 0 4 7 7 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0

0 . 0 0 0 0 . 1 8 9 2 0 . 0 2 0 9 7 3 . 0 0 0 0 0 - 0 . 0 5 2 7 0 . 0 1 0 0 0 . 1 0 0 0 0 . 5 0 0 0 . 2 6 43 0 . 0 2 0 4 7 3 . 0 0 0 0 0 - 0 . 0 5 8 2 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 . 3 3 9 3 0 . 0 2 0 1 7 3 . 0 0 0 0 0 - 0 . 0 6 3 3 0 . 0 1 0 0 0 . 1 0 0 0 1. 5 0 0 0 . 4 1 5 7 0 . 0 1 9 9 1 3 . 0 0 0 0 0 - 0 . 0 6 8 7 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 4 9 1 6 0 . 0 1 9 7 7 3 . 0 0 0 0 0 - 0 . 0 7 3 7 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 5 6 7 4 0 . 0 1 9 7 1 3 . 0 0 0 0 0 - 0 . 0 7 8 7 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 4 2 4 0 . 0 1 9 7 4 3 . 0 0 0 0 0 - 0 . 0 8 3 4 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 7 1 6 0 0 . 0 1 9 8 5 3 . 0 0 0 0 0 - 0 . 0 8 7 7 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 7 8 8 0 0 . 0 2 0 0 4 3 . 0 0 0 0 0 - 0 . 0 9 1 7 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 8 5 7 5 0 . 0 2 0 32 3 . 0 0 0 0 0 - 0 . 0 9 52 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 9 2 3 4 0 . 0 2 0 7 0 3 . 0 0 0 0 0 - 0 . 0 9 7 9 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 9 8 3 9 0 . 02 1 2 4 3 . 0 0 0 0 0 - 0 . 0 9 97 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 1 . 0 1 8 5 0 . 0 2 2 0 7 3 . 0 0 0 0 0 - 0 . 0 9 6 7 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 1 . 0 5 0 1 0 . 0 2 3 4 6 3 . 0 0 0 0 0 - 0 . 0 9 3 9 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 1 . 0 8 4 6 0 . 0 2 52 2 3 . 0 0 0 0 0 - 0 . 0 92 4 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 1 . 1 1 3 9 0 . 0 2 7 5 3 3 . 0 0 0 0 0 - 0 . 0 9 1 0 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 1 . 1 3 8 9 0 . 0 3 0 5 0 3 . 0 0 0 0 0 - 0 . 0 9 0 1 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 1 5 9 8 0 . 0 3 4 1 6 3 . 0 0 0 0 0 - 0 . 0 8 9 7 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 1 7 9 5 0 . 0 3 8 4 9 3 . 0 0 0 0 0 - 0 . 0 9 0 1 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 1 9 7 3 0 . 0 4 3 5 4 3 . 0 0 0 0 0 - 0 . 0 9 1 1 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 2 12 9 0 . 0 4 9 3 0 3 . 0 0 0 0 0 - 0 . 0 92 6 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 2 2 7 5 0 . 0 55 3 7 3 . 0 0 0 0 0 - 0 . 0 9 4 3 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 2 3 7 2 0 . 0 6 2 3 6 3 . 0 0 0 0 0 - 0 . 0 9 62 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 2 4 57 0 . 0 6 97 3 3 . 0 0 0 0 0 - 0 . 0 9 8 3 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 2 5 2 2 0 . 0 7 7 5 8 3 . 0 0 0 0 0 - 0 . 1 0 0 5 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 2 5 6 4 0 . 0 8 5 9 3 3 . 0 0 0 0 0 - 0 . 1 0 2 8 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 2 5 8 3 0 . 0 9 4 7 9 3 . 0 0 0 0 0 - 0 . 1 0 52 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 2 5 7 7 0 . 1 0 4 1 1 3 . 0 0 0 0 0 - 0 . 1 0 7 8 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 0 0 0 1 . 2 5 6 4 0 . 1 1 3 9 0 3 . 0 0 0 0 0 - 0 . 1 1 0 5 0 . 0 1 0 0 0 . 1 0 0 0 1 4 . 5 0 0 1 . 2 5 7 5 0 . 1 2 3 4 2 3 . 0 0 0 0 0 - 0 . 1 1 32 0 . 0 1 0 0 0 . 1 0 0 0 1 5 . 0 0 0 1 . 2 5 5 1 0 . 1 3 4 0 2 3 . 0 0 0 0 0 - 0 . 1 1 6 3 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 8 5

XFOI L Ve rs ion 5 . 0

Calculated polar for : V3 6 0NR1

1 Reynolds number fixed

xt rf = 1 . 0 0 0 ( suct ion) 1 . 0 0 0 (pre s sure ) Mach ...

a lpha - - - ----- 4 . 0 0 0 - 3 . 5 0 0 - 3 . 0 0 0 - 2 . 5 0 0 - 2 . 0 0 0 - 1 . 5 0 0 - 1 . 0 0 0 - 0 . 5 0 0

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 1 2 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0

0 . 1 5 0

CL --------- 0 . 2 5 0 9 - 0 . 1 8 0 1 - 0 . 1 0 3 2 - 0 . 0 2 6 2

0 . 0 5 9 0 0 . 1 4 1 4 0 . 2 2 2 0 0 . 3 0 8 3 0 . 3 8 9 4 0 . 4 6 8 1 0 . 5 4 9 7 0 . 6 2 7 6 0 . 7 0 1 0 0 . 7 7 0 9 0 . 8 4 32 0 . 9 1 1 4 0 . 97 62 0 . 9 7 62 1 . 0 3 6 8 1 . 0 9 9 5 1 . 1 5 7 8 1 . 1 9 7 9 1 . 1 9 7 9 1 . 2 3 0 4 1 . 2 6 1 2 1 . 2 9 9 5 1 . 3 3 0 7 1 . 3 3 0 7 1 . 3 5 5 4 1 . 3 7 3 6 1 . 3 8 2 0 1 . 4 0 62 1 . 4 2 5 9 1 . 4 3 9 9 1 . 4 4 7 0 1 . 4 3 8 0 1 . 4 5 5 0 1 . 4 6 6 3 1 . 4 7 2 3 1 . 4 7 1 0 1 . 4 5 7 5 1 . 4 6 8 1

Re = 1 . 0 0 0 e 6 Ncr it

CD Re ( CL ) CM ------- - - --------- --------

0 . 0 1 9 5 1 1 . 0 0 0 0 0 - 0 . 0 4 4 3 0 . 0 1 8 3 0 1 . 0 0 0 0 0 - 0 . 0 5 0 3 0 . 0 1 7 4 6 1 . 0 0 0 0 0 - 0 . 0 5 6 5 0 . 0 1 6 9 9 1 . 0 0 0 0 0 - 0 . 0 62 0 0 . 0 1 6 3 3 1 . 0 0 0 0 0 - 0 . 0 6 9 5 0 . 0 1 5 9 8 1 . 0 0 0 0 0 - 0 . 0 7 5 7 0 . 0 1 5 7 8 1 . 0 0 0 0 0 - 0 . 0 8 12 0 . 0 1 5 5 0 1 . 0 0 0 0 0 - 0 . 0 8 8 2 0 . 0 1 5 4 2 1 . 0 0 0 0 0 - 0 . 0 9 3 7 0 . 0 1 5 4 3 1 . 0 0 0 0 0 - 0 . 0 9 8 4 0 . 0 1 5 4 3 1 . 0 0 0 0 0 - 0 . 1 0 3 9 0 . 0 1 552 1 . 0 0 0 0 0 - 0 . 1 0 8 4 0 . 0 1 5 7 2 1 . 0 0 0 0 0 - 0 . 1 1 1 9 0 . 0 1 6 0 2 1 . 0 0 0 0 0 - 0 . 1 1 4 5 0 . 0 1 62 7 1 . 0 0 0 0 0 - 0 . 1 1 7 8 0 . 0 1 6 5 7 1 . 0 0 0 0 0 - 0 . 1 2 0 2 0 . 0 1 6 9 9 1 . 0 0 0 0 0 - 0 . 1 2 1 8 0 . 0 1 6 9 9 1 . 0 0 0 0 0 - 0 . 12 1 8 0 . 0 1 7 5 5 1 . 0 0 0 0 0 - 0 . 1 2 2 7 0 . 0 1 8 0 1 1 . 0 0 0 0 0 - 0 . 12 4 1 0 . 0 1 8 5 7 1 . 0 0 0 0 0 - 0 . 1 2 4 7 0 . 0 1 9 4 1 1 . 0 0 0 0 0 - 0 . 1 2 2 2 0 . 0 1 9 4 1 1 . 0 0 0 0 0 - 0 . 1 2 2 2 0 . 0 2 0 7 6 1 . 0 0 0 0 0 - 0 . 1 1 8 8 0 . 0 2 2 5 4 1 . 0 0 0 0 0 - 0 . 1 1 5 9 0 . 0 2 4 2 1 1 . 0 0 0 0 0 - 0 . 1 1 4 8 0 . 0 2 6 4 6 1 . 0 0 0 0 0 - 0 . 1 1 32 0 . 0 2 6 4 6 1 . 0 0 0 0 0 - 0 . 1 1 32 0 . 0 2 9 3 9 1 . 0 0 0 0 0 - 0 . 1 1 1 7 0 . 0 3 3 1 9 1 . 0 0 0 0 0 - 0 . 1 1 0 5 0 . 0 3 8 3 6 1 . 0 0 0 0 0 - 0 . 1 0 9 7 0 . 0 4 2 52 1 . 0 0 0 0 0 - 0 . 1 1 0 2 0 . 0 4 7 4 5 1 . 0 0 0 0 0 - 0 . 1 1 0 9 0 . 0 5 2 9 9 1 . 0 0 0 0 0 - 0 . 1 1 1 5 0 . 0 5 9 5 6 1 . 0 0 0 0 0 - 0 . 1 1 2 3 0 . 0 6 8 1 5 1 . 0 0 0 0 0 - 0 . 1 1 3 2 0 . 0 7 3 9 0 1 . 0 0 0 0 0 - 0 . 1 1 4 3 0 . 0 8 0 5 5 1 . 0 0 0 0 0 - 0 . 1 1 5 7 0 . 0 8 8 0 7 1 . 0 0 0 0 0 - 0 . 1 1 7 3 0 . 0 9 6 6 8 1 . 0 0 0 0 0 - 0 . 1 1 9 0 0 . 1 0 7 0 9 1 . 0 0 0 0 0 - 0 . 12 1 0 0 . 1 1 4 3 9 1 . 0 0 0 0 0 - 0 . 1 2 2 6

POL . W3_3 6 0_1 0_9 ; 1

9 . 0 0 0

S xtr P xt r ------- -------0 . 4 1 7 2 0 . 37 0 0 0 . 4 0 5 3 0 . 3 8 0 3 0 . 3 9 7 5 0 . 3 8 6 9 0 . 3 8 4 0 0 . 3 9 1 7 0 . 3 7 6 9 0 . 4 0 1 7 0 . 3 6 4 7 0 . 4 0 8 3 0 . 3 5 8 4 0 . 4 12 3 0 . 3 4 8 0 0 . 42 2 5 0 . 3 3 9 4 0 . 42 8 0 0 . 3 3 3 6 0 . 4 3 2 0 0 . 32 3 8 0 . 4 4 0 3 0 . 3 1 7 6 0 . 4 4 6 3 0 . 3 1 1 7 0 . 4 5 0 3 0 . 3 0 3 5 0 . 4 5 3 8 0 . 2 9 7 3 0 . 4 6 2 0 0 . 2 9 3 4 0 . 4 6 6 9 0 . 2 8 7 2 0 . 4 7 0 5 0 . 2 8 7 2 0 . 4 7 0 5 0 . 2 7 9 1 0 . 4 7 3 9 0 . 2 7 5 7 0 . 4 8 02 0 . 2 7 2 4 0 . 4 8 5 8 0 . 2 6 7 6 0 . 4 8 9 3 0 . 2 6 7 6 0 . 4 8 9 3 0 . 2 6 1 7 0 . 4 92 5 0 . 2 5 6 5 0 . 4 9 5 1 0 . 2 5 4 3 0 . 5 0 1 4 0 . 2 5 1 5 0 . 5 0 6 3 0 . 2 5 1 5 0 . 5 0 6 3 0 . 2 4 8 0 0 . 5 0 9 9 0 . 2 4 1 8 0 . 5 1 2 7 0 . 2 3 6 4 0 . 5 1 5 1 0 . 2 3 4 3 0 . 5 1 9 0 0 . 2 3 1 8 0 . 52 5 4 0 . 2 2 8 5 0 . 52 8 9 0 . 2 2 3 5 0 . 5 3 1 7 0 . 2 1 6 8 0 . 5 3 4 0 0 . 2 1 4 6 0 . 5 3 6 4 0 . 2 1 2 1 0 . 5 4 0 6 0 . 2 0 8 6 0 . 5 4 6 4 0 . 2 0 32 0 . 5 4 9 6 0 . 1 9 7 1 0 . 5 5 2 0 0 . 1 9 5 0 0 . 5 5 4 6

FFA TN 1 9 9 0 - 1 5 8 6 POL . W3_3 6 0_1 0_TU 1 ; 1

XFOI L Version 5 . 0

Calculated pol a r for : V3 6 0NR1

1 Reynolds number fixed

xt rf = 0 . 0 1 0 ( suct ion ) 0 . 1 0 0 (pres su re ) Mach - 0 . 1 5 0 Re = 1 . 0 0 0 e 6 Ncrit = 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xtr ------- -------- - -------- --------- -------- ------- -------

2 . 0 00 0 . 32 0 0 0 . 0 2 8 8 4 1 . 0 0 0 0 0 - 0 . 0 3 1 0 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 00 0 . 3 7 3 7 0 . 0 2 92 8 1 . 0 0 0 0 0 - 0 . 0 3 4 5 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 42 6 4 0 . 0 3 0 12 1 . 0 0 0 0 0 - 0 . 0 3 8 0 0 . 0 1 0 0 0 . 1 0 0 0 3 . 50 0 0 . 4 7 8 5 0 . 0 3 1 3 5 1 . 0 0 0 0 0 - 0 . 0 4 2 0 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 0 . 52 8 0 0 . 0 3 3 0 9 1 . 0 0 0 0 0 - 0 . 0 4 6 0 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 5 7 5 4 0 . 0 3 5 3 3 1 . 0 0 0 0 0 - 0 . 0 5 0 2 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 62 0 6 0 . 0 3 8 1 1 1 . 0 0 0 0 0 - 0 . 0 5 4 6 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 6 6 3 0 0 . 0 4 1 4 7 1 . 0 0 0 0 0 - 0 . 0 5 9 2 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 7 0 2 3 0 . 0 4 5 3 9 1 . 0 0 0 0 0 - 0 . 0 6 3 8 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 7 0 2 3 0 . 0 4 5 3 9 1 . 0 0 0 0 0 - 0 . 0 6 3 8 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 0 . 7 3 9 4 0 . 0 4 9 8 2 1 . 0 0 0 0 0 - 0 . 0 6 8 4 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 0 . 7 7 2 9 0 . 0 5 4 8 0 1 . 0 0 0 0 0 - 0 . 0 7 2 9 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 0 . 8 0 2 7 0 . 0 6 0 2 9 1 . 0 0 0 0 0 - 0 . 0 7 7 2 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 0 . 8 2 9 4 0 . 0 6 6 22 1 . 0 0 0 0 0 - 0 . 0 8 12 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 0 . 8 2 9 4 0 . 0 6 62 2 1 . 0 0 0 0 0 - 0 . 0 8 12 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 0 . 8 5 2 5 0 . 0 7 2 5 9 1 . 0 0 0 0 0 - 0 . 0 8 4 9 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 0 . 8 7 2 1 0 . 0 7 9 3 9 1 .. 0 0 0 0 0 - 0 . 0 8 8 4 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 0 . 8 8 9 3 0 . 0 8 6 6 2 1 . 0 0 0 0 0 - 0 . 0 9 1 8 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 0 . 9 0 4 7 0 . 0 9 4 2 8 1 . 0 0 0 0 0 - 0 . 0 9 52 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 0 . 9 1 8 4 0 . 1 0 2 3 4 1 . 0 0 0 0 0 - 0 . 0 9 8 6 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 0 . 9 3 0 5 0 . 1 1 0 7 1 1 . 0 0 0 0 0 - 0 . 1 0 2 0 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 0 . 9 4 2 3 0 . 1 1 9 2 7 1 . 0 0 0 0 0 - 0 . 1 0 5 3 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 0 . 9 5 2 3 0 . 1 2 8 4 0 1 . 0 0 0 0 0 - 0 . 1 0 8 7 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 0 . 9 6 1 0 0 . 1 3 8 0 3 1 . 0 0 0 0 0 - 0 . 1 1 2 3 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 0 . 9 7 0 3 0 . 1 4 7 6 1 1 . 0 0 0 0 0 - 0 . 1 1 5 8 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 0 . 9 7 7 9 0 . 1 5 7 8 1 1 . 0 0 0 0 0 - 0 . 1 1 9 3 0 . 0 1 0 0 0 . 1 0 0 0

FFA TN 1 9 9 0 - 1 5 8 7 POL . W3_3 6 0_20_9 ; 2

XFOI L Ve rs ion 5 . 0

Calculated polar for : V3 60NR1

1 Reynolds number fixed

xt rf • 1 . 0 0 0 ( suct ion) 1 . 0 0 0 (pressure ) Mach • 0 . 1 5 0 Re = 2 . 0 0 0 e 6 Ncr it 9 . 0 0 0

a lpha CL CD Re (CL) CM S xt r P xt r -- ----- -------- --------- --------- -------- ------- ----- --- 6 . 0 0 0 0 0 - 0 . 5 0 1 2 0 0 . 0 1 9 5 7 2 . 0 0 0 0 0 - 0 . 0 3 7 4 0 0 . 4 3 1 2 0 0 . 32 8 1 0 - 5 . 5 0 0 0 0 - 0 . 4 3 8 2 0 0 . 0 1 8 0 6 2 . 0 0 0 0 0 - 0 . 0 42 4 0 0 . 4 1 6 4 0 0 . 3 3 7 2 0 - 5 . 0 0 0 0 0 - 0 . 3 67 3 0 0 . 0 1 6 8 8 2 . 0 0 0 0 0 - 0 . 0 4 8 1 0 0 . 4 1 1 0 0 0 . 3 4 1 1 0 - 4 . 5 0 0 0 0 - 0 . 2 8 9 7 0 0 . 0 1 6 0 0 2 . 0 0 0 0 0 - 0 . 0 5 4 4 0 0 . 4 0 0 9 0 0 . 3 4 9 6 0 - 4 . 0 0 0 0 0 - 0 . 2 0 9 3 0 0 . 0 1 5 2 8 2 . 0 0 0 0 0 - 0 . 0 6 0 8 0 0 . 3 8 6 3 0 0 . 3 5 9 2 0 - 3 . 5 0 0 0 0 - 0 . 1 2 4 3 0 0 . 0 1 4 5 6 2 . 0 0 0 0 0 - 0 . 0 6 8 2 0 0 . 3 7 9 6 0 0 . 3 6 6 1 0 - 3 . 0 0 0 0 0 - 0 . 0 4 4 0 0 0 . 0 1 4 2 6 2 . 0 0 0 0 0 - 0 . 0 7 3 6 0 0 . 3 6 9 2 0 0 . 3 6 8 9 0 - 2 . 5 0 0 0 0 0 . 0 4 3 1 0 0 . 0 1 3 7 8 2 . 0 0 0 0 0 - 0 . 0 8 0 8 0 0 . 3 5 6 5 0 0 . 3 7 9 3 0 - 2 . 0 0 0 0 0 0 . 12 8 8 0 0 . 0 1 3 4 1 2 . 0 0 0 0 0 - 0 . 0 8 7 4 0 0 . 3 5 1 8 0 0 . 3 8 9 0 0 - 1 . 5 0 0 0 0 0 . 2 1 1 8 0 0 . 0 1 3 2 2 2 . 0 0 0 0 0 - 0 . 0 9 3 2 0 0 . 3 4 3 6 0 0 . 3 9 3 6 0 - 1 . 0 0 0 0 0 0 . 2 9 3 8 0 0 . 0 1 3 0 7 2 . 0 0 0 0 0 - 0 . 0 9 8 6 0 0 . 32 9 5 0 0 . 3 9 8 3 0 - 0 . 5 0 0 0 0 0 . 3 7 7 4 0 0 . 0 1 2 9 1 2 . 0 0 0 0 0 - 0 . 1 0 4 4 0 0 . 32 5 0 0 0 . 4 0 8 2 0

0 . 0 0 0 0 . 4 5 8 4 0 . 0 1 2 8 5 2 . 0 0 0 0 0 - 0 . 1 0 9 5 0 . 3 1 9 5 0 . 4 1 5 6 0 . 5 0 0 0 . 5 3 7 2 0 . 0 1 2 8 5 2 . 0 0 0 0 0 - 0 . 1 1 4 1 0 . 3 1 0 9 0 . 42 0 8 1 . 0 0 0 0 . 6 1 1 1 0 . 0 1 2 9 6 2 . 0 0 0 0 0 - 0 . 1 1 7 3 0 . 3 0 1 1 0 . 4 2 3 3 1 . 5 0 0 0 . 6 8 7 5 0 . 0 1 3 0 2 2 . 0 0 0 0 0 - 0 . 1 2 1 2 0 . 2 9 7 6 0 . 4 3 1 9 2 . 0 0 0 0 . 7 6 0 4 0 . 0 1 3 1 9 2 . 0 0 0 0 0 - 0 . 12 4 3 0 . 2 92 6 0 . 4 3 9 8 2 . 5 0 0 0 . 8 3 1 8 0 . 0 1 3 3 9 2 . 0 0 0 0 0 - 0 . 12 7 0 0 . 2 8 6 4 0 . 4 4 4 8 3 . 0 0 0 0 . 9 0 1 4 0 . 0 1 3 62 2 . 0 0 0 0 0 - 0 . 12 9 3 0 . 2 7 8 6 0 . 4 4 8 7 3 . 5 0 0 0 . 9 6 8 8 0 . 0 1 3 9 3 2 . 0 0 0 0 0 - 0 . 1 3 1 2 0 . 2 7 1 8 0 . 4 5 0 7 4 . 0 0 0 1 . 0 3 9 1 0 . 0 1 4 1 4 2 . 0 0 0 0 0 - 0 . 1 3 3 7 0 . 2 6 9 2 0 . 4 5 8 3 4 . 5 0 0 1 . 1 0 6 3 0 . 0 1 4 4 6 2 . 0 0 0 0 0 - 0 . 1 3 5 6 0 . 2 6 5 7 0 . 4 6 5 4 5 . 0 0 0 1 . 1 7 1 2 0 . 0 1 4 8 3 2 . 0 0 0 0 0 - 0 . 1 3 7 0 0 . 2 6 0 9 0 . 4 7 1 3 5 . 5 0 0 1 . 2 3 4 4 0 . 0 1 52 3 2 . 0 0 0 0 0 - 0 . 1 3 8 1 0 . 2 5 4 8 0 . 4 7 4 6 6 . 0 0 0 1 . 2 9 4 8 0 . 0 1 5 7 0 2 . 0 0 0 0 0 - 0 . 1 3 8 6 0 . 2 4 8 3 0 . 4 7 6 9 6 . 5 0 0 1 . 3 52 7 0 . 0 1 62 3 2 . 0 0 0 0 0 - 0 . 1 3 8 8 0 . 2 4 4 5 0 . 4 7 8 7 7 . 0 0 0 1 . 4 1 1 3 0 . 0 1 6 7 4 2 . 0 0 0 0 0 - 0 . 1 3 92 0 . 2 4 2 5 0 . 4 8 5 4 7 . 5 0 0 1 . 4 62 5 0 . 0 1 7 4 5 2 . 0 0 0 0 0 - 0 . 1 3 8 3 0 . 2 3 9 6 0 . 4 9 3 1 8 . 0 0 0 1 . 4 8 5 2 0 . 0 1 8 7 6 2 . 0 0 0 0 0 - 0 . 1 3 2 7 0 . 2 3 6 3 0 . 4 9 7 4 8 . 5 0 0 1 . 5 1 8 4 0 . 0 2 0 2 0 2 . 0 0 0 0 0 - 0 . 12 9 5 0 . 2 3 1 7 0 . 5 0 0 8 9 . 0 0 0 1 . 5 4 8 4 0 . 02 1 9 9 2 . 0 0 0 0 0 - 0 . 1 2 6 5 0 . 2 2 6 6 0 . 5 0 3 3 9 . 5 0 0 1 . 5 7 0 1 0 . 0 2 4 4 9 2 . 0 0 0 0 0 - 0 . 1 2 3 2 0 . 2 2 1 4 0 . 5 0 5 3

1 0 . 0 0 0 1 . 5 9 3 0 0 . 0 2 7 2 3 2 . 0 0 0 0 0 - 0 . 12 0 8 0 . 2 1 9 5 0 . 5 0 7 1 1 0 . 5 0 0 1 . 6 1 8 0 0 . 0 3 0 2 2 2 . 0 0 0 0 0 - 0 . 1 1 9 4 0 . 2 1 7 6 0 . 5 1 3 1 1 1 . 0 0 0 1 . 6 3 5 1 0 . 0 3 4 2 1 2 . 0 0 0 0 0 - 0 . 1 1 8 1 0 . 2 1 5 3 0 . 5 1 9 0 1 1 . 5 0 0 1 . 6 4 7 5 0 . 0 3 9 0 3 2 . 0 0 0 0 0 - 0 . 1 1 7 3 0 . 2 1 2 2 0 . 52 3 7 1 2 . 0 0 0 1 . 6 6 0 2 0 . 0 4 4 1 4 2 . 0 0 0 0 0 - 0 . 1 1 6 9 0 . 2 0 7 9 0 . 52 7 3 1 2 . 5 0 0 1 . 6 7 0 6 0 . 0 4 9 7 5 2 . 0 0 0 0 0 - 0 . 1 1 6 9 0 . 2 0 2 8 0 . 5 3 0 1 1 3 . 0 0 0 1 . 6 7 3 1 0 . 0 5 6 3 8 2 . 0 0 0 0 0 - 0 . 1 1 7 0 0 . 1 9 7 4 0 . 5 3 2 3 1 3 . 5 0 0 1 . 6 7 9 3 0 . 0 62 8 7 2 . 0 0 0 0 0 - 0 . 1 1 7 4 0 . 1 9 5 7 0 . 53 4 4 1 4 . 0 0 0 1 . 6 8 5 0 0 . 0 6 9 63 2 . 0 0 0 0 0 - 0 . 1 1 8 0 0 . 1 9 3 7 0 . 5 3 5 7 1 4 . 5 0 0 1 . 6 8 4 9 0 . 0 7 7 4 3 2 . 0 0 0 0 0 - 0 . 1 1 9 1 0 . 1 9 1 1 0 . 5 4 0 8 1 5 . 0 0 0 1 . 6 8 3 9 0 . 0 8 5 3 3 2 . 0 0 0 0 0 - 0 . 12 0 1 0 . 1 8 7 4 0 . 5 4 6 3 1 5 . 5 0 0 1 . 67 9 5 0 . 0 9 3 97 2 . 0 0 0 0 0 - 0 . 1 2 1 5 0 . 1 8 2 4 0 . 5 5 0 9 1 6 . 0 0 0 1 . 6 6 7 2 0 . 1 0 4 1 4 2 . 0 0 0 0 0 - 0 . 1 2 3 2 0 . 17 6 7 0 . 5 5 4 4

FFA TN 1 9 9 0 - 1 5 8 8

XFOI L Ve rs ion 5 . 0

Calculated polar for : V3 6 0NR1

1 Reynolds number fixed

xtrf = 1 . 0 0 0 ( suct ion) 1 . 0 0 0 (pres sure ) Mach =

alpha -------- 4 . 0 0 0 - 3 . 50 0 - 3 . 0 0 0 - 2 . 5 0 0 - 2 . 0 0 0 - 1 . 5 0 0 - 1 . 0 0 0 - 0 . 5 0 0

0 . 0 0 0 0 . 5 0 0 1 . 0 0 0 1 . 5 0 0 2 . 0 0 0 2 . 5 0 0 3 . 0 0 0 3 . 5 0 0 4 . 0 0 0 4 . 0 0 0 4 . 5 0 0 5 . 0 0 0 5 . 5 0 0 6 . 0 0 0 6 . 0 0 0 6 . 5 0 0 7 . 0 0 0 7 . 5 0 0 8 . 0 0 0 8 . 0 0 0 8 . 5 0 0 9 . 0 0 0 9 . 5 0 0

1 0 . 0 0 0 1 0 . 5 0 0 1 1 . 0 0 0 1 1 . 5 0 0 1 2 . 0 0 0 12 . 5 0 0 1 3 . 0 0 0 1 3 . 5 0 0 1 4 . 0 0 0 1 4 . 5 0 0 1 5 . 0 0 0 1 5 . 5 0 0 1 6 . 0 0 0

0 . 1 5 0

CL --------- 0 . 1 8 3 6 - 0 . 0 9 9 4 - 0 . 0 1 3 1

0 . 0 7 3 9 0 . 1 5 8 5 0 . 2 4 3 0 0 . 32 6 5 0 . 4 0 8 0 0 . 4 8 6 0 0 . 5 6 2 4 0 . 6 3 6 1 0 . 7 1 0 2 0 . 7 8 3 1 0 . 8 5 4 0 0 . 9 2 4 2 0 . 9 9 43 1 . 0 6 2 8 1 . 0 6 2 8 1 . 1 2 9 9 1 . 1 9 5 8 1 . 2 6 1 7 1 . 3 2 6 0 1 . 3 2 6 0 1 . 3 8 7 8 1 . 4 4 6 9 1 . 5 0 4 0 1 . 5 5 8 6 1 . 5 5 8 6 1 . 5 9 32 1 . 62 4 3 1 . 6 5 5 1 1 . 6 7 7 7 1 . 6 9 9 4 1 . 7 1 9 5 1 . 7 3 6 5 1 . 7 5 0 9 1 . 7 6 4 3 1 . 7 7 3 3 1 . 7 7 4 5 1 . 7 8 2 9 1 . 7 8 2 3 1 . 7 8 6 8 1 . 7 8 4 2 1 . 7 7 7 2

Re = 3 . 0 0 0 e 6 Ncr it

CD Re (CL) CM ------ - -- --------- --- - -- - -

0 . 0 1 3 9 4 3 . 0 0 0 0 0 - 0 . 0 6 8 4 0 . 0 1 3 4 8 3 . 0 0 0 0 0 - 0 . 0 7 4 9 0 . 0 1 3 0 6 3 . 0 0 0 0 0 - 0 . 0 8 1 8 0 . 0 12 6 8 3 . 0 0 0 0 0 - 0 . 0 8 8 6 0 . 0 12 4 4 3 . 0 0 0 0 0 - 0 . 0 9 4 8 0 . 0 12 2 2 3 . 0 0 0 0 0 - 0 . 1 0 0 7 0 . 0 12 0 6 3 . 0 0 0 0 0 - 0 . 1 0 6 4 0 . 0 1 1 9 8 3 . 0 0 0 0 0 - 0 . 1 1 1 6 0 . 0 1 1 9 7 3 . 0 0 0 0 0 - 0 . 1 1 5 8 0 . 0 1 2 0 1 3 . 0 0 0 0 0 - 0 . 1 1 9 6 0 . 0 12 1 4 3 . 0 0 0 0 0 - 0 . 1 2 2 8 0 . 0 1 2 2 3 3 . 0 0 0 0 0 - 0 . 1 2 6 1 0 . 0 1 2 3 6 3 . 0 0 0 0 0 - 0 . 1 2 9 0 0 . 0 1 2 5 5 3 . 0 0 0 0 0 - 0 . 1 3 1 6 0 . 0 1 2 7 6 3 . 0 0 0 0 0 - 0 . 1 3 4 0 0 . 0 1 2 9 5 3 . 0 0 0 0 0 - 0 . 1 3 6 3 0 . 0 1 3 2 1 3 . 0 0 0 0 0 - 0 . 1 3 8 4 0 . 0 1 32 1 3 . 0 0 0 0 0 - 0 . 1 3 8 4 0 . 0 1 3 5 0 3 . 0 0 0 0 0 - 0 . 1 4 0 1 0 . 0 1 3 8 4 3 . 0 0 0 0 0 - 0 . 1 4 1 6 0 . 0 1 4 1 6 3 . 0 0 0 0 0 - 0 . 1 4 3 1 0 . 0 1 4 5 1 3 . 0 0 0 0 0 - 0 . 1 4 4 3 0 . 0 1 4 5 1 3 . 0 0 0 0 0 - 0 . 1 4 4 3 0 . 0 1 4 9 5 3 . 0 0 0 0 0 - 0 . 1 4 5 1 0 . 0 1 5 4 4 3 . 0 0 0 0 0 - 0 . 1 4 5 4 0 . 0 1 6 0 0 3 . 0 0 0 0 0 - 0 . 1 4 5 4 0 . 0 1 6 6 0 3 . 0 0 0 0 0 - 0 . 1 4 4 9 0 . 0 1 6 6 0 3 . 0 0 0 0 0 - 0 . 1 4 4 9 0 . 0 1 7 5 2 3 . 0 0 0 0 0 - 0 . 1 4 1 0 0 . 0 1 8 8 4 3 . 0 0 0 0 0 - 0 . 1 3 7 0 0 . 0 2 0 3 8 3 . 0 0 0 0 0 - 0 . 1 3 3 5 0 . 0 2 2 6 1 3 . 0 0 0 0 0 - 0 . 1 2 9 8 0 . 0 2 5 2 5 3 . 0 0 0 0 0 - 0 . 1 2 6 9 0 . 0 2 8 3 5 3 . 0 0 0 0 0 - 0 . 12 4 5 0 . 0 3 2 0 8 3 . 0 0 0 0 0 - 0 . 1 2 2 7 0 . 0 3 6 4 7 3 . 0 0 0 0 0 - 0 . 12 1 6 0 . 0 4 1 33 3 . 0 0 0 0 0 - 0 . 1 2 0 9 0 . 0 4 6 9 4 3 . 0 0 0 0 0 - 0 . 12 0 7 0 . 0 5 37 6 3 . 0 0 0 0 0 - 0 . 1 2 0 8 0 . 0 5 9 9 7 3 . 0 0 0 0 0 - 0 . 1 2 1 1 0 . 0 6 7 5 4 3 . 0 0 0 0 0 - 0 . 1 2 1 8 0 . 0 7 4 5 6 3 . 0 0 0 0 0 - 0 . 1 2 2 6 0 . 0 8 2 6 4 3 . 0 0 0 0 0 - 0 . 1 2 3 5 0 . 0 9 1 62 3 . 0 0 0 0 0 - 0 . 12 4 8

POL . W3_3 6 0_3 0_9 ; 1

9 . 0 0 0

S xt r P xt r ------- -------0 . 3 6 9 3 0 . 3 4 6 6 0 . 3 6 0 8 0 . 3 5 0 2 0 . 3 5 2 4 0 . 3 6 0 0 0 . 3 4 1 2 0 . 3 6 8 0 0 . 3 3 4 3 0 . 37 1 5 0 . 3 2 3 3 0 . 3 8 2 8 0 . 3 1 7 7 0 . 3 8 8 6 0 . 3 1 1 5 0 . 3 9 3 0 0 . 2 9 9 8 0 . 4 0 2 2 0 . 2 9 6 3 0 . 4 0 9 1 0 . 2 9 1 1 0 . 4 1 2 3 0 . 2 8 32 0 . 4 2 0 2 0 . 2 7 7 3 0 . 4 2 8 1 0 . 2 7 3 4 0 . 4 3 1 8 0 . 2 6 8 0 0 . 4 3 6 0 0 . 2 6 1 1 0 . 4 4 5 1 0 . 2 5 6 0 0 . 4 4 9 8 0 . 2 5 6 0 0 . 4 4 9 8 0 . 2 5 33 0 . 452 8 0 . 2 4 9 1 0 . 4 5 6 3 0 . 2 4 3 3 0 . 4 6 4 5 0 . 2 3 7 3 0 . 4 6 92 0 . 2 3 7 3 0 . 4 6 92 0 . 2 3 5 0 0 . 4 7 2 4 0 . 2 3 2 3 0 . 4 7 4 4 0 . 2 2 8 4 0 . 4 8 0 6 0 . 2 2 3 3 0 . 4 8 6 3 0 . 2 2 3 3 0 . 4 8 6 3 0 . 2 1 8 4 0 . 4 9 0 2 0 . 2 1 6 3 0 . 4 9 3 4 0 . 2 1 4 7 0 . 4 9 52 0 . 2 1 1 5 0 . 4 9 9 0 0 . 2 0 7 8 0 . 5 0 4 5 0 . 2 0 3 4 0 . 5 0 9 0 0 . 1 9 8 8 0 . 5 1 2 7 0 . 1 9 7 0 0 . 5 1 4 9 0 . 1 9 5 4 0 . 5 1 6 5 0 . 1 92 9 0 . 52 1 1 0 . 1 8 8 1 0 . 52 6 1 0 . 1 8 3 4 0 . 5 3 1 0 0 . 1 7 9 0 0 . 53 3 6 0 . 1 7 7 8 0 . 5 3 5 8 0 . 1 7 5 8 0 . 5 3 7 3 0 . 1 7 2 7 0 . 5 4 1 3

FFA TN 1 9 9 0- 1 5 8 9 POL . W3_3 6 0_3 0_TU1 ; 2

XFOI L Version 5 . 0

Calculated pola r for : FFA-W3- 3 6 0

l Reynolds number fixed

xtrf • 0 . 0 1 0 ( suct i on ) 0 . 1 0 0 (pressure ) Mach • 0 . 1 5 0 Re • 3 . 0 0 0 e 6 Ncrit • 9 . 0 0 0

alpha CL CD Re (CL) CM S xt r P xt r ------- -------- --------- --------- -------- ------- - -- - - --- 6 . 0 0 0 0 0 - 0 . 1 9 1 6 0 0 . 0 4 2 9 5 3 . 0 0 0 0 0 - 0 . 0 4 63 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 5 . 5 0 0 0 0 - 0 . 1 5 9 1 0 0 . 0 4 0 7 8 3 . 0 0 0 0 0 - 0 . 0 4 6 6 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 5 . 0 0 0 0 0 - 0 . 1 3 0 9 0 0 . 0 3 8 2 4 3 . 0 0 0 0 0 - 0 . 0 4 6 8 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 4 . 5 0 0 0 0 - 0 . 0 9 7 9 0 0 . 0 3 6 4 5 3 . 0 0 0 0 0 - 0 . 0 4 67 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 4 . 0 0 0 0 0 - 0 . 0 6 7 1 0 0 . 0 3 4 6 4 3 . 0 0 0 0 0 - 0 . 0 4 62 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 5 0 0 0 0 - 0 . 0 4 3 0 0 0 . 0 32 4 0 3 . 0 0 0 0 0 - 0 . 0 4 5 4 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 3 . 0 0 0 0 0 - 0 . 0 1 6 6 0 0 . 0 3 0 7 9 3 . 0 0 0 0 0 - 0 . 0 43 9 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 2 . 5 0 0 0 0 - 0 . 0 1 8 0 0 0 . 02 8 9 5 3 . 0 0 0 0 0 - 0 . 0 3 8 6 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 2 . 0 0 0 0 0 0 . 0 1 3 3 0 0 . 0 2 7 4 3 3 . 0 0 0 0 0 - 0 . 0 3 8 3 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 5 0 0 0 0 0 . 0 5 72 0 0 . 02 6 3 2 3 . 0 0 0 0 0 - 0 . 0 3 9 5 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 1 . 0 0 0 0 0 0 . 1 0 7 0 0 0 . 0 2 5 0 2 3 . 0 0 0 0 0 - 0 . 0 42 1 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0 - 0 . 5 0 0 0 0 0 . 1 6 5 0 0 0 . 0 2 4 2 6 3 . 0 0 0 0 0 - 0 . 0 4 5 2 0 0 . 0 1 0 0 0 0 . 1 0 0 0 0

0 . 0 0 0 0 . 22 7 7 0 . 02 3 6 5 3 . 0 0 0 0 0 - 0 . 0 4 8 9 0 . 0 1 0 0 0 . 1 0 0 0 0 . 5 0 0 0 . 2 9 5 2 0 . 02 3 0 3 3 . 0 0 0 0 0 - 0 . 0 5 3 4 0 . 0 1 0 0 0 . 1 0 0 0 1 . 0 0 0 0 . 3 6 4 3 0 . 0 2 2 6 5 3 . 0 0 0 0 0 - 0 . 0 5 7 9 0 . 0 1 0 0 0 . 1 0 0 0 1 . 5 0 0 0 . 4 3 3 4 0 . 0 2 2 4 7 3 . 0 0 0 0 0 - 0 . 0 62 1 0 . 0 1 0 0 0 . 1 0 0 0 2 . 0 0 0 0 . 5 02 7 0 . 0 2 2 3 7 3 . 0 0 0 0 0 - 0 . 0 6 63 0 . 0 1 0 0 0 . 1 0 0 0 2 . 5 0 0 0 . 5 7 1 2 0 . 0 2 2 3 4 3 . 0 0 0 0 0 - 0 . 0 7 0 4 0 . 0 1 0 0 0 . 1 0 0 0 3 . 0 0 0 0 . 6 0 5 6 0 . 0 2 2 6 5 3 . 0 0 0 0 0 - 0 . 0 6 8 5 0 . 0 1 0 0 0 . 1 0 0 0 3 . 5 0 0 0 . 6 5 62 0 . 02 3 2 8 3 . 0 0 0 0 0 - 0 . 0 6 9 8 0 . 0 1 0 0 0 . 1 0 0 0 4 . 0 0 0 . 0 . 7 1 3 4 0 . 0 2 42 0 3 . 0 0 0 0 0 -o. 0 7 2 5 0 . 0 1 0 0 0 . 1 0 0 0 4 . 5 0 0 0 . 7 6 3 1 0 . 0 2 5 5 2 3 . 0 0 0 0 0 - 0 . 0 7 4 4 0 . 0 1 0 0 0 . 1 0 0 0 5 . 0 0 0 0 . 8 0 8 6 0 . 0 2 7 2 7 3 . 0 0 0 0 0 - 0 . 0 7 6 4 0 . 0 1 0 0 0 . 1 0 0 0 5 . 5 0 0 0 . 8 5 0 1 0 . 02 9 5 4 3 . 0 0 0 0 0 - 0 . 0 7 8 3 0 . 0 1 0 0 0 . 1 0 0 0 6 . 0 0 0 0 . 8 8 8 9 0 . 0 32 3 2 3 . 0 0 0 0 0 - 0 . 0 8 0 6 0 . 0 1 0 0 0 . 1 0 0 0 6 . 5 0 0 0 . 92 1 5 0 . 0 3 5 8 3 3 . 0 0 0 0 0 - 0 . 0 8 2 7 0 . 0 1 0 0 0 . 1 0 0 0 7 . 0 0 0 0 . 9 4 9 4 0 . 0 4 0 0 7 3 . 0 0 0 0 0 - 0 . 0 8 4 8 0 . 0 1 0 0 0 . 1 0 0 0 7 . 5 0 0 0 . 9 7 5 5 0 . 0 4 4 7 4 3 . 0 0 0 0 0 - 0 . 0 8 7 0 0 . 0 1 0 0 0 . 1 0 0 0 8 . 0 0 0 0 . 9 9 9 1 0 . 0 4 9 9 1 3 . 0 0 0 0 0 - 0 . 0 8 9 3 0 . 0 1 0 0 0 . 1 0 0 0 8 . 5 0 0 1 . 0 1 9 0 0 . 0 5 5 5 7 3 . 0 0 0 0 0 - 0 . 0 9 1 6 0 . 0 1 0 0 0 . 1 0 0 0 9 . 0 0 0 1 . 0 3 6 6 0 . 0 6 1 72 3 . 0 0 0 0 0 - 0 . 0 9 3 9 0 . 0 1 0 0 0 . 1 0 0 0 9 . 5 0 0 1 . 0 5 3 5 0 . 0 6 7 9 9 3 . 0 0 0 0 0 - 0 . 0 9 62 0 . 0 1 0 0 0 . 1 0 0 0

1 0 . 0 0 0 1 . 0 6 6 9 0 . 0 7 4 97 3 . 0 0 0 0 0 · - 0 . 0 9 8 6 0 . 0 1 0 0 0 . 1 0 0 0 1 0 . 5 0 0 1 . 0 7 6 6 0 . 0 8 2 7 3 3 . 0 0 0 0 0 - 0 . 1 0 1 2 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 0 0 0 1 . 0 8 4 5 0 . 0 9 0 7 0 3 . 0 0 0 0 0 - 0 . 1 0 3 8 0 . 0 1 0 0 0 . 1 0 0 0 1 1 . 5 0 0 1 . 0 9 4 2 0 . 0 9 8 4 9 3 . 0 0 0 0 0 - 0 . 1 0 62 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 0 0 0 1 . 0 9 8 1 0 . 1 0 7 7 4 3 . 0 0 0 0 0 - 0 . 1 0 9 1 0 . 0 1 0 0 0 . 1 0 0 0 1 2 . 5 0 0 1 . 1 0 6 8 0 . 1 1 6 0 9 3 . 0 0 0 0 0 - o . 1 1 1 8 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 0 0 0 1 . 1 0 8 3 0 . 1 2 6 2 8 3 . 0 0 0 0 0 - 0 . 1 1 5 0 0 . 0 1 0 0 0 . 1 0 0 0 1 3 . 5 0 0 1 . 1 1 4 1 0 . 1 3 5 4 9 3 . 0 0 0 0 0 - 0 . 1 1 7 8 0 . 0 1 0 0 0 . 1 0 0 0