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NASA Co ntr acto r Report 172531

NASA.CR-17253119850014054

EFFECTSFLEADING-EDGE EVICESNTHELOW-SPEEDERODYNAMICHARACTERISTICSFA HIGHLY-SWEPTRROW-WING

SAMUEL, SCOTT, ORAN W, NICKS,AND P,K, IMBRIE

TEKWORLDOMPANY ' "-_"

HAMPTON, VIRGINIA1,'I..':i' "c: ,, _,. j,,.

. a_ ., _ 'd 6JI; .r_ .-_ 7

PURCHASE ORDER L-69215B

FEBRUARY985 _i_r'_ _ __r_.r

: ',i ;_,50

tJ-,NGLEYRESEARCH,:EN rERLI_.RARY,NASAij : r. "'_T('_pJ............. VIRGII'IIA

I IASANationalAeronauticsandSpaceAdministration

Lan gleyRe searchCenterHampton,Virginia23665


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CONTENTS

Page

Symbols iioem o mooosmooo o mmomoooomm e IeooamIo

Summary .................................. iv

Introduction ............................... i

Model ................................... 2

Tests and Correction 2ao, o oooooeaoeeoooeeooeo, . o

Presentationof Results .......................... 3

Results and Discussion .................. ........ 4

LongitidunalAerodynamicCharacteristics ............... , 4

Effect of ReynoldsNumber .......... ............ 4

Effect of Leading-EdgeVorticies .................... 5

Effect of Simple Leading-EdgeDeflection ............... 5

Effect of Leading-EdgeSlat ..................... 6

Effect of Variable Chord Leading Edge ................ 7

ComparisonofLeading EdgeDevices 8me em,o,,o e ,, o ,oo,

Effect of Trailing-EdgeFlap Deflection ........ , ..... 8Lateral-DirectionalAerodynamicCharacteristics. .-........... 8

Effective Dihedral-Derivative ............. ....... 9

Summa_ of Results ......................... .... 9

APPENDIXA .......... ............ .... 10

References 26o ,oo,eo e o, oo o , e eoelo,oeoooo e ,ooo

Table I , ................................ 27

Figures .................................. 28


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SYMBOLS

The longitudinaldata are referredto the stabilitysystemof axes, and the

lateral-directionaldata are referredto the body systemof axes as illustrated

in Figure 1. The moment referencecenter for the tests was located at 59.855

percent of the referencewing mean aerodynamicchord. The referencewing area

and referencemean aerodynamicchord are based on the wing planformwhich

results from extendingthe inboardleading-edgesweep angle 73.02 and the out-

board trailing-edgesweep angle 41.46 to the model center line. (See Fig. 2.)

The dimensionalquantitiesherein are given in both the International

System of Units (SI)and the U.S. Customary Units.Computer symbols used are

given in parentheses.

b2

A - aspect ratio, Sref

b - wing span, m (ft)

Drag

CD (CD) - drag coefficient,q-_ref

CDi - induced drag coefficient

CD - minimum drag coefficientmin

CDsym - drag coefficientof the configurationwithout twist andamber at zero lift (seepg. 4)

CL (CL) - lift coefficient Lift ' q--_re

C_ (CRM) - rolling-moment, Rolling momentqSref b

Cm (CM) - pitching'moment coefficient, Pitching momentqSrefC

Cn (CYM) - yawing-moment coefficient Yawing moment' qSrefb

ii


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Cy (CSF) - side-forcecoefficient,Side force qSref

- referencemean aerodynamicchord, m (ft)

q - free-streamdynamic pressure, Pa (Ibf / ft2)

S - Leading-edgesuction parameter

Sref - referencewing area, m2 (ft2)

X,Y,Z - body axes system

a (ALPHA)- angle of attack, d eg

(BETA) - angle of sideslip,deg

6f - trailing-edgedeflection,positivewhen trailing edge is down, deg

6L.E. - leading-edgedeflection,positivewhen leading edge is down, deg

Derivatiyes:

CL - @CL / a_, per deg(_

C_B - @C_ / _B, per deg

iii


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Introduction

The NationalAeronauticsand Space Administrationis currently investigat-

ing the aerodynamiccharacteristicsof advancedaircraftconceptswhich are

capable of cruising efficentlyat supersonicspeeds. The conceptualdesigns are

representativeof future generationcommercialand militaryvehicles and incor-

porate wing sweepson the order of 70 to 80 (e.a.,Refs. 1 and 2). Unfortu-

nately such configurationshave typicallyexhibiteddeficient subsonicaerody-

namic characteristics. These deficiencieshave been attributedto the formation

of leading-edgevorticies. Numerous leading-edgedevices and conceptshave been

consideredto eliminate or minimizethis vortex formation (see, for example,

Refs. 3 through 5). The present wing geometrydiffers slightlyfrom the geome-

try consideredin References3 through 5. The leading-edgebeing modified to

obtain a constant inboard leading-edgesweep of 73.05.

The present study was specificallyintendedto providea direct comparison

of severalleading-edgedevices. The tests were conducted in tileTexas A & H

University7-by-lO ft Wind Tunnel over an angle of attack range from about -6

to 16 for sideslipangles of 0,- 5 and -10 and at Reynolds numbers (basedon

the wing mean aerodynamicchord) from 4.1 x 106 to 5.3 x 106.


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2

Model

The principal dimensional characteristics of the model used in the present

investigation are listed in Table I and shown in Figures 2 and 3. A sketch of

the model and mounting arrangement in the Texas A & M University 7-by lO-footwind tunnel is shown in Figure 4.

The model incorporated three different leading-edge systems and a trailing-

edge flap system as shown in Figure 3. The model did not incorporate either

nacelles or an aft fuselage.

Tests and Correction

The tests were conducted in the Texas A & M University 7-by lO-foot low

speed wind tunnel. The model was mounted in a wings vertical attitude so that

the wind tunnel turntable could be used to obtain a -6 to 16 angle of attack

range (see Fig. 4). A variable knuckle was used to provide side slip angles of

0, -5 and -i0 . Forces and moments were measured with a standard six-

component strain-gage balance mounted internal to the model. Flow visualization

was accomplished using 0.048cm (0.019 in.) diameter nylon tufts. Test were

conducted at dynamic pressures of 3064.3, 4069.8, and 5123.16 Pa (64, 85, and

107 Ibf /ft 2) these values of dynamic pressure resulted in Reynolds numbers

(based on the wing mean aerodynamic chord) of 4.1 x 106, 4.8 x 106, and 5.4 x

106. The majority of the tests were run at the lower dynamic pressure which

resulted in a Mach number of 0.21.

Jet boundary corrections to the angle of attack and drag were applied in

accordance with Reference 6. Blockage corrections were applied to the data bythe method of Reference 7. Balance chamber pressure and model base pressure

were measured and the drag measurements were adjusted to correspond to


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3

conditionsof free-streamstatic pressureacting over the base of the model. An

angle-of-attackcorrectionof 0.8 was applied based on comparisonsof previous

tests of similar configurations(Refs.3 through 5).

Presentationof Results

A data supplementcontaininga run scheduleand tabular listing of data is

provided in AppendixA. The results and discussionare presentedin accordance

with the followingoutline:

LongitudinalAerodynamicCharacteristics

Effect of Reynoldsnumber

Effect of leading-edgevorticies

Effect of simpleleading-edgedeflection

Effect of leading-edgeslat

Effect of variablechord leading-edge

Comparisonof leading-edgedevices

Effect of trailing-edgeflap deflection

Lateral-Directional AerodynamicCharacteritics

Effectivedihedralderivative

In additionto the standardlongitudinalaerodynamiccoefficients Cm,

CL, and CD and the lift-dragratio (L / D); the leading-edgesuction

parameter(S) is also presentedas a figure of merit. The leading-edgesuction

parameteris fully discussedin References4 and5 and is defined as :

CD - [ + CL tan [CL /C L )]S = CDsym a

CL2 _ -C k tan (CL /Ck ]

Where CDsym is the drag coefficient of the confi guration without twist and

camber, at zero lift. (See ref. 4 for a discussion of CDsym). The value of


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CD has been estimated for the present model tests using the relationshipsym

CL2CDrain

CDsym= CDmin - _A

Evaluation of this relationship yields CD:y_ = 0.0107. The value of CLhas been determined experimentally (from the linear region of CL versus _)

to be 0.039.

Results and Discussion

The present study was specifically intended to provide a direct comparison

for the effect of several leading-edge devices on the aerodynamic performance of

highly swept wings. The model did not incorporate either nacelles or an aft

fuselage.

Longitudenal Aerodynamic Characteristics

Effect of Reynolds Number.- Figure 5 presents the longitudinal aerodynamic

characteristics for the configuration with undeflected leading-edges over a

range of Reynolds numbers of 4.1 x i0 G to 5.3 x 106. As can be seen, for the

configuration with undeflected leading-e dges, increasing the Reynolds number

from 4.1 x 106 to 4.8 x 106 results in only slight chan ges in Cm, CL, and CD.

However, the nature of the changes in CL and CD are such that significant

increases in leading-edge suction and lift-drag ratio occur with increasing

Reynolds number. Further increasing the Reynolds number to 5.3 x 106 yields

no further changes in the aerodynamic characteristics. Reynolds number sensi-tivity studies were also conducted for a number of deflected leading-edge

configurations. These data are not presented, but are contained in the

tabulated data of this report. Results of these studies all showed that with

deflected leading edges, no Reynolds number effects existed.


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5

Effectof leading-edgevorticies.-References3 through 5 have shown that

this class of highly swept-wingconfigurationexhibits vortex separationon the

outboardwing panel for angles of attack of approximately2 and that wing apex

vorticiesbecome evident for _ > 4. Flow visualization,using mini-tufts,

verifiedthis phenomenonfor the present configurationwith undeflectedleading

edges. Unfortunately,the photographicquality of this particularsequencewas

quite poor and tuft photographsare not available.

The data of Figure 5 illustratesthe effect that such vorticies have on the

longitudinalaerodynamiccharacteristicsof the configuration. As can be seen

for a = 4, a pronounced non-linearityin CL and Cm versus a exists.

These results are consistentwith previous studies,the non-linearityin CL

being termed vortex-liftand the non-linearityin Cm being termed pitch-up.

Effect of simple leading-edgedeflection.-Reference 3 has shown that a

simple leading-edgedeflectionof 30 is an effectivemeans to forestall leading

edge vortex separationfor a similar,highly-sweptarrow-wingconfiguration.

For the present configurationfigure 6(a-d) shows the effect of simply deflect-

ing the leading-edgeabout the hinge-lineshown in Figure 3(a), for conditions

with the outboard verticalf ins on and off, and 6f = 0 and 20. In as much

as the higher RN data was obtained for the configurationwith aLE = 0,

only for conditonswith tileoutboardverticalfins on, plots of S and L / D

are presented for the configurationwith aLE = 0, only for conditionswith

the vertical fins on. However,noting that Cm, CL, and CD are only slightly

influencedby RN , these data are presentedfor the configurationwith aLE =

0 for conditionswith verticalfins on and off. Comparisonof the data of

figure 6a with that of figure 6b, and comparisionof the data of figure 6c with

that of figure 6d indicatesthat the outboardvertical fins may provide a slight

reduction in the pitch-uptendancyat higher angles of attack.


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6

Most importantly, the data of Figure 6 shows that deflecting the leading

edge through either 30 or 40 is effective in delaying the angle-of-attack at

which pitch-up occurs to _ > 8, and that the vortex lift increment is

virtually eliminated. The data further show that for the range of lift coeffi-

cients of interest (i.e., 0.3 _ CL _ 0.6), aLE = 30 provides better

performance than aLE = 40-

Tuft photographs for the configuration with aLE = 30 are presented in

Figure 7. As can be seen for a > 8 some vortex separation is apparent for the

inboard wing panel, while the outboard wing panel experiences plain separation.

This condition, as expected, worsens with increasing angles-of-attack.

Effect of leading-edge-slat.- The leading-edge slat tested, was designed

using simple sweep theory in conjunction with two-dimensional methods. The slat

design was intended to limit the normally high leading-edge suction peaks, to

values for which it was considered that attached flow could be maintained. This

resulted in an average value of slat gap of approximately 0.170 cm (0.067

inches) and an average value of slat overlap of approximately 0.079 cm (0.031

inches). Results for the configuration with the leading edge slat (see Fig.3(b) for geometric details of the slat) are presented in Figure 8(a-c). The

data show that for af = 0 the leading-edge slat is effective in postponing

the occurence of pitch-up to _ : 12 (corresponding to CL : 0.55), and that

with _f = 20 pitch-up could also be delayed to CL _ 0.55. Tuft

photographs for the configuration with the leading-edge slat are presented in

Figure 9. Comparison with the tuft photographs for the configuration with the

simple aLE = 30, shows that the slat tends to suppress the inboard vortex

separation to higher _'s, but the flow over the outboard panel is essentially

the same and is experiencing separation for _ > 8.


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deflection)it also results in a significantperformancedegradationrelativeto

the 20 deflection,at lower lift coefficients.

Tuft photographsfor the configurationwith the variablechord leading-edge

are presented in Figure 13. As can be seen for either the 20 or the 40

deflection,vortex separationis apparentfor _ > 4. These results are consis-

tent with the force and moment data shown in Figure 12.

Comparisonof leading-edgedevices.-Figure 14 presentsa comparisonof the

longitudinalaerodynamiccharacteristicsfor the leading-edgeconfigurations

considered. As can be seen, the simply deflectedleading-edgewith aLE =

30, and the leading-edgeslat provide improvementsin longitudinalstability

and performancewhich are similar,however,the leading-edgeslat generally

exhibits slightlybetter aerodynamiccharacteristics. Both of these geometries

exhibit substantialimprovementsrelativeto the undeflectedleading edge and

the variablechord leading-edgeconcept.

Effect of trailing-edgeflap deflection.-Figure 15 shows the effect of

trailing-edgeflap deflectionfor the configurationswiththe simply deflected

leading edge and the leading-edgeslat. As can be been, the trailing-edgeflap

effectivenessis essentiallythe same for both configurationsand remains rela-

tively constant for the range of conditionsinvestigated.

Lateral-Directional AerodynamicCharacterictics.

As noted previously,the present model was comprised of a wing-fuselageand

was intended to addressgeneric problemsassociatedwith highly swept wings.

Reference 5 indicates that one of the major deficiencesof this class of highly

swept wings is the excessivelyhigh levels of effective dihedral.


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9

Effective dihedralderivative.-Figure 16 presentsthe variationof C_B

with a and with CL for severalo f the leading-edgeconfigurations

investigated. As can be seen, deflectingthe leading edge has the positive

effect of reducingC_B. This result is thought to be due to the deflected

leadingedgeeffectivelyrepresentingsome geometricanhedral.

Summary of Results

An investigationwas conductedto provide a direct comparisonof the effect

of several leading-edgedevices on the aerodynamicperformanceof a highly swept

wing configuration. The results may be summarizedas follows:

1. For the configurationwith undeflectedleading-edges,vortex

separationfirst occurs on the outboardwing panel for angles of

attack of approximately2 , and wing apex vortices become

apparent for _ > 4 .

2. Occurrenceof leading-edgevortex flows may be postponedwith

leading-edgedevices. Of the devices considered,the most prom-

ising were the simple leading edge deflectionof 30 , and the

leading-edgeslat system.

3. The trailing-edgeflap effectivenessis essentiallythe same for

the configurationwith either the simple leading-edgedeflection

of 30 or the leading-edgeslat system.

4. Deflectingthe leading-edgesdownwardin an attempt to postpone

leading-edgevortex flows, has the positiveof effect of reducing

the effectivedihedral.


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I0

APPENDIXA

WIND-TUNNELTEST SCHEDULENDDATA TABULATION

As an aid to the reader, the appendix provides the wind-tunnel test schedule and

tabulated longitudinal aerodynamic data.

TABLE AI. - TESTPROGRAM

RUN q,PSF 13,Deg Vertical Fin 6f, Deg Leading Edge

64 0 On 0 Undefl ected5 0 On 0 Undefl ected

107 0 On 0 Undefl ected4 0 Off 0 Undefl ected6 107 0 On 20 Undeflected

64 0 On 20 Undefl ected4 0 Off 20 Undefl ected

9 64 -5 Off 20 Undefl ectedi0 64 -I0 Off 20 Undefl ectedIi 64 0 Off 20 Slat, IA12 107 0 Off 20 Slat, IA13 64 0 On 20 S|at, IA14 107 0 On 20 Slat, IA15 64 0 On 0 Slat, IA16 64 0 Off 0 Slat, IA17 64 -5 Off 0 Slat, IA18 64 -10 Off 0 Slat, IA19 64 0 Off 0 Slat, IIA20 64 0 On 0 Slat, IIA21 64 0 On 0 Slat, IIA22 64 0 Off 0 Slat, IIA23 64 0 Off 0 Slat, IA

Taped Intersegment24 64 0 On 0 Slat, IA

Taped Intersegment25 64 0 Off 0 Simple, 3026 64 0 On 0 Simple, 3027 64 O On 20 Simple, 3028 64 0 Off 20 Simple, 3029 64 -5 Off O Simple, 3030 64 -10 Off 0 Simple, 3031 64 0 Off 0 Simple,4032 64 0 On 0 Simple, 4033 64 0 On 20 Simple, 4034 64 0 Off 20 Simple, 4035 '64 -5 Off 0 Simple, 4036 64 -10 Off 0 Simple, 40


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TABLEAI. - TESTPROGRAM(Concluded)

- RUN q ,PSF 13,Deg V e r t i c al Fin 6f, Deg Leading Edge,,'.. _ . . J,. , ,.

37 64 0 Off 0 VariableChord, 20 38 64 0 On 0 VariableChord, 20 39 64 0 On 20 VariableChord, 20

40 64 0 Off 20 VariableChord, 20 41 64 -5 Off 20 VariableChord, 20 42 64 -10 Off 20 VariableChord, 20 43 64 0 Off 20 VariableChord, 40 44 64 0 On 20 Varia]beChord, 40 45 64 : 0 On 20 VariableChord, 40 46 64 0 Off 20 VariableChord, 40 47 64 -5 Off 0 VariableChord, 40 48 64 -lO Off 0 Variable Chord, 40 49 64 0 Off 0 Slat, IB50 64 0 Off 0 Slat, IB51 64 0 On 0 Slat, IB52 64 0 On 0 S l at, IB

Out 'BD Gap Sealed53 107 0 On 0 Slat, IB54 64 0 On 10 Slat, ,IB55 64 0 On 20 Slat, IB56 64 0 On 10 Simple, 30 57 64 0 On 0 Simple, 30 58 64 0 On 0 Simple, 30 59 64 0 On 0 Simpl e, 30


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TABLEAll. - TABULATEDATA 12

mt,k 2

_ I. I'1'-# n t T_ (-1 -_ CP Cp_, CYP C _F

. 1." .Oe . l?=:p .01_ .0175 .non5 -.ooo p .nOn3-_,b P ,bO -, I _ 7- . ,Np n P -,O02 P ,O Oq7 -, O 0 0 Z ,000 _

-3.t3 .CO - .0411 .0175 .o051 .Oon7 -.O00p .O00_-I.13 .00 . r.(,22 .nlIn .012_ .Ono5 -.ONO P .0004

1.13 .UP . I; '=F .(_14 7 .O17q .no04 - .OU03 .000 33 . 4 o , UC ._IF4 .OPFO ,02 3 ( ; ,.000 6 -, O00 p ,nO0 ]3.r9 .t.O . 3pn4 .0.SA .036(. .0001 -.0004 O00l7 ,9 7 , tO ,46 ;; , 0 7 _ ,n4_9 -,O00 l -,oDor, , o oo 3

10.31 ,UC .5_P_ .1165 ,06F. 9 ,O .qN O -.nOlo .ooo3I_,', F GO , _ 7 57 , l _ q b .OS4 q ,OnO 9 -,O O3 P . -,,_O?n14 , ',_ -, (;1 ._q? ] ,P3Iq .I_PI ,Onl l -.005" -.OOe3

1.15 .O c .13_f .014 = .(;1P5 .O n05 -. no03 .OO0_

AL PF_ cE TA fl. FP CF C_J Cy_ CSF

I,]_ , U_ , 1 2 aP , 0143 ,0 1 7 _ , _005 - ,0 004 -,O OOl-_ , _ ,On - ,1 3_ I , OPo P -, NO2 a ,On o 5 -,nO0 3 , n o 0_-3,1 7 ,UO -.03_ .O1P_ .n OSO .n on7 -.ooo 3 .hOO p-l,n q - (_0 .0_7_ .nln7 ,O _ P .Oon5 -.nO03 ,oOq O

],I F , 00 , 13 _4 . 01 4 3 , 0 17 P , Oon3 -,o00a , oO n n3,_P , 00 ,_FP4 . fl 2 _ 7 ,02 2 7. ,o q n_ -,0 00 3 , nOnO5,_'A ,uO , 3 4 2 _ ,o&41 .034_ -eOl IN_ 1,0 006 ,000_R, I P .Ue , 4 F1 7 07P4 , O5_F -, On0 3 - , 0 00 7 -,no04

l o, _ P .oO ,_ P 47 . i ppg , 07 3q ,Go00 - , 001 5 -,nooq1_. q_ -,1)2 .TNFq .177_ .102_ .On lO -.n04_ - ,O0_ i]_._h . .04 .r_;f .Pg_2 .1 _6_ .On pO -.O08 P -.O13F1P, nI -.r_: l,_ )P6q .36 n4 ,1571 ,of)q6 -.011 3 -,0176

1. 7 _ .On . 1 44_ . N] 4_ , o l Tq ,On02 - .000 4 . O00S

_l,k 4

ALF_A _TA CL CP C_ Cn i_ CYP C _F

].P= .00 .141= o]4q ,0176 .Onn4 - .OO0 5 ,OOO3- 5._ 7 , UO -,1 3 F= ,(.PN4 -.0033 . Oon4 , ,non_ .0oo7-3,34 -I 'O -.03F : ,_]Pl ,OOSp ,On o5 ,0003 ,OOCA-I.OF .UN .N S]2 ,l' loq ,01_7 ,OnnF .00114 ,_004

I,E_ ,On , 12PP . oI4P .0173 0 003 -,000 _ ,noo43._ ? ,DO . _400 . n p_ 3 ,0 2 3 5 , OOn4 - . 0004 ,oooq_.00 ,O0 ._rr_. .,_ ,n4 o o ,036? - _OO4 - ,n O07 00065, 4 ? .on .4m 3F ,0_4 ,055_ :bnn3 -.o009 .00_ 7

]O, U6 ,U o ,_ ] I , = ,1 3? _ , OP 03 : Onn_ -, O0_ P -,On0 3,_8 , I , O . 1 4_,_ , Ol4q ._ITP 0,In 3 -, n O0_ , 000_

,_k P F..A _E I '_ CI. ('F) f.F' C_t_ 'v k C_F

1,17 ,GO ,1417 .nJ a4 ,0181 .OnnF -,{ _001 - ,,no0=-__.5 2 .on -.1 71_ ,O lql -.o011 ,COn8 ,O00(i - ,OO Op-3.P.a -{_0 - .(i?6q .011 5 . t_067 .00o7 -.O00 l -.qO0 _.-l.lt; .00 . n.r-(_0 .nln3 .013r5 , { , nne .o00n - .noo4

l,J F ,0 0 l 3 q.'? n l -3 ,Ol Vl , On n_ - , _nO ] - , nO N= .3 ,44 . 00 F37_ , n P_ . ? , OF. E_- , Onn7 - ,OU 0 3 -,oo0 15 . 7_ , uo .34_ ._. . o_._p ,n 3 9_ ,On n ? -,o00_ -,oo o p7,qc , GC .4zf7. , 0 7o_ ,061F ,Ono_ -,_100 3 -,(_00_

10. 31 .ON .S_6 ; .1 P| 1 .oP_] Oi_n_. -. OOOla -,_O O] 4 ;.F,' , -,Ol .f-70_ . 173_ ,liFO .0o 1 6 -,003 _, -,O04 e.14.q7 -'('Z ,7q=3 ._'3 Qq .] 463 ,0031 -.0070 - .O0_'n

1,1F .Uo ,i_ .31 .0144 ,0 l F_(. .0q{16 -,O00l -, 000_ a


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TABLEAII. - CONTINUED 13

_t. F, e .

ALnt -b n I , _ CL ( D CI4 C o t , , _ ( Y P CcF

-_ .09 .00 .03_ 'q .n? 4 *.P243 .00_)5 -.0{_03 - .nO0 ?-27 .00 ,1 204 .r)pq 4 -.0_42 ,oon4 -.0003 -.000 2

-._ . Un .;0_7 .(_? _ -.niP5 .non5 -.{boO4 -.on03I .e l .uO .pc:;. / .,_3_ . _. -.01 54 .oon; _ -.nuo 5 -.nO0 34.IP .00 .4 0_q .OC_f'; -.OOP l .UonO - ,0003 -.000 2

,5 _, .uO ,_;' _ ,h_n4 .O0_.q -,0004 - ,0007 -,0007c ,. (1f. *00 . _._,_, '- . I _':.? , O_._E6 -.O lin5 -.(IUU7 .0003

11.51 ,O0 ,7q _cz . 1n31 r)-r'O -,Onnl -,0024 -. 000 =12,90 -*1:3 ._ FP .2_.7q ,0867 .Olin7 -.O05P -.O07 Q

I ,_J z, ,nO .30nF . n .'zT._ -,olEI ,00o -.000 '_ ,n Oel

Pt: h 7

ALPI -A pET_ CL CP CV C_ M CyV CF F

I._;F .CO .2 _72 .n_6 -.0147 .Oon3 - .o00 _ .0000-_.ll .uO .0_5 .n? n_ -.03 _3 .oon7 -.000 ? .00C1-_._P .o0 -1 _3 .o_ pn -.n _2T .Otln_ -.nOO P - .0_01

-,_9 ,Oq ,gn_ ,0?_6 -.017 F ,O()ob -.000 2 -.0002],SF ,OU . 2_7P .03_4 -,Ol4q ,Oon _ -,OOU _ -.ooo]3.P7 ._10 .400_ .q_q -.O0_O .O _nO -,000_ - ,0003_,]e *00 .EIIO .0234 ,0073 -.00_? -,00 0_ -,0003P .4_ .UO .6_6 , 1? _q ,0 _23 -,00n3 -,O00h .00 0]

l_._, .uO .7 _]? . 17, _ .041 _ -.oon3 -.nol_ -.0 00_13,1g .,0 , _79 .P 3_ .0694 ,On _ -._04& -,003_l_.4P -,01 ,g? ?_ .30 70 ,lOB? -*Ooa& -.0063 -.00_17,75 .,02 1 ,0_7 .? _ ,15 32 -,O_3F -, _08_ -,00_|

1,59 ,UO ,301= ,n_7 -,014_ ,0002 -.0003 -.00 02

gU_ P

ALP FA pET A CL r P C_ Cn_, CYV CS F

1.52 .O O ._qPp .02_4 - .014_ .0()04 - .O00P -.nO0_-_. lO ._O .0_ 30 . n2o 6 -,O323 .00n7 - .o001 -.o0 o3-_._ 8 .00 .1 2_3 .o]oP -.0_27 .On o_ - .000 1 -.o0 0?

-,hp .O0 ,_070 ,n?62 -,0177 ,Onl )7 ,OOO n -,00071.59 *00 ._q_7 ._?R _ -.0148 .001 _3 -.000 _ -.06 _3.gl . 00 ._07F .P _6_ - .0059 .Oonl -.00 02 - .00046.]q ._0 ,_140 .n _O .o10 _ .oo0o . -.0002 -.OOn __._P .00 ._42 .17_ _ .O_q5 .00 00 -.0003 -.0003

lO.P3 .O0 .74 _3 .17qq .0 504 .O on -.OOI)9 -.001_13 ._1 .,01 ,F7 _7 ._a _ .02 _7 ,on13 -.OO3R -,00 _3]E,SE -*02 l,O06P .._7_1 ,1095 *0030 -._0_7 -._7_17,qO -.03 1,1 2_7 .414_ . 14q q .Onn7 - .n07 _ -,_ ;0

l.hl ,o0 ,30_ 7 .0_7 -,0146 ,oon3 -,ooo p -,0007

_U h e

ALPPA pET_ CL CP C_ CgM CYW CFF

]*_l =.Ul .30_ .O_n -.OIE? .Oq _4 .004 2 -.0227-E.O 9 _.01 .0_72 .O? ]F -.033 P .O_nF .n047 .00 _3-_,RF _.0 1 .|_ F? ._2n p -,0_3_ ,00 _3 ,Ofi4 P -,O0_P

-._7 :*(' . _OP = .Op=_ -.0123 .00 ,5 .0039 -. 01_I.SC _,01 .3o1 . o3_P -.012_ .oob_ ,O0_l -,022__.q _ _ ,eo .40 _ = .0_ -.O0_P .O Oql .1J04 3 -.0347(.lq F*(: O ._I_F ._h7 .013[ .OIIU ,_03_ -.O_

I0. _ _ ._q .7_? .1 _1_ .O_B? ,014 _ -.000 _ -._7_;

1_._1 6-_7 I.OIP; .3 7_ = .117 1 ,01 _7 -.quT _ -.lu3?|5.q& 4._ T 1.1&_ ._q%P .I _ .01_ ._ -,v1093 -,IIPO


20/70

TABLEAll. - CONTINUED 14PU_ 10

ALPP F pETA [ f_ CM Cn_ CYM CS F

I,F? 10.0P .3141 ,O_F -.OOZ3 .0130 .OIO N -,n 4A_-_.0_ i0.04 .04_ .n p46 -.o330 -.0_) il .o111 .ooR3-2._ In.U 3 ol31q .077_ -.o21o .0t_37 .OOgq - .OO eB

-o@6 0.03 ._lqE .OP? G -.0114 .Oo R6 . 009 _ -.02 qO

1.62 l;_.O_ . 31_P .03q4 -.0 026 .0130 .O09q -.044_3 .9_ IO.Ul .kiln . n=p_ .OOOP ,0175 .o094 -,06_06.lq I_.0 1 ._14_ .nA 7_ .0_74 .Olqe .OOB3 -.0R77P .51 In. U0 ._3_q .IPe4 .05 07 .0 _31 .0053 -.1107

13.1_ q. _P .F3 73 .P353 .lle7 .O pn2 -.0029 -.lff7115,3_ _ ._e .q3o4 ._0 3P .15_1 .Ol_e - .o053 - .17_o

1._ la.02 .31_ .O_ q5 - .0021 .0135 .aOq 9 -.0_5_

_ Uh 11

ALPF_ n EI A _L Cn _ Cp_ CY P CS F

1.50 .0_ . ? ec S .n_3_ -.0_15 . Ono3 -.0001 . 000_-_.IP .00 .nl4e .,3_ -.0571 . Onn7 -.o003 0 003-2 94 . u p . I _ 4 _ . n 3n7 -.0439 .00o(, -. 000 2 .000_

- . 77 . _0 .1 , _ ._ Q6 - o0 3 _6 .{ ] _ n _ - .O OO_ .O 0 0 q1.5_ -flO ._ 71 .fl?_ -.OZIQ .0_1_) 3 -.0001 .0010

3.7F .OO . 347C .0_1_ -.nl4P .Onol -.ooo3 .OOQ_5.q F . OO . 4 _ 7 _ .l__ _ -. OORl . On n O -. oo 0 _ .OOn7

10.43 .00 ,_ q; .oqo_ ,005_ -.OnO_ -,0013. -,OOl _12._4 -.Ul .eTl_ ,13PO .0 211 -,Onl 3 -,003_ - ,004_16 .H_ --O2 .7_7_ .17_7 .03 45 000003 -00055 -0010717.1_ --1}_ ._4_ ._?01 .0514 -.On_l -,_0_0 -, 007_

l.bO . bo .?e_ .07_4 -.oP l_ .Cq 03 -.OOOl .O01q

PUb 17

ALP_ pLT4 CL 0 CM Cgu CY_ CSF

1. _p .OG . _7P ._3 -.0223 . 0_(_ -.no0_ -.OCO_-5,_4 ,Off -.0 00_ ._|_P -.0603 .0003 -,_00? -,000_-_o91 . DO .Oq _ .n31_ -.0460 .OA_)4 -.nO_ -.O00P

1._7 .00 ._7F .q _q -o0223 oOq l02 -._OG 5 -oO00_3.qq . 00 .2_0c .04 7? .fll _P -.0011 -.flU0 5 -.0010_.Z? .OC .435F .OCEA -.0079 -.O _)fl_ -.OOO_ -.00 11P.SF -'01 .5_ ._7_; -.0013 -.Oonq -.00 05 -.001_

lO.e _q -.0_ ._]P3 .1057 .0077 -.0011 -.O01 P . -.004313.?0 -.04 ._6_ .I_P_ .0_3 -.0010 -._10 44 -.OOqP15.5 G -.u7 .7 _ .1_3a . 0414 -.Onl _ -.n07 o -.nlel

_0. 37 ..07 I._P _c .3_q .oel _ -.0n 72 -. oo lp -.nlpp .7 _ .00 ,_05 .n ? _7 -.O_ CH ,O On3 -.000_ -._ CO7

Rt:t. 13

ALP t.'. _ PI'.' TA CL _n _ CP t_ CYP CFF

I ,r' -? .O 0 ,_7_ .1_4 I -. 0;_0_ .Ono O -,hO OP .onoP-5.IP .00 ,OI F7 .n37n -. o5 (:(_ ,{'onb -.OUO_ -.Oe nl-2 .9? .uo .lOPe .n _n_ - -.n43o .oon5 -.n OO3 -.o ool

-.74 .on . l ':;o: .n3 o] -.0317 .oqoP -.00o'_ .nool1.4,_ .00 ,;.70(; .n _?7 -.020R . UO00 -._)003 ,oOn33.7_ .t' O .34 _(; .o_ .1 p -.n13 4 -.Onnl - .0oo4 -.O 0Ol5.q3 . _0 ._pC_l .nc43 -.0074 -.t_on3 -. POO h -.no038.1 _ .U(, .=1_,c .07_ -.0015 -.UoI , q - .nO07 -.00 13

10 .3_ -. 1}1 .e._31 .Oq a5 .0_3_. -.Oooq -.0013 -.0C331_ .5CY -.I ) I .ef.O_ .IPQI .004_ .Ooql .00_7 -. O0( -'-14.7 n ..03 .TlPC_ . _ .7 . n(_F ._. - .Onil -.oO Tp -.h i3 ]15.r_? -.1 :3 .7 _.h l .;I _7 .O&_7 -.Ut_ 34 -.nlO() -.013119. _C ..o,_ .F_5 7 .pP n_ .OEIR -. Oor_P . -.0075 -. 0077

I .4_ .oo . _-eR 7 . {,337 -.n _oe .Onn ? -.00 0;_ .non=


21/70

TABLEAll.- CONTINUED 15 I_ l . t, 14

ALPP_ ptl^ CL C9 C _ C_u CYP CSF

|,bP , O0 o_7_ ._4_ -o 02GP oOo03 -.000 _ -,OOn7..1_ . uO . nO_q .O_P C -.05R_ .O on4 - .0003 .000 2.2._q .CO .leO0 . _1_ -.04_0 .On n4 -. 0003 -.O00_

*.E_ .UO .laT I .rt_N_ -.032 _ oOo N3 -.0005 -.000 41._5 . UC o 27C .0 _47 . -.o21 .O,o| -.0005 - .0002

6,2 _ ,OO ,{_c? .N_? - .O0 6_ -.OLIN3 -,OO OF -.NOe

P .5_ *o01 .5 _1_ .077 _ -,0003 -oO ONA -,1 )007 -.OOl _lOoP7 .o O_ ,e _4 . 1o_4 , OO_8 -.01)14 -,fl O|_ -oflOk613,0 _ . .04 .b _2 .1 _77 0335 -.no? ? - .0037 -.009 _1_.30 -.u , o7 __ olO ?; . 0541 -,00 _ -.o Oe_ 3 -.Ol *n

20. |_ - .|C ._731 . _?47 .O P gP -.u n_O -.n u33 ..n?_1.70 .OO .;767 .,)7_ -..:203 .Oon l -.OOOfl -.O00_

ALPHA _TZ (L C_ Cu C _N CY_ C_F

|._p ,OO . _17 . _177 .CO _] .0_1_ -.O00 p -.0002- 5,_ E .( I0 . , l ap _ ,o _ nl *,0 26_ ,on nP -.qOO _ - , _ n0 7-2.3_ .,_ -.0_1 .n?_? -.0131 .001 0 -._UO_ -.0011-|.15 .UG ,0_0_ .NIP_ -.0020 ,OnnP - .onn _ -.no0_

I.I; .O o .1E97 .oI PO .oOPO . (,,I0_ - .0003 -.00023.37 .O 0 ._I_ .NP I? .015_ .Onnk -.0003 -.O00F_._ .oo ._ql_ .07_I .022? .Oonl -.oOO _ - .OOll7.75 .00 ._ 741 .O _l_ .OPt7 .O noO -.0007 -.G_I_

lO.On ..Ol , _{'0 .O _nq ._34B -.o nn_ -.ool_ -._o3q12.?E ..u _ ._4(.7 .oaTh .O _lq -.OnnP -.0029 -.no _14.4_ ..03 .@1,1,7 .1177 .0_43 -.0.41 -.oo5. -.011_16 .53 .,O_ .e _P_ ,1_7 .O _Oq -.0_3_ - ,_OP1 . -._107_.R2 ..0_ .7_P O .21_0 .1094 -._U_ -,oUP _ -,O07p

l.lO ,UO .1313 .017_ ._UB_ .00o5 -.0007 -.O00E

_b h 16

ALPHA p kIA CL _n (_ Cop, CYF CSF

1.10 .GO .1304 ._lTO .O07 q ,.ONn 5 ,QoOn -,00 _--_._l .00 -.]47g .0_77 -.0?_ ? .OnnP -.o00_ -.oOn _-_._I .oO -.14P] .n 37_ -.0_63 .oooP -.ou o_ - .o _0_-3.37 .o 0 -.0532 . _? _7 -o0130 .OotO -,O003 -.O Oln-1.1 3 .00 .0 _24 .Ol P= -.0017 .ONo P -.00 0_ - .O00 q

1.0 _ .00 .127 _ .P174 .0077 . O_n_ -.0_01 -. OO0_3.3_ .00 .2120 .oPn2 .0157 .Oo o_ -.0001 -.000__.57 .O0 .EgEO .07_0 .021_ .Oonl -.000 3 -.O01 07,7 _ .00 , 372_ .0_ _ .h2 fl| .O,) o_ -.000 5 -.001_

I0.01 ..01 .4_00 .O_O0 .0357 -.0111 13 -.0015 -.003012. _ ..02 .$4 _7 .0 P77 .O _4g -.On)6 -.nO30 -.00 _714,43 ..03 .blgO .IP ? _ .0629 -.0005 -.004 _ -.011_|6.67 .*02 .700 _ .IFPfl ,OR2O -.0044 -.OU PP -,ooq _18,9 3 -,01 ,7 _73 .? _7_ .I017 -.00 _0 -._090 -.005 _

1.1 _ ,uO .l_e .o173 .OOe _ .Ono _ .ooo _ -._oo_

ALP PA _ET_ CL CE CV Cp _ CY_ CSF

1.1 , _.0_ .123. .olO* .006o .0 0_3 .OOe2 .OOt _-_.bO . O_ -.143 _ ._07 -o 02_3 -.003 _ .olO R ,03_P-3.3_ F.04 -.0,74 .n?Tl -.0135 - .On07 .olO .n ?_-1.13 _.03 .0,6_ .o;n _ - .O02P .On n7 ._oq_ ,_1_1

1.1_ =.03 .131 _ ._I q4 .O0 _b .O, _P 2 .NO_2 .OOl _3.37 _.03 .7143 on e? _ .014 _ .ori e l .no7 0 *.oOE3

7,7 P _.0_ .375_ .{_42[' .0300 .0_I_ Q .n073 -.0177]O.C J _ .b3 ._t.7_ .liA3 q .N3P g .00_5 .OOe_ - .N_ 7I_._e =. 00 .E4FE .n _13 .()540 .OI J _ ._0 7_ -.0,_?14.4 _ _ ._p .F 2_ .177 n . _7_q .Ol _ .00 _7 -,O _2P16.73 4.qp .71P c .17#_ .0E95 .Oli6 .no_ -.07 _

lq. O0 _ .q _ ._l_n .;_P .107 7 .N,71 .nO_ -.OTRQ


22/70

TABLEAll. - CONTINUED 16

_LPh _ BETA CL C_ CP C_, CYP C_F

l , Ip I0.07 , 13P4 . nps P . 007 3 . 00 36 , e l * 6 , 0 05 7- 5, ,7 I 0 o 10 - ,1 3 1q . 04 7 1 - o 02 74 -,O0 7 P , 0 23 6 , 06 _S-3.3_ In , u P -.03 3 1 .033 5 - , 0146 -oO Opq ,0 2 1& , 0 431- I . l ] iO.C7 .05 6 F .O P_P - . O0 3P -oOnn] 019P . OPlq

I.I 0 I0,07 . 12 _ , OP4 R .007 7 ,0035 ,01 8 4 , OOffq3, 3n I 0 . C7 . _PO ,O p n 7 . 0 1 8 0 ,0 o7 5 , 0 17 8 -. OOP__,6_ le ,07 .3063 .n 777 .0 283 .01 16 ,h iE? -.024n7,P3 lr.O_ .2q7& .0_33 .039 7 .Ol_l .0706 -,04 _&

I 0.08 1 0.0 _ .4 8 5 6 . 07 3 _ .0 54 7 .02 pI . 0201 - , 076 q] 2 .3F IO,OI ._776 .I 05 F . 072 0 .0 _ 3 _ ._18q -.Oq q O1 4.57 In . O0 , 66 4 P . 1 44 p .08 8 9 .O p05 .of 7& -. I I _ 3I _ . _4 I0,00 .7 _1 2 .IO F O , l l Ol .OI R6 .o le6 -. 1 37 619 . 11 _ . qP . P _93 .p_ 4 .13 5 1 .013 7 . 01 53 -.1 6P ?

l,lE 10 .06 ,137P ,oP_ . 0075 .0o3 6 o018 4 o00 3

rt.h l_

_LPP A v[T# (L Cr C _ Cp M CYP CFF

l.l ,bo .130 _ ,n]_a ,OOq4 oOnn7 -,ooo p -000 7-_,t_ .00 -,14P C ,n377 -.0250 .O0 0e -,O00 P -.O0 0&

-3.37 . 00 -,u fs_ . 0P47 -.010 8 ,Oo nF -.0OO p -.0004-1.14 .00 .040E .O]oP .O00P .00nq -,0001 -.O00 FI,ll ,00 .i_? .01_7 , OOq4 .Oon7 - .0001 -.00063,37 .UO ,? IO_ .(;? O_ ,0167 ,0 003 -,OO OP -,000 _5.b6 .00 . 2PC _ .027 q .0F35 .Ono P -,0003 -,00 077,7q .00 . _ 7 4_ ,_4 n _ ,030 4 ,O0 0 P - ,OO OP - , 001 _

IO,O P - ,01 .45P_ ,fl606 ,03_ -,00o3 -.OOl_ -,0 037)_,27 -*t)_ ._e_2 ,O POP ,04 q3 -cOOl U -,q03 7 -,008 314,46 -.03 .e Pl; .]PFO , 0680 -, no n& -.OO&9 -.O]Oq1 5 .6_ -, Of ,700_ o 17 10 ,O_ q 4 -,Oo a 5 -,00 55 -, 0 06 7]9.q _ o 0 1 , 7_6_ . p3 p l .I1 34 - .0o n 6 -. n 0 5 3 o00 _ 0

I.IP ,o0 . I731 .o] a o .oO qq oO(|n6 -o00 0? ,000 =

_t_ ;0

^LP_a _L1h CL rp (.p C =t,_ f YV CFF

]l ; ,co .1 3 _ ,q1 7P ,0 0 9 7 .oo n7 -,co n 3 - , 0 0 0 1-5.h i ,{_0 -, ]_h O .O_ 7P -,0Z43 ,Oot)P -.OOOP ,OOO l-3,3_ ,O0 - .O_S C .h?5_ -,0103 ,0o10 -,O00p -,00 0_-1o13 . bO .0_11 oO lP7 ,0010 ,Ono _ -,O00 P -,0oo|

1,14 ,#_0 ,12110 ,n1 74 ,oOq _ ,ooo7 -,o00P ,00003,3_ . 00 ,;oq7 .nP]l ,0171 ,Ono_ -,0003 -,00015.5_ ,1;0 ,_qnG ,opt? ,024 ? ,Gn ,l -,0005 -oOO Oa7.77 * 1 1 0 ,27Fg ,o a ]6 ,030_ , Oo o F -,0OOP -,0011

lO,O l -.01 ._=o ; .0_1 _ ,03FO - ,Ooo_ -,o017 -,00 3_l_.2q -.OE .5_Cl ,nnq_ .o_6 h -.Onoa ' - ,0031 -.OOq31_,43 -,02 .*077 ,l_nl ,0697 - .oo_o -.o037 -,00_616o%P -.o_ ,{f ]_ ,l_f17 ,og P7 -,O0 3P - .0_43 -.O07Plq,P_ ,01 ,7_54 ,PlP7 ,1_06 -.O07P -,0043 ,0037

1,10 , u O . 131_ ,0170 .o o gg ,OO O6 - ,OOU3 ,000%

r Ub ;I

ALP P_ n t7_ CL _ CF ' Co_ CYP C_F

l,l; ,O0 ,130 q ,0170 ,OOg7 ,Onn7 -,0003 -, 0003-5,67 ,00 -,14_ 3 .o_TP - ,0_47 ,Oo lO - ,O00p -,0003-3,3_ ,00 -,05_ ,oF67 -,n llo ,Onll -,0003 -,CO03-1,14 ,uO ,0404 .OJPP ,000 4 ,On]O - ,0003 -,OO04

l,ll .bo ,l_gP ._|70 0096 ,on07 -,000 3 -,O00P3.37 ,00 ,PI07 ,opo7 ,0173 ,on04 - ,O00 & -,00045 .5 7 . CO ._O0 ,O_P_ .0_4 3 ,0003 -,nO0% - .c o n P7.77 ,00 ,775f ,041 0 ,0307 ,O( IoP -,000_ -,0016

10 ,04 - .01 .4_64 ,o_P1 .0361 ,O0oO -,POIF - ,004112,zo -,t)? ,54P_ ,o_o_ .o&_o -.Onl ? -,oo_ q -.OOO314 ,4_ _.OE ,_17E .1P37 ,()7Z3 -.Oop7 -.n037 -,OlO I16 ,FB .,Op ,_q56 .lTP _ ,hqO 4 -.0034 --,O05 A -.007319. 0_ -.Of .P l_6 .TAP_ ,lZFq -.Oo_q -,0037 -,OOE7

1,11 . 00 ,13; P .01_ ,OOgq ,On 06 -,0003 ,0001


23/70


ALPHA pE TA CL CP C V CpN Y_ CEF

1.1_ .00 .12_0 .ol _P .009 7 .ooo7 -.0 o0 - .no0,-5,63 .00 -.14P 0 .0_ 72 -.0245 .O hiO -,o0o1 -.0_0_-3.39 .O0 -.0F37 .O ? 4Z -.OIOP o Vnl2 -.0 00? -.0007-1.1S .{=0 .0416 .o17 6 . . 000 8 .o onq -.000 ? -.0004

l.ln .00 .12ga .01 63 .oo q5 .oon7 -.0001 -.oO Oa3.3 P .oo .211 _ .o loq .hi70 .oo n3 -.0007 -. 000_5.57 .0 0 ,2PEP . 0774 . 0235 ,0002 - .non & -,oOOQ7.7 q .00 o374P .n_ q o . 0301 o0000 -.00 09 -.OOl_

I0.01 -.01 . 46P 1 .n _nF . 0374 -.O00P - .qol4 -.003112 .27 ..02 ._ 41 4 .nA n 2 . 05 26 -.0 o 0 5 -.no4p -,00 9 314 .51 . .03 .6_ 35 .133 P .066 8 -.0002 -.n0 34 -o011_16 .81 ..OE .7453 .lnqO .0 _ -.O04& -.OOSn -.O0 6F19.1_ .00 .P (_ .p_P 6 .11 21 -.O07 b -.o02 l -.o00 e

1.1_ .00 .]3_ P .el_ .O Oq9 ,_00 7 -.0007 -.0006

_h _ 3

ALPP _ pLT A CI. Cn CV C_ CYV CF

1.15 . o0 .12FF .n lTO .o077 .ono_ - .O00P -.oen_-5,bO .GC -.14P_ .n 373 -.0266 .non _ -.00 o3 - .o00_-3.33 .On -.o&*F oOP, F -.0 131 o0_] -.nO0? -.0001

-1.1_ .0 0 .o4_ 1 .nl_ -.0o21 .nolo -.oooP .noon1.13 .bo .1 _= .n] _ .007_ .Ono_ -.0003 -.000_3.3P .00 .2 11 _ .O;O 1 .0153 .Onn _ -.nOn? -.OOO_5 .5_ .00 ._5 .0775 . 021 7 .On02 -.0003 -.O01n7,8P ,oo , 379g ,0413 .0281 ,0=100 -,0005 -,000_

10,01 ,.01 .4E_O .n=qs .0344 -.OOn P -.00 13 -.0020I2._P .,01 . 53P _ .0_7? .0478 -.00 i5 -.0040 -.005_1_,5 3 .,0_ ,639 4 .1P *_ .OSq P -,onn_ -.0o 5_ -,OOS qI_.7 P 02 .73F_ .IP 2_ .075_ -.0035 -.O06O -.010719 ,10 .,02 ,P&_3 .26c 7 . 0 q 34 - .0067 -.OOb8 -,OOEP

1.15 .00 .13n4 .n]_7 .0083 .On06 -.noo l .000_

ALPP a =E T_ CI C_ CP Cnt. CYP C _F

1.15 .00 ,12qq ._ 1 77 ,0081 ,O o f15 - . 0 003 -.0006-5,5g ,n O -,14_0 ,037 q -,0270 , O_O P - ,000 4 -,000 5-3.3 _ -_0 -.0557 .o ? _g -.0137 .000_ -.0005 -.0007-1.1 4 .00 o03 PI .01_7 -.00 2_ .On o7 -.000 4 -.000 _

1 . 15 ._ 0 . 1_74 , Ql 7q . 007 6 .O on5 -.000 3 -.O00 P '.3.3q . 00 .21 0_ ,n? 13 , 0 156 .Oon_ -.0003 - .00045._0 ,00 .2901 .op*n .0220 .0 001 -o00 04 - .OOlP7.78 .CO .3733 .04]1 .028 4 -,O00l -,0007 -.00]7

10 .0_ - .01 .4_ 3E .n 613 .033 4 -.On06 -.oo l? -.on3 e1 2.2 8 -. 0 2 .F 4_ 7 .O P T_ . 0 43 _ - . On lg -,0033 -.OOP O14,4 5 .,0_ ,6130 ,1206 ,0657 -,003 2 -,0061 -,OO P P26 ,66 . ,0_ . _9 01 . 2_7 3 ,08 go - .On3 _ -. 0 0 7 5 -, OI OF18.9 = ..0 2 .792 R .?? _3 .lOB3 -.0 0S 5 -.0070 -.0077

1.13 .00 ,| PF q .0277 .00 80 .Oon4 -.0003 -.0002

nLh _5

ALPH_ _ETA CL _ CM C_M CY_ CSF

1.I 0 .o0 . l lfiO .nl a l ,o13 q .O o Oq - .00 01 -.0007-5.b6 .00 -.1750 . _377 -.0094 .00 _1 .000 1 -.0007-3.3_ .00 -.ObO0 .0_4_ 0022 .0_14 .oOO l ,0007-I,1_ ,00 ,0_77 ,01 7_ , oO g7 ,DO 10 -,000_ -,00 03

1.11 .o0 .2P1 3 ,014 _ .o13B ._ ,)0 _ -,0002 - . 00 0 33.37 ,00 ._013 .hi ll .02 76 .O on5 -.0003 -.non 55._6 ,O0 .E7 3_ .OP_A .025b .Ooo_ -.000 3 -.00 207.74 .00 _ 4- .n37_ 0347 . Oon5 -.0 003 - 0016

10.02 ..01 .446_ .0_6 .04 21 .O_n7 -.0013 -.003]12,2 _ ..o_ .5_55 . o o17 .0553 . onnc -.0031 -.o08_14, 52 -.03 . _333 .1310 .078P .Ono4 -. oO b3 -.n 12F1_.75 .,03 .7164 . 17 P 6 .flqq 6 -,O0 2l -,0077 -,O13g29 .0_ .00 .P_fi3 ._74 .1225 -.Oo_ P -.n |)SP .oo0_


24/70


_t_ h _6

AL.PFA pE Ta CL Cn CV CNu CY_ CFF

I.II .o0 ,IPnF .O l4P .0140 . o007 -.O00 P .0000- 5 . 66 . 00 -. 173 q . e 3 al -. 0100 .Oo l l -.OCO l - .0001-_o42 .OO -.oro _ .op4P o0021 .OOl3 .O00 p -.0004- I . I P .o 0 ,0200 .017 7 .0 1 00 0 0 0 8 -. o 00 a -. O00 1

1,13 ,00 ,118P , O14q ,O13q ,oon7 -,0004 -,000]3,36 ,oO ,_03P ,olP2 .0176 o0 005 -,0004 .no0 o5,57 ,OO , ? 7P_ ,0? 60 ,0745 , 00o 2 -,000 4 -,OOCP7,76 ,00 .3613 ,n3_ ,0323 ,0o03 -0006 -,0010

10.04 -.01 .453q .OFoP .060 P .00o 3 -.nO 13 -.00 2_lP, 3Z -,0_ ,F_ ,F ,nqn3 ,0497 ,00o6 -,0033 -,007_14,57 -,O3 , 64Rq ,lppp .0677 ,0002 -,007] -.011 _16 ,P4 -.03 7460 .lTnO .OP4P - ,00?3 -,008_ -,012819,15 - ,01 , 8_3f o?4_q 10 61 -,0060 -,OG k6 -,0 027

r t _ 77

ALPP_ m ETA CL _n C_ Cp u CYP CSF

]. _ F .oo . p 73 4 .0 3 Pl - .OI S P . 00O 4 - . 000 _ .0 00 3- 5 ,_ 0 * u o - . OOgl .o 3n 6 -,041 6 .On Oq - ,o 00p ,000 3-p. 9 7 .00 . OP_ .npoO -.0 3 04 . OL_ o 6 - . o o op ,oo c 3

-.74 .OO ,]TCq .npTF -.NP2g .O No7 - .00 0_ .NO0_1 .5 : .00 ._ 7 01 .n y lq - . OI P A . Oo o_ - .O00_ .nOn__. 7 q ._0 ,3_03 ,Oa l_ -.0134 ,Onq l -,0004 OO O4",qq .O0 .4 317 ,o=a l -.OO P3 -.On(,1 -.000_ . On OpP.l a . o o .=17 P . 0 7Pq oO l _ . o n o] - 00 0 7 -. OOlO

lO,a_ , O0 ,607_ ,OqO5 0076 -Onn 7 -,001_ -, 001 _I_ .7 7 . .02 o 7 1 35 .1 1a n 0195 - . 0 , ) 0 1 -._ 0 _ 3 - . 0 0 711_,q5 -,02 .TPR_ ,IPP O o_0o - ,o015 -,COb l -,o0_17.2P .. 0 7 .P P7 7 .;_77 . 0 60 , -, On ? q -.o071 - n l 3 V1q,51 -,0] . q _l .3Qq7 .0835 -,00_0 -,0037 -,0036

1."4 ,oo ,p7_ u .o3Po .0 1 _5 .OooE -. OOO4 ,ooo_

_Lt'F_ nF1 a CL r _ CP C_ (IY N C_ F

1.53 ,00 .271_ . n 3n c -,OlqO .000_ -.0 0 0 3 -.0004- 5 ._0 ,CO -.OOF 6 ,qT_ -, o_l_ ,Onn q ,0000 -, 0 0 07-Pq7 . Uo ,0_7_ . (.pTq -,0305 oOnn 7 -0001 -,0004

-. 7 _ .oo .1 7 q F .np_4 - . 0 23 5 .On 0 6 - .O00P - . o eo41.54 -bO . ? 7 01 . n _o5 - .olql .Onn_ - . 0 0 0 3 - .no n33,7P ,00 ,3ara ,_3o_ -,0140 ,000 2 -,000 3 -,0007_ . q _ .CO .4 7 _ 7 .n _ lP - .OO PO ,onno - , 0 004 -. o0 0 qP,l n ,00 ,_135 ,0713 ,0000 - ,Oq nl -,o00_ - ,OOC _

10, 4_ .Go .6 04 F . Oq n _ ,O lO l - ,On07 - ,oOl a -,OOP O12,7_ -._;_ ,710_ . l_p_ ,0_5o -.Oo n 3 -.ooao -,0 07_14. q _ - .0 2 .TP a _ . .l a _ .0_05 -.O o nP -. ( ,Oh 3 -,OILS17.20 . . 0 3 .t 7f . P .Pa= = .C70P - .00 3 _ -. ObTP -.01 2q1_,_ 7 ,oO ,q_ 7F .37? n ,on2 0 -,0n7 2 -,OOA] ,O01P

1.El , UC .}7_ ._na -,OIPP .0{105 -,0003 0_00

_t_ Eo

ALr FA _E TA e L CD CP C pw CYN CS F

1 .14 _.0_ ,IP_F . nl_l . 01 3 1 . Onl 3 .00 5 1 -, OOIP-_,h_ _, C2 -,lF7 l ,n7o = -,01 07 -,On S ,0 085 ,n 3flp-3,40 S .0 2 -.t .731 ,Opt6 ,O CIP -,0015 .007_ ,01_5-1,1e F ,e_ .o_rP ,OIQI ,OO P7 -.o ono ,006_ ,00_1

l.ll _.0 ) .17{:3 . o 1 _ 0 .0130 .0 o ]_ ,OObl - .OOln3 ,3q 5-e 7 ,7_47 ,n lO _ ,0193 ,oon4 ,o0_ -.noP7_._P ,OZ ,_F3 = .0773 ,0_74 ,ONTO ,eO_5 -.Ol_q7.7q _,0_ .3_72 .nan_ .0 3_ q .O NTO .OOe_ -._)_ 3 3

10,03 _,01 ,45G3 .nF;6 , 0477 , 0{1_3 ,006 9 -,03_P1_.31 4 ,Sq .E',gq ,to31 ,06_8 ,OlPP .00 71 -.n53a14.54 4._7 . 64 ; _ . 1 3 _ .o_1 ,011 7 .O0_P -,071716. PP a . b_ ,7_71 .lOlS . I 0 5 7 ,OoT T . nOl_ - 07 4_19, 14 F ,Ol ,paq q ,p_O .IPqq -()o3_ ,( .o 63 -.0761

1 . 1 7 c . n_ .1 7 1 r .OI _ P .nl 3 ? . _nI F .o o b| -. 00_ ;


25/70

TABLEAll. - CONTINUED. 19

_U_ 30

_LPP_ pLIA _ L CP CP C_v CYP CS F

1.13 le. Or .1;53 .n? n; .0151 .OOP 3 .012 9 .O00E- 5 . _0 In . O_ -.1 4 P r . r_42 - . 0 13 _ -. 0o7 3 . O1 7q . 0_ I I-2.25 10 .1'6 -.053P .O?q_. -.0024 -.on4_ .0161 .038_-1.I_ j_.Oe .03F4 .npP3 .005 7 -.Oop7 .0141 .Ole3

1.19 IQ.OE .IE57 .n_ n4 .0150 .00 ?3 .0130 .OOn53 .4_ I 0 . 05 ._ 1 7_ .OP_I .0_4_ .once .O 1 2q -.0 1 7_

5.55 1_.04 .304P .r_4 .0354 - O IP_ .OI3A -.0 3537. P5 _ . 03 .3 9 4 0 . n4p_ .0 4 P2 . OI F O . 01_ 4 - . 055 4

I0.11 Io. OC .4P_7 .0701 .0_50 .O jpP .O1 7p -.OeS_IP.4 1 q .q_ .5P12 .1036 .OPI3 .0 714 o0165 -111 71 4.6_ _.g 7 ._ P_7 .147 6 .I01 0 .Opol .0160 -.13 2 P

16.q_ -q_ .7_1 3 .Pn3P .1251 .0145 . 0175 .142P1g . 25 In .n O . _7 . _76_ .1 544 . 00g 3 . 0155 -. 15g ]

1.1_ _ .u5 .12_ .0?ol .0154 .Oop5 .0130 -.0005

_LPP_ p ET_ C L rp _P c _. _yp C_ F

1.0_ .on .lb O_ ._17 1 .o146 .O nN_ -.OOO p -.OO C_-5. 7 0 -_0 -. I P 6_ .O4_P 0103 .Oon9 . 0 0 01 - .0004- 3.4 7 .o C -.0_7= .Opa6.00E5 .0010 .0000 -.00 0 S-1.23 .UO -.Obl l .0;lo ,010 6 .UOn g -.0001 -.0003

l.O5 .00 .0_0 .0 171 i0146 .O00R -.OOUP -. 0003

3.3_ .00 .iq_9 .nlPP o l b_ .bOO6 - .0001 -.O00P5.57 .00 .E7_O .opt4 e211 .OooP - .o00S .0oOP7.76 ._0 .? Cr .n4pO 0307 .000_ -.no0 1 -.GO00q.q3 .11 0 .4_ 10 .(,_ 044 1 -.Onol -.1_00_ -.0020

12.2 3 -.03 .514P .ri m3 ? .n54_ .O n p 4 -.0027 - .0 1 1114.44 -.04 .(,037 .1P07 .0716 . OOpq - .0057 -.OI7S16.74 -.o 4 .700P .1_ 77 .OP_P -.oopP -.007S -.o]7q1P .q_ -01 .7_44 .PLY4 .lOng -.0 070 -.0066 .0043

l.Oq .o0 .IOPF .01A7 .015 1 .Onoq -.0003 . 000_

_U_ 32

_LPF_ mi Te CL CP C P Cpu C_h C_F

l.O P . 0 0 . o q g 7 . n l _l .01 4 7 - 0008 -.0003 .0000-5,_q .00 - .IP74 .0_4S -.010_ .0010 .0000 .0000- 3 .44 . 0 0 - . 0q 7 4 .n? n_ . 0 0 2 1 .O_ ll -. O00 p - . 0 004-1.2_ .00 -.001_ .ep ]_ .010 3 .Oong -.O00p .00 00

1.07 .00 .0q74 .n iP 3 .GI_5 .000P -.ooo 3 oO OCn3.33 .00 .lqlO .npnl .01_ .Ono _ -.po03 .O00l5.57 .00 .2 7FP .O_7P .oP0 3 .OooO -.ooop 00017.75 .00 .255_ .04?4 .O$BP -.00o1 -.0003 -.no0_

10.01 -0o ._34= .oS_3 .03P4 .0001 -.0010 -.OOP P12.2_ -.02 .5_6 .OP?_ .0495 .00ig -.0035 -.nln_14.50 ..04 ._ ;_5 .11_ = .0613 .0027 -.0071 -.016416.77 ..04 . 723P .I_FI .0741 -.00;3 -.007_ -.016_19.04 .0 0 .P llq .P1 75 .0914 -.0057 -.oOb6 .0003

1.09 .00 .1010 .01Pl ._1 4_ .O00 P - .0004 -00 03

P L_ 33

_LPP _ pET_ CL CD C_ Cn _ Cy_ CFF

1.52 .00 .2_18 . 0_67 -.0_04 . 00q8 -.000 4 -.0004- S . 24 .00 -.015E .n410 -.0436 .oolo -.000_ -.0001-3.0 _ .00 .07 23 .0_34 -.03 1fi .Oon_ -.000_ .0001

-.78 .00 .164_ .03J3 -.0 _41 .Onn P -.0004 .00001.53 .00 .P60 E .0347 -.0207 .000 7 -.0005 -.no033.77 .00 . 34 7 1 . 04 P8 -, 0171 * 0 0 0 2 -. 0004 . 00 0 3

5.97 .00 .4__ .n_61 -.0 125 -Oonl -.0003 .O00l8.20 .00 .51EP . 07_3 -.00 63 -.Oon4 -.000 5 -.O00 p

10._3 .00 .5P57 .n_ .0065 -.oon2 -.o011 -.001_12.69 ..0_ .674_ .1_7_ .0 1 7_ .Onl _ -.003_ -010314.96 -.04 .77 1 3 .171n .0304 .Onl_ -.0075 -.O lE _17.20 --03 .P6 5P ._P 30 .04 70 - .One7 -.007_ -.013319 . 4 0 .Off ._ ] p .27_ .0675 -.On e4 -. oo4 P - 0020

1.5P . 00 .F6 3 _ .n q4_ -.070_ . Qon7 -.0005 -. nO01


26/70

TABLEAll. - CONTINUED 20RU_ 3 4

ALPHA F&Ta CL CP C_ Co L, _y V C_ F

1,5 1 .Oo ,2_ IS . O_P _ -,D20 R .0007 -, OON_ -.O00B-5.2A .00 -,0 1 6 7 ,nAn? -. 0 43 N ,O 01l ,O00 I -, O0 0 P-3,00 .00 .0 71 6 ,O)P _ -.03 17 ,Oo n q -,O00I -.O00B

-. 7_ .D O .1 6 2 F . OPQ7 -. 0 2 _ 6 .O o nq -,D O0 ? - , 0OOF1 ,51 ,0 0 . 25_? . 037_ -. OPO_ , Oo n7 -. nO03 -. O00 B3 ,76 ,00 . 2 4 57 .o_O p -,0 177 . Oon _ -.0 0 0 5 ,0 0 0 1

5 .g_ ,uo . 4_ 2 F .OF ] 6 - . 0 1 19 -.Onn l -.000_ ,000_8 , 1B ,00 ,_Oql .0743 - , 0046 - . 00 03 -.O00a -, 0 00_

10,3q -, 01 . 57 @q .OQn n . 0090 .OnO3 -. COIl -. OOP6

12 , 65 -,0 3 .66 7 _ . I PP O , 0 2 13 ,0 0 19 -,o0 3 6 -, 011714.q0 _. b4 .75P _ .173= .03 g_ ,On l 7 -,00 52 -,Ol_q17 . 12 ., C4 . HE35 . 2 7 7 P .05 5q -,On_ b -, 0 0 73 - . 0 15 119 . 37 ,01 , q2P7 ._0 ,0 772 -, 007 _ -.0 0 5 7 .O 0 4 P

1 ,51 , 0 0 ._6 1 4 .037_ - .OZOg .C007 -.0003 - .0007

_UK 35

ALPHA mETA CL CP C X Cp u CYF CS F

1,0g F .0 3 .1 05_ .Ol ql .O I 2B , 00 03 .005g ,OOP_- 5 . 67 F .U4 -.17q7 . P 4 _4 -.OIl q -,0035 .0093 ,03_0-3,46 5.03 -.O PP1 .0315 - .000_ -.Onl_ .n0 83 .0 2_2- 1, 22 c,O 3 .0 0 5 _ .07 ? 6 .OOe P - , 001 3 .0o 7 3 , n121

l.OP =. U3 .104 3 .nlqO ,0129 .O on3 ,O05q ,O0_P3,3_ F.02 . lOlq .n_ ]7 .017_ ,0n36 .o055 -,n066_.5_ c. O_ .277 0 .e3 n2 .0 2 _4 ,O o_ ,0055 -.0 1A 47,75 _ .,02 .257_ ,n44_ ,03a3 ,Oohq ,O0_F -,017_

I_,2 F 5 .0_ , 51Pl .o_ q3 .06 3 0 ,0 0 _ 7 .00 51 -,n 3 e lI_._ _.00 .6 0 _ 4 .l P no , 0 7 6 F , Onq_ , 003_ -,0_5_1 6. 72 0.uO .6_ 7 0 ,Ia_7 .O q 4_ .00_5 ,005_ - , 0 01 61_,01 F,o4 ,eo_ .P3o1 ,11_5 ,OoA4 ,OOq7 -,0_37

1,0_ :,0 3 , 1 _ 5 1 ,nl_ ,0 131 ,0o04 ,o05g ,0023

\.

_l'k 36

_LPv e n tt_ CL r n C_ Coy CyF C_ F

],ll 10,_ ,113_ .nP_ .0 127 ,001 1 ,nl_O ,00 70- E-FI Im. Oc -.1 5 P C ,_=?n - . 0 1 6P -.00 77 .n 1 9: .06qn-2. 4 0 I O.(;P ,O_5 F ._c -.OOA g -.Cn4_ .OI Po .0 4 _1-I. 1 6 _0, 07 .O? FC .0 7 7 2 .O0 2 A -, Un pl .015Q ,02AP

1,11 lO,U_ ,1 1 _ ,_747 ,0126 ,OnlO ,o 13Q ,00713,37 In,06 ,I_G_ , pp71 ,O_lq , 0 0 5 q ,013? -,01055 ,_ ] 0,0 5 . _Q I _ . n_: ? .030q . 0110 , n1 3 1 - , o P TY7,63 _,u_ ,377p ,n_n a ,0420 ,O IJ_ ,n 13_ -,04 16

1 0.05 I n. Co , _5_ 7 . 07 _ , 0F93 ,0 1 _ 3 , 01 1 6 -,05qa12,30 in,0 3 .5_ .lnl ,07_ P ,01_6 ,01 37 -,0_ ?14,5 2 in , [.? .63E P .13P_ . Og_ F ,0 1 19 ,OIBl -,O_ P_16.81 _0.(2 4 .74 FE .lm74 .1070 ,O l&O .0 243 -, l lt q1_,1 3 Io.04 .p4F4 ._4_ ,12_3 ,noo_ .n 266 -,1 2_1

1.11 1r-c6 . 115a ,np4 7 .012_ ,001 1 .0141 ,006_

_L_ 3 7

_LP P_ mE T& L Co C_ Cu u CYP C cF

1.17 .u_ .1_7 .PI_; .0204 .00 11 - .o00_ -.ooo_-5.iF . co -.l_'l q .o_p_ -.co 22 ,un_)_ .o00 1 -,00o_- 2 ._: .O h -.0_ 2 C .n?_P .OOg4 .Ooi_ ,0000 -.0 0 0_-1 .1_ .uo .020a . n il6 ,0171 .o)[I ,COO n -,_Oq:

1.12 .o0 .1_30 .n]_ .n205 .Ohio -,tOO2 -,000_2, 4 _ .Uo ._12_ .fpn a ,0_ , o nlo -.0003 -,0o0?r F I , GO , _ q _t . q ] ] _ , 0 _ _ 7 _ ,00 0 7 - ,00C3 - , 0 00_7._2 .bF .57_; .0=_ .CEC4 .00 01 -.OOO= -.001 1

1C. I _ .U C ._&O ._7_ P .07 71 ,nnn5 -.001= -.Or)I P12._c ..01 .Fr l,;' _ .)p_ .lOO P .Un]_ -.0037 - .06_414.77 _.07 .71qC .IP_ .13_7 .On lv -.noep -.ol_n

19 .7o -.t' Z ],(_7_ ._ 74P .lqOq -.U D_ -,IOPS - ,_07 P

l . l _ . Vf, . i_ . r l C_ , . O_ O_ , t Oll -,O(*b? , O00_


27/70


P ( ' h 3 P

_LPH_ _ETA CL CP CN C_ CYP CS F

] . ] 4 .ON .12_F . N]6 7 . 0 _07 ._(l g -.NUO_ -. O0 0l

-E. h l .o C -.1 7q 7 .n_PP - . O0 33 . ON] O -.O 0 0 P .O00R- 2 . 4 2 - . _0 - . DFP_ . np_ = . 0089 .O0 P -.ODOP . O0 0 n-l. lg . 0 0 .01_7 .n]P3 .ole6 .O o l O - .OOO_ .oono

l.IA . oO .1 _4 1 . n I ?O . 0206 . Ono q -. 00 0 3 .fl O003 .40 - q (} .2 151 . o P t 4 .0 254 .Ooo q - .0 _ 03 -. oO o 2

_ . _ . UO . Tq_ .n 3 1 7 . 0 3 45 . Onn5 - . 0004 -.0 00_7._I . o 0 . 3P 1 7 .n4_ I .n4F7 . o nn2 - . 000: -.flOllI0,17 ,(JO ,_ 9 41 .0 7 7 7 .Ob96 . N()o_ -.oGI 4 -,O0 1 N

17.51 ..GI ._1o(; ,IPYO .oq40 .0013 -.()0 4 n -,006_14,_3 -. t)? ,74e7 .1Phi ,1227 ,Onl3 -,0067 -,0 11_17 . 7 _ -.('2 .Fc 3 T .? c _l . 1521 - .00 ? 0 -.OOPB -.01 4 51o._ 7 -.03 l .e 4 n_ . 3 _1 .IFO C -.nq 4 _ -.n06 3 -.Olll

1. 14 . o O . ] Pf 2 .I )IF P . OE0 7 . Oo n P -.000 3 .O CCN

ALPFA pE T_ Ct. CP CF' Cp . ._ CYP C_F

1.5_ .{JO . F Fl_ .n 3 aP -.OIZA .Onn7 -.nO0_ .non4-5,2a .oO -.0 1 23 .0_ -,0351 .(; On(_ -. o O0_ .0_0 3-2.q_ .00 .e_2_ .ePe_ -.n2Z q .00_7 -.0003 .OGO4

- . 7 3 . 0 0 .1P 3 3 ,oppP - . 0167 ,Oqn8 -.000 3 . 0 00 31.55 .00 . 27g_ . n3 a l - . 0127 .Onn7 -. O0 0 _ .nne_3 . _F . _0 .3 _ 7 . 0 4_ P - . 00_ 0 . 0 0 04 -. 0 0 0_ -.00016.04 .oO ._ 31 .0_ 03 .0034 . OonO - ,0003 -.0004_.2q .u_ .%cTt _ .07q_ .ollq .C _)O -,0005 -,000_

10 .63 .00 .e71_ .J P_ .0361 .OonP - .0017 - .O0 |l1 3. 00 . . U2 . 7 ' 3 7 3 . I n 0 3 .062 7 .Oqn_ -. nO4 P -. 00 _15.3_ ..u_ ._ IfF .;a_4 .e g:4 -,On o_ -.o07fl -,010717,_7 -,03 1,03_0 ,_P .1314 - ,Oq_O - .00_ -.011 _?0.0 . ,0 3 I . IR_ O .4 1 _? .16s6 -,00_0 -,O06P -, 0 11_

1.56 .UO . _F_F .OY_ - .0 1_ ? . Oo n7 -.000_ .0 0 03

rt.K 40

ALP P A FEI a _L r n C_ C_ , CYP CFF

1 .5_ .CO ._7Pl ._p C - . 0 1 _6 . 0 0 1 0 -.0003 -.noo?- 5 .21 . uo -.0 1 24 .n3 Fn -.0 34 B . oo o_ . 0 000 -. o oop-2 . q7 . on .Oe lf .npP4 - .02 2g .O()n q -.{) 001 - . 0 0 03

- .7_ . 0 0 .1_ 4 e .n_ Tq -. 01_8 .ol )] o -. oOOP . O0 0 p1.54 .O0 ._7_ 3 .0331 -,01_5 ,O nlO -,000_ -.OOOl3,80 .UO .3633 .04&_ -.0057 .0007 -, 0005 -,O0_l6.0_ .00 .445_ ._o l ,G055 ,O00P -.0003 -, O00P8 . 2@ .00 ._27_ . OVP_ .014_ .00o1 -,O00A -.0016

10._? .( } 0 ,_3_ .]2_ ,o411 ,Oon l -,nol_ -,001113 .00 .,0_ ,7e 7_ ,]p_7 .07 00 ,00_0 -,O04P - ,007_15,30 - .o3 ,qll_ ,p_3 .1G3 8 ,OO l5 - . no7 n -,013117,6q -,u3 1.0461 .341A ,1_07 -,ooPe - ._oe_ -,01_12 0. 1 7 -.Or 1.215 1 ,_77 . I 7 1R -.0o_5 -. OUSq -.00_

1 . 5 7 .1} 0 .2 E1 7 .0_30 -.U 121 .oo in -. no 03 -.o0oi

ALPPA mETA CL C_ CW Cp_ , CYF CS F

1,1_ 5 .oE ,1_70 ,0175 .OPO0 ,Oonq , 00_ ,nO on-5,6_ _ ,03 -,167q ,03_ -.00_ -,0040 ,OOe_ ,OEq7-3,_ 0 5,03 -,07e l ,OPq_ ,o06_ -,0037 ,0054 ,Ole?-1,1_ :,02 , 02_ .nln: ,0148 -, o017 ,no47 ,o oBP

1,1_ _.op ,1 2_0 ,Ol? _ ,o19_ ,_NN9 ,0041 ,OOOO3.3 _ _ . 0_ .213 _ .N P P _ .0 277 .t _ ( _ a _ . 00 4 2 -.0 0 775,61 _,0_ ._q6 C ,03_ ,0 41q , O07b , o04 n -,OlSa7. 8_ F-o0 ,3ql_ .n=pq .0 5 96 .OlIR7 .n0 5 4 -,03_7

10,10 _.q 7 .S _R7 ,07_ ,07 _5 ,n lO0 ,0 05_ -,056_12,50 4,q4 ,_ 121 ,l? _g ,lOqP ,0 134 ,005? -,07q614 ,_ 4,q4 744e , lpq7 ,1 41R , OIPP -,_OP q -,OgO617 ,_0 4.q4 ,e777 .;_70 .1730 ,Onn3 -,o0 5_ -,10_119.7_ 4 .96 l,oel P .3777 ,lqOl ,O{iqO - .005_ -.lI P3

1,13 : ,o_ .1_ 57 .O lTF .0_O l ,oniP .oo_n -.oCO5


28/70


_L_ 42

ALP P_ pt TA C[. CP CP Cp _A fyV CS F

1 .IF I0,0 5 . 1 3_0 ,0 ? 1 7 . O_6 P .O o I P , OI Gq - . 0005- 5 . 60 ] 0 , 07 -.1 4_7 .N _ p & - . 0 1 1 4 -. 00_3 ,n 1 4_ .0 57 0-3 . 35 10.06 -,0_5P . opqO . 0 0 T7 -.O n6_ .0130 . 036P

- l , I E 10 . 05 .040 F . n Pp2 . 0 1 2q -. oo3 n . 0 1 1 _ .01 7 11.1_ 10.05 . 1 3 2 P . 0?17 .0 _? . 0016 .o l lP -. OOO=

3.4_ 1 0.04 .P3_ .O_P6 .0415 .0o_ ,ol lP -.O _I P5,70 In ,03 ,3300 ,n_ 6 ,0603 .OIP_ ,011_ -, 04617 . 9 4 1 0 .00 .4 P7 1 .OtiS2 .07 9 3 .0154 . 0 11 7 -. 073_

lO,Z_ q ,96 ._277 , nqn O .1054 ,0177 .0091 -.1112IP . F_ q . 91 . _43 1 . I Pn O . 12 9 P . 0730 . 0 0 7 0 -. 15P71 4.9 0 O . q_ .7 #7_ ,l q l m .1 5_ 3 .01 75 . 0 0 17 -. 1 7C _17. 20 q . 9_ . 9 1 27 . _ 7 _4 .IP 6_ . 01 1 _ . 0 0 2 0 - . I 0 3 61 9.8 0 . 97 1 .0 _ 2 0 .3 7 70 . PI l O .0052 - . 0 01 5 - . 2114

1,17 10 ,05 ,13_l .0P 16 ,OZ70 .onl_ ,01 10 -,oon p

rb k _3

ALPP_ mEl_ CL C D Cv Cmu _ YP _F

1.04 . 00 . 0_ 61 . nP P 3 , 020_ , 000 7 . n O0 2 -. O00F-5 ,79 ,00 -,_183 .ncq q -,0126 ,O nn _ ,000 1 -,O00P-3,54 ,u O -.IPE_ .0433 ,0013 ,0010 ,o00n -,0007-1.2P .00 -.olq3 ,o3PF .0 12 1 . 00 0 7 ,0ooo -,_00_

1,03 ,o0 ,0F45 .OPP3 ,0208 ,000_ ,0002 -,00073.33 .o n .I_51 . n312 .02_ .OooP ,o00n -.00035,57 ,00 .PS lP .n 4nP ,0371 ,000 3 -.O00 P -,00037.7q ,00 .3711 ,0_ _ ,0473 ,OnnP -,o0o3 -.0007

1 0 . 06 -,01 .4 5F0 .07F_ ,0 635 ,On02 -,000_ -,OOE_]F,2P -,0 2 ,5361 .flq 6_ ,O80 A ,00_0 -,0030 -,00q 414 ,4_ .,04 ,6065 .1702 ,1 023 , OhiO - ,0053 - ,n 15316,83 _,Op .7440 ,IP7 _ .13B0 -,0014 -,0066 -,OOq 619, 2P .00 ,9030 ._7_5 ,1653 1,0 _77 - ,P O6p ,000 3

1,03 ,00 .OPFI .oPT q ,0211 ,Ono_ .0001 -,CO03

_Uk 6 4

ALPH_ pi T6 CL f_ CM _pM CY_ OFF

1,03 ,00 .Op4p .n? ?q ,0210 .Oo n_ -.0001 -.000 3-5,7q , 00 -,E17_ .n_n4 -,0135 ,0007 -,0001 ,0001-3,52 .00 -,IE?? .0430 ,0011 .Onnq -,ooop -,000 3-1,29 ,00 -,oE31 ,0330 .0 132 .Oo n_ -.0001 -,000 2

1.03 .00 .0_43 .OP P2 , 0_0 9 ,O( It)R -,000 1 -,00023,3_ .00 ,1_7P .n 30_ ,0270 ,OonP -, 000 1 -,000 35,60 .00 .p07_ .n3q 3 .o341 ,0000 . -,O00P -,o00 37,_3 ,00 ,3_P3 .0_40 .042P -,00o 3 -,nO0_ -.oOO R

lO.Op -, Ol ._70P ,n73_ .056P -.On o2 -.O01 P -.OOP P1_.3_ -,0_ . 55_? ,oo_4 ._719 ,Ont) 6 -,o03P -,00_11_.54 .,03 ,_3_ ,IPP1 .0915 ,Ono_ -,005_ -,014316,he .,0_ ,7_0 ,IP PP ,133_ -,OO l_ -,0070 -.00_ PlC,3I -,01 ,q15 5 ,?F _P ,159 2 -,0 05_ -,005_ -,o02n

1.04 .00 .OrP l .02PO ._213 .non 7 -.O00P -.OOOp

FUk 45

_LPP _ p ET_, CL CP _ Cq ,_ f. YN C=;F

1.4q . oo ,pf41 .o '3 v - ,0125 . Onn(- -,0002 -,0001=.2 _ .0 0 - . 0 3 _. .0_41 - . 0_ 50 .O nn6 - , O00p , 0001

-3,OF ,00 , 0_/'1 ,O4_P ,0305 ,0005 -,O00 P . ,00_1-.f_4 .oo . ] ,_ ,04 |3 . o_00 .ONo. _ -._o0_ ,oo01

. _.... 4 . o/. 37 01_4 ,00o. _ -,eo0_ -,OflOp3.7 F . OC .3F . _ 'q .00 32 00 6 5 ,0001 -10003 ,OOfl O

, 6,0. r - .00 .6r_7 .oFq4 0003 -,ONI )_ -,0003 ,0000F ._7 .00 ,r -4 jO . )P(_IF O 1P3 -,OI)O0 -.0005 -eGO07

10.57 -.01 .FS] I .1143 0 ZF, f-, -.000 _ -,o011 -. 0 0 2 7]p.TP .,u; _ .71Pq .141 c 040G .000 4 -,0033 -,oOg ]i 4.90 - 03 .794 P . 177n . e6 4_. - 1)onq - . e034 - . 0 ] P7l 7.24 . (;_ . _7_ . _&PF * ] 002 * (-IIt _q -- . r| 0 _ .'_ -- . D o_r;t:1 q*_v - ' b l 1.0t'90 .3FO4 1 4r '7 -,OOZ E -.no40 -,OPt*7

]..t.O .(in .p .r. 7F .0437 - ,G1_4 ,0005 -.0003 -,00C4


29/70


I:;UF 4_

ALPF_ pL Ta ('L C P C w CpM CYP CSF

1,4e ,oo , ;-4c )o ,n4 36 - ,ollq ,0007 ,OOn l -,o(}1_-5.2 _ ,0 -.O_' Oq .n_SF -,0450 .Oo oq .0000 -,oOOq-3 .OF ,00 ,OS4 F . q,44 . -,0316 ,OOnR ,0001 -.0010

-.P_ .o n .l=O q .n,nq -.o _on .oo07 ,0o01 -,O01l1.47 ,u o .P4 f 3 .04 37 - .01_1 .Onn7 .O OOl -.00173 ,77 ,00 ,34F7 ,05 :_7 -,00 40 .Oon 5 ,noon - ,00076.03 . 00 ._4 7_ .P? 03 .0020 ,onnl - ,eO 0_ -.GO0_8, , ;E . OO ,.=. 3 4_ , nat, =_ ,0155 , oono -, n o0 3 - , 0 01 3

]0 ,4 7 . ,O l , F If--_ , ll 4 P . 0 3 0 4 -,no n 3 - ,O00B -, 11 0 3f- .I P. 7 3 -.u3 . 7o o 0 .i .. 1q .C4 7q . Oon8 - . no3 ] -.ol i n14.q 2 -,04 .7777 .1741 , ('7 3P ,Oo n6 -,i}0o7 -,017017,3_ -.OF ,q _9_- .:_=: _ .4 .10 64 - .('033 -,O0_] -.007319 , 7 7 .O N 1 , 06 2 & . 7 4q;3 ,1 46 2 - ,o n t o5 -,o05 f . , 00 1 7

1 . 50 , no , _540 , n4 3 7 - ,0 1 17 ,()no7 , 0 0 0 1 -,00 1 P

_ t ; I x 4 7

ALP FA uE T_ ('t CP Cf_ CpP. , (-yp v CSF

1,0_. _, 0 . , 0 P75 . {} 31 f ,01_ 7 -, On P5 ,00_# , ,n l Jl- 5 ,7p =, o_ - , ? I 4 F , n_ . 3 _ - , 0 14(, - , one 7 , n 074 , 04 3 3-3 , =- F . = , 05 -, 11P 3 ,l4q -' _ - , 00 07 - , on so ,006 5 ,0 3 2 3- l, ? -. ' .- =, 0_ -, e l bC . n S F .; . 01 0 3 - ,On 3 6 ,n0 5 4 , o_ Z. 1

l,O.r :. t;r: .OF re . Oai 7 .t}lq4 -,0024 .0043 ,01333 ,3 4 =* 0-= , I I _- ; : . n3 4n , n_ 7 .'i -,Onf1 3 ,o0 3 5 , 004 05.61 _ o{ : f. ._P? 7 , n ,.,. , 0 3 0 ? , On lo , on3n -,00 177 .F_ O _ .t' F .3 ( .PI . I) _- _ . 0520 .O, s F .O 02P - . 0 C6 _

1 0,04 c.. O& . 4_ 1 4 . 0707 . n(07 ,(,077 ,n Ol 0 -,0 1_31?, 34 _* O--= ,_FI O , In_q .Oq{l ,O t I Ql ,noo n -.037414.59 ,.';in ._r_r ] 14r'_ . I P06 .Onq4 .nO l_ -.0_501 6 . O_ 4 .5 4 . 70= . 1q 07 . 14 37 ,0n73 . OOZ'4 - . Oq l 71g. 33 4, 9 7 .q14 1 -;_7 _'_" ,1710 [_;11]q , O04 7 -,0q 63

1,04 r ''O= . OP7.) .031_' . 01 r ;_ -, O nP,4 ,0043 ,O12P

rUN _

ALFP _ ofT# L C_ C P Cn _ CYN CF F

1 .05 ] o . lq .o q o_ . h 3 7 n ,0207 -,One5 ,O]Oq oO_F_-5 , 7 3 I n , ll -, 1q9_ . n_ q 7 -. o1_ 4 - , 0 1 4? , Olb q . 0_6_

-3 , 4@ ]n- lo -.1014 .oF| q - . 0 0 46 -,01_4 ,0145 ,OF*I-1._3 .n,lo -.eOb_ .n4 1_ ,00_ - ,Oon_ .ol_6 ,045a

1,0 5 Io ,l O , 0_94 , n_n , 0_07 -,0n_6 , 0 11 0 , O_q?3 .33 In ,lo . 1_7 .o4n4 ,0333 -,Ooin ,olOp ,fllSn5,5 a l O*ll . P TP _ , 04 q 4 .0_ 7 ,0 () i_ ,O O9 _ -,0 0] _7.P4 l _,lo ._77F ,0 674 .07_4 ,00_ ,00_ 7 -,O_S q

I0 ,I _ I, , 0 7 , 4FC F .nn31 ,0960 ,0 11 0 ,n0 9 7 - ,05 6712 , 4 0 i 0 , 04 , F OI7 . IP ql , I_ E7 ,nlSp ,oog 3 - , _q C_14,76 1 _,Ol , 71 OP .171 0 , 1 5 27 ,0115 , no 77 -, ] _ I _1 7, 1 4 q , _ 7 . P =O_ .?_?_ .1 7 3 4 .O l i n .0 07 3 - ,I FF 4

1,o+ l e ,l O .OGI_ . n 3 7P .OEOQ - .0065 .nlOn oO _n_

RUk 4 9

ALPP _ _t1_ CL q_ Ct ' CO,_ CYP CSF

1. 17 . 0 0 .13 01 . olvo .ooOu . 0005 - . ooop - . 000 7- 5 ,5 9 ,00 - , 1 4 9 1 . n HTF - ,0 _6 7 ,O on_ - , n o n4 - ,oo0_-3 ,34 ,00 -,n540 ,o p41 -,o1 35 ,Oon_ -,no04 - ,OOe P-1,10 - 00 ,04 03 ,_17 P - . oo_o .oo, ) 6 - . no u 3 - . non_

1 ,17 ,uo , 1 _ 9 4 ,n l _ a , 00 80 , oqn5 -, OOU? -,0 0 0_3 .3_ ,00 ,PI P_ ,qP o3 ,n]5_ ,coo p -.oOop -,000_5,@1 . bO ._qlP .027q ,OPE 3 .1)0 00 ",000_ --,OO n_7 , Rp ,00 ,2 75 P , o_ n l , O_ P4 -,O oq 3 -,nO0_ -,O0 1F

10,05 ., 01 ,4 fS E ,n_ o= ,0351 -,POol -,oola -,n0 3 112.3 n -.01 ,_n l .on_q .04P7 -.O qll -,003_ -,00_

14,53 .,0_ ,63_F ,IP_O .n_2q -,on1 3 - , o05 3 -,010016.80 --01 ,73 _0 , 1_o_ .07_.q -.0n7 3 -,0067 -, O05p1q,17 -,Ol ,_4 73 ._470 .OqPI -,0n7 3 -,nOe l -,0030

I,I_ ,00 ,130P ,01_7 ,OOP 3 , On n4 -,O00 p -,0004


30/70

24TABLEAll. - CONTINUED

_U_ _0

ALPP_ p El_ CL cn C P CpH CY W C_F

1.17 .uO .130P .n169 .0081 .00o5 -.O00_ -.0007

-5._P .00 - .14_ .0373 - .0267 .Oqn 6 -.rO04 -.oooP-3.3? .00 -,0534 .0?_0 -. 0133 .On09 -.0004 -.0000-I.11 .00 .04 (_S .n 177 -.002 1 .On06 -.000 3 -.no07

|.18 .00 . 129P ool6q .0079 .Oo nS -oOOO p -.oo u73,41 . OO ,P IE4 .qP 04 .01S 6 .Onn3 - ,000 ? -.nO075.6P .00 .291 q .O_7q . 0221 . 0001 -. nO0 3 -.00117.U1 .00 .374P .0400 .02_6 -.Onp4 -.0005 -.0014

lO.OR -.01 .463_ .n6n 7 .035 0 -.Oonl -.0015 -.0031IP.30 _.02 ._3_4 .OP _m .0487 -. 000 7 -.n 03_ -.006714 .55 -.02 .f 315 .129_ .06E7 -.0016 -.005 6 -.n0 9616.82 -.Ul .735_ .1An q .07 _6 -.0075 -.007_ -.n 04619.13 .00 .P403 .?4_ .o97 e -.0n77 -. 0084 -.001_

1.17 .00 .131_ .nl_n .OOP3 .no05 -.o00P -.0004

nUk _1

ALPHA pLT A CL Cn CH C UP CYP C SF

1.17 .00 .1314 .O]Tfi .0083 .OOn 4 -.0004 -.0004-5.5 e .00 -.1 489 .03 AO -.0266 .On 08 -.0005 -. O00 R-3.33 . o0 -,053_ .n?4_ -.0134 .Oon 9 -.ooo A -.OO lO-1,10 , 00 ,0 39q ,0]o4 -,o0]q ,0007 -,0 004 -,0006

1.14 .00 .12e7 .olnl .0080 .0005 -. 0004 -.000_3,39 ,o 0 ,212E ,o?1 _ ,015 9 ,oon2 -, oou4 -.ooo _5.61 .O0 ._q17 .o Pq l .0_26 .O000 -.OO0 5 -.OO ln7,no ,00 ,37 60 .N41_ ,02q3 -,0 004 -,000_ -,OOlq

IO.O P ..01 .4670 .06P2 .0338 -.0002 -.0015 -.O03 P12. 32 -.02 ._4_ .n_TP .04 47 -.Oon _ -.0033 -.O 07m14.4q -,02 , 615_ ,l? Oq .06_4 -,O op5 -,0 05] -, 010616.69 ., 0_ ,6_6_ ,I_P ,090_ -,OoA6 -,007 _ -,00731_,q8 , 00 ,TPP_ ,P _3P ,11 0P -.0 067 -,0085 -,0 01_

l.lP . ,o O .]31_ ,nl7? . 00_ 3 .000 4 -.000 3 -.O0 0S\.

PUk _2

ALPM_ pET a CL CO C N CR_ CYP C SF

1.18 .00 .132P .0171 .0002 .Oon 4 -.O00& -.no04-_.59 .00 -.14qe .n 3_l -.0267 .0007 -.0005 -.ooc_-3.3_ .O0 -.OS_O .O p4_ -.0137 .uonq -. 000_ -.000_-1.13 . O0 .0 400 .Ol_ -.0023 .00 _7 -.O00_ -.0004

1.16 .00 .1301 .0170 .O07q .000_ -.000_ -.00033.40 .VO .pl4] .0;1 _ .0157 .On0 3 -.0003 -.000 35.b 4 .00 ._9_4 .q pq_ .O_2P .(_onO -.nO0 5 -.00077.R_ .00 .3_1 .043 & .0_ -.OooP -.11007 -.COl&

10.06 -.Of ._0 .06?7 .034h -.Onn b -.t_O l_ -.002_IP.32 -.o2 ._4q F .o_q .0448 -.Onn5 -. o03n -. on7414,4P -, 02 ,61 5_ ,I?&6 , 065_ -,00_3 -,005 0 -,OOP 616.73 -.UI .703_ ,170P .OP _I -.00_4 -.0078 -.00_

_l,h _ 3

ALPP _ pLT _ CL _P C_ CgM CyV C_F

1.2 5 .00 .13 02 .0176 .O07R .0 003 -.000 _ -.00C6-E.7S .00 - .]65 _ .o_nl -.02q 7 .ono3 -. 000_ .0000-3._0 .00 -.003_ .OP_ -.014_ .Oon 5 -.000_ -.o003-1.1o .o0 .033q .hin t -.o o2_ .ooo5 -.hO OT -.oOo_

1.24 .00 .]_67 .017P .0074 .00113 -.0007 -,00063.56 .O0 .214P .07]_ .OlStl . CooO -.0007 -.0003S.P3 .00 .Pgq_ .o3nn .0231 -.00_4 -.O0o? -.000_R.II .00 .3_ 6P . 043 = .02_6 -.Oon 7 -.0007 -.0011

10 .44 -. 01 ._837 .e6_ .0361 -.0006 -,001 5 -.00 3312.74 -.04 ,_65F .no42 .o_o2 -.oooS -.oo31 -.nlO014.9S - . b_ ._34_ .13_ ? .0756 - .On e7 -.0084 -.016 3

17 ,3e .,Op . 7_ .lq _ .oqo3 -,Oo3P -oOlOW -,n? 07


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25

TABLEAll. - CONCLUDED

ALPh J pETP C L ?P CV C_Pv C YP C_F

1,3F ,00 , ?05_ .n?_P -,0068 ,0001 -,0005 -,0004-5,35 ,00 -,05P2 .0742 -,0435 ,0007 -,0006 -,000 _-3,0c ,UO .0 35P .OP4q -,0 598 ,Oon 6 -,000 6 -,000 _

-,Be .00 ,I _IF .OP30 -,0176 .00 07 -,0006 -,00031,3_ ,00 , 204_ ,073 0 -,0070 , OOo E -.0004 -,nO053._1 ,00 ,2854 ,n_oo ,00] -,O nn2 -,000 _ -.ONO_5,81 ,00 ,3647 ,04n0 ,OOeO -,0004 -,000_ -,00068,0? ,00 ,451 0 .n _ ,0135 -, 0005 -,0007 -, 001_

10,2P .,01 ,_397 , OP02 ,ol q_ -,Oon_ -,0013 -,n0 2512,_1 -,02 , _171 ,lOP7 ,0320 -, S no _ -,0034 -,007716. _? .07 .F604 .1 _0 .05P q -.00_6 -.00 70 -.O0? Q16._P .0_ ,7663 ,10 41 .0766 -o0_51 -,0084 -oOOgq

ALpP_ =LTD (L ?m CV CoN CYw CFF

1,_5 ,00 ._740 .0 _46 -,OZOg ,Ooo O -.00 06 -.000 7_,1_ ,00 0732 .037_ -,OSbO OOn_ -,nO0 _ -,00 0_

-2.HP .bO .] IUP .0_11 -,0440 ,O ff05 -,PO0 _ -,000]-.71 ,00 . lC ;e .e_ n = -,03 EU ,Onn3 -.n 004 -,na_ClI _ .Vfl _723 .0_4 -.0209 _ qi 1_ -._004 oO00n-, .

3.77 .o0 .3523 .n 4_O -.01 35 ion l -.n 004 -.00 036 0 | ,(I0 .433_ ,n=_P - .006 # Onn3 -,nOO_ - .0006_._p .00 . T?4| . OTCE -.O0 2R 00 06 -.O00R -.O0] O

10. 66 ..01 . e c r_ .1o15 ,00 5_ -,8no 6 -,oo 14 -,oo3 _1_._7 ..0 _ ,6771 .13P0 .021 0 -.0o16 -.003R -o007414 ,_ -,U3 ,74_0 ,174F .0_45 -,Onlh -,0067 -.011317.07 ..0 2 ,8 _qP .pP_3 .063_ -,0_4 0 -,O0_q -,0O_n

ALPP _ pET _ CL CP C_' CpF , CYP C SF

1.36 .00 .2007 .n _l_ -.0030 .00 03 -.0004.0000

-5,41 ,0 0 -._P? p .n _ -. 11 6 9 .(,f)nR -.no 0_ i0000

-3.1_ .00 .OlO_ ,0737 -,015 1 .PO O4 -.000 3 000_-.93 ,00 ,1 056 .OJ q7 -,O0 6P ,0002 . -.0004 000 ;1.33 . o0 . 1 9 94 .opjn -.00 30 .O on? -.o004 00o?3.5_ .o0 ._7P _ .0_73 . O02P . 000 0 -.O00S 00015.7_ ,00 ,3576 ,O_P O ,O OP7 -,0 003 -.000_ - 0002_ . 0 1 . o0 . 4 4 4 P . _ 43 oOl_U -.0oo_ -. 0 00 4 0 0 05

lO ,3F .,01 ,53+P . OTVP .0_37 ,0002 -,0015 -,00_41 2 . 5 3 .,0_ . 6 31C .llnl , 0356 ,0000 -,003 q -,0 06_1_ .77 ., 0_ .72 _0 .1_? _ ,0531 - o0007 -,o06 n -, OOq ?17.06 .. 03 ._OE .7nvl .07_1 -.0n31 -.n07 _ -.0111

P Ub 7

ALPF_ _ETD CL _D CV Cp u CYP CFF

.7 5 .00 . 0014 .0 1 F 6 . 01_ . 0010 .00 00 - .n OOn-6,53 ,00 - ,=O lq .P417 -,8103 .Oon3 ,0000 -,0002-4.30 .00 -.I0 7 ? .0273 .0 031 oO00 h .0000 - .0004-2.04 .o0 -.010 5 .01ol .o llq .0o0 8 .000 1 -.O00F

,25 . 00 ,0_13 .01_ F ,0167 .On ll .CO On -,0010$,_ ,bO .]P OI .OJ _Z ,O) _g ,O00g - .0001 -o00114.70 .0 0 . _ 57 _ .n ? _3 .0E 4 9 .On o_ . 0000 -. 0 0 1_

6,93 ,o0 .3303 .03_ 7 ,0331 o0OO 7 .no00 -,00199,21 .,01 , 433P ,n 570 ,0419 o001 7 -,0007 -,0 037

11 .4_ . ,0_ ,F43P . onpP ,05_4 ,Onto -,001 -,OOPP13,74 - . I' 3 . _4 FP .1P qJ ,060o .On p o -,005_ - ,OIPo1610 .,03 ,7_0 ,IR7? ,078_ oOOnP -0090 oO l3q


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26

REFERENCES

1. Robins, A. Warner; Morris, Odell A.; and Harris, Roy V., Jr.: Recent

Research Results in the Aerodynamics of Supersonic Vehicles. J. Aircr.,

vol. 3, no. 6, Nov.-Dec. 1966, pp. 573-577.

2. Robins, A. Warner; Lamb, Milton; and Miller, David S.: Aerodynamic

Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-Body

Configuration With and Without Integral Canards. NASATP-1427, 1979.

3. Coe, Paul L., Jr.; and Weston, Robert P.: Effects of Wing Leading-Edge

Deflection on Low-Speed Aerodynamic Characteristics of a Low-Aspect-Ratio

Highly Swept Arrow-Wing Configuration. NASATP-1434, 1979.

4. Coe, Paul L., Jr.; Huffman, Jarrett K.; and Fenbert, James W.: Leading-Edge

Deflection Optimization for a Highly Swept Arrow-Wing Configuration. NASA

TP-1777, 1980.

5. Coe, Paul L. Jr.; Kjelgaard, Scott 0.; and Gentry, Garl L., Jr.: Low-Speed

Aerodynamic Characteristics of a Highly Swept, Untwisted, Uncambered Arrow

Wing. NASATP 2176, 1983.

6. Gillis, Clarence L.; Polhamus, Edward C.; and Gray, Joseph L., Jr.: Charts

for Determining Jet-Boundary Corrections for Complete Models in 7- by

lO-Foot Closed Rectangular Wind Tunnels. NACAWRL-123, 1945. (Formerly

NACAARR L5G31.)

7. Pope, Alan; and Harper, John J.: Low-Speed Wind Tunnel Testing. John Wiley

& Sons, Inc., c.1966.

8. Carlson, Harry W.; and Walkley, Kenneth B.: An Aerodynamic AnalysisComputer Program and Design Notes for Low-Speed Wing-Flap Systems. NASA

CR-3675, 1983.


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27

TABLE I. - GEOMETRICCHARACTERISTICSF MODEL

Wing:

Aspect ratio ........................................................ 1.838

Reference area, m2 (ft 2) ................................ 0.863 (9.293)

Gross area, m2 (ft 2) .................................... 0.949 (10.210)

Span, m (ft) ................................................ .260 (4.133)

Root chord, m (ft) .......................................... .674 (5.492)

Tip chord,m (ft) ........................................... .161 (0.529)

Referencemean aerodynamicchord, m, (ft) ...................0.895 (2.937)

Leading-edgesweep, deg:

At body station 0.530 m (1.738 ft) ...............................3.02

At body station 2.027 m (6.651 ft) ...............................0.0

Verticalfin (each):

Span, m (ft) ................................................ .107 (0.350)

Root chord, in (ft) .......................................... 0.326 (1.069)

Tip chord,m (ft) ........................... ...............0.048 (0.158)

Leading-edgesweep, deg ............................................ 3.4

Taper ratio ......................................................... .148


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C

L CDWind

Cy

Windc_>

X

Figure 1.- Systemof Axes,


35/70

I b j

L_o.53o2-7o_o-"---_ "',,I (I,38) I.220 _ i_ : O.895-_,

(4.002) -' _371 ' "',,_ I. 7 5 6 f_ '(5.60) I_ \-_ 41.46,

= 2.02 7 _ _n o_,,,,, . _( 6 . 6 51) -1 '

2.487 __(8.1 6 1)

( L_I

a = 0 Referenceine_

Figure 2.- Three View Sketch Of Model. Dimensions Are Given In MetersAnd Parenthetically In Feet.


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2.375 _ i2.326 (7.793)

_. 2 .054 (7.632)I

2.027 (6.738) 53.69 (6.651) O.3132.108 (I. 028

(6.91 7) _[

AO.530(1.738) 73.02 Hinge-line

m m

L_ 0.680_ (2.230) 2.204 _ 0.242I - (7.230) -- (0.795)0.061 O .179

SectionA-A SectionB-B (0 .200) (0 .589)

_40 deflection normalto hinge-line

Figure 3. - Details Of Leading- and Trailing-Edge Flap Systems.Dimensions In Meters (ft) Unless Otherwise Noted.


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b

Slat I

Configuration I1I ii _" Shimhickness_

-- -I

Slatelement '6Le _" 6Le* cm inches

(_ 35 20 .254 .100

(_) 35 35 .254 .100

(_) 35 35 .254 .100

35 35 . 27 .050(_ 30 30 .076 .030

@ 30 30 .076 .030 __ /(_) -

normaltowing, ding-edge (_J /_

6Lemeasuredo increases latg p _- -'--__ ._._.

_Sh im ins erted ea

_racket locations

SectionA-A typical

_:=_51at brackets allstreamwise

(b) Leading-Edge Slat

Figure 3. - Continued


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2.375=_. 2.054 17.632) I I B

:_ 2.027 (6.738) _ -___ /,,,_;"- _ 56.651) 3.69 o

A " A /

.65 . .(1.7 38) [-_

2.2 04 _ 17.230)SectionA-A SectionB-B

_deflection instreamwisedirection

(c) Variable Chord Leadin g Edge

Figure 3,- Concluded

'


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___] P itot-s ta ticrobe

-- ,-- ,_ IttI-" ,_ 111---] 2.13

'_ (7 O)| I O.1.52 / /I/

O.300 _ I. 086 (0.500) //,_l

(0.984) "__. 563) /J i (3. 46 )

,' , / l i ' ii

Turnta bleI

O.69 7__(2.292 )

Figure 4. Model mountin g arrangement in Texas A & M University 7-X lO-footLow-Speed Wind Tunnel. Dimensions are in meters and parenthetically in feet.


40/70


41/70

12 1.0

.o_ _ 0 0 ._ .c,_ _ . s_ [] 30 s "'------- o ,o _.- ._

-.o_ 0 40 .2

-.08 0 "

1.0 12.0

_ i _o_2 L LID J _ 2.o1

F _\ .-'28 -q 0 u_ 8 1 2 16 20 0 .Oq .08 .12 .'16 .20 .2_ .28 01. .2 .3 . ,5 ,6 .7

c_leg CD CL

(a)Vertical fins on, 6f - 0

Figure 6.- Effect Of Simple Leading Edge Deflection.


42/70


43/70

12 .0

04 .6 r

Cm S

o . _ _ - P [] 30 .4 ,_

- . o__ _ ,s ; _ 0 40 .2- .08 0

1 . 0 , 12 .0

Z ,o . _ f 6.0 _ ; _

0 _ - ,.,_ 2.0

-.2_ _ Ll O 8 1 2 16 20 0 .04 . 08 . 1 2 . 1 6 .20 .24 . 28 C .2 .3 . 4 . S .6 . 7

_,_g CD e L

(C) Vertical fin s on , 6f - 20



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12 _j 1.0

.o6 _ / _. 6IF, deg ._

.o_ _ _,_ ..o/ [] 30 _0 _ .4

40-.Oq _ .2

-.OB O

/ oi.o .. _. 12.0

8 _"S - io.o

Lfb2 _ _ _ q.O_ _ 2.0

-'28 -_ 0 4 8 12 16 20 0 .0_ ,08 .12 .16 .20 .2_ .28 01 .2 .3 ._ .5 .6 .7

a ,deg CD CL

(d)Vert icalfins off , 6f - 20

Figure 6. - Concluded c


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39

Figure 7. - Tuft Photographs of the Configuration With SimplyDeflected Leading Edge (_LE = 30u)"


46/70


47/70

12 _ Z 0 1.0 j.08 ] _ Leading-edge //_ _-. ._._ 0 Undeflected . .

[] Slat, i(see fig . 3b) s

-.o_ _ Slat , 1 (seefig. 3b)

-.08 0 n

I.0 12.0

' ,ooy 8 . o \N

_ _ 2.0-'2-8 -q 0 u , 8 12 16 20 0 .0 .08 .12 .16 .20 .2 u , ,L:>8 0.1 .2 ,3 .u, ,5 .6 .?

a ;ieg CD CL

(b} Verticalfins off, 6f - 0.



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12 ( / 1.0_I Leading-edge .8o_I / _ Undeflected .6 / _ %

am :_ .:r [] Slat , l(see fig. 3b)..o...o3:_ , ._I

-.0ul o ._ .2_cr

-.08 0

12.0

"_ " S ' /_'_--,. /_ / _ -- 6.0 /

0 "' 2.0

-'28 -U. 0 _ 8 [2 16 20 0 .04 .OB . t2 .J.6 .20 .2u , .e8 0 /. .2 .3 ._ .5 .6 .7

_leg C D CL

(c) Verticalfins off, 6f - 20.

Figure8.- Concluded


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43

Figure 9, - Tuft Photographs of the Configuration With Leading Edge Slats.


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12 Io0

f_' Intersegment oints .8 -,'"-_ _o8 / _

/0 Sealed i

0_ ,6,_ _. x, -_x''_- /] Unsealed so ,_ .. /oI

-.0_ .2 _,8

- . 08 0

1 . 0 12 . 0

' j ( "%LiD ,

2 m Lt.OI

./, -Oo'2-8 -4 0 8 12 16 20 0 .0_ .0 8 ,12 .16 .20 ,2u_ ,28 ,1 .2 .3 ._ ,5 ,6 .7_g CD eL

(a)Slat I , verticalfins on.

Figure 10. - Effect Of Sealing Intersegment Joints Of Leading Edge Slat Configurations. _f =0

j


51/70

12 i .0

.o8 _ Intersegmentoints .8 _ :_="'_ _-

.o. _ 0 Sealed

o _.._ [] Unsealed s ._-. o_ . 2 o

-.08 0

1 . 0 12 . 0

8 _ _ -_ ] o - _

_ __ 11_ _o . oe f _0 ,,i 8.0

.,. / l =.o .,.,o _ ,. 2.0

o/-'2-8 -_ o _ 8 12 Is 20 o .o_ .o8 .12 .is .2o .2_ ._8 1 .2 .s ._ .s . e

a_leg CD CL

(b) SlatI, ver tica linso ff

Figure 10.- Continued


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. 2 1.0

OB .B

.o_ __. 0 Sealed

cm _ _,_ .6o _ ..-_ [] Unsealed s .4oi-.0_ '- ,2 0

1.0 12.0

8 n _ , I0.0 :_

.s _ =f. 8 .0_14 -- s .o -x

f .._,,f _.oo/-'2_ 8 _u , 0 LI 8 12 1 6 20 0 .Oq .OB .12 ..16 .20 . 2q .28 01 .2 .3 .q .S .6 .7

a,deg CD CL

(c) SlatI I, verticalfins on.

Figure 10.- Continued

g I


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.12 I i .D I oO

.oB Intersegmentoints .B / _, ,.o4 j_* Sealed .6

[] Unsealed s _='_-0 4 0-,04 .2

- .08 0

1.0 , I 12.0

/ -e ,_ _ f _ _ 1o .o "_ -" \.6 =i- ,_...- o.oC1

o._s _ _.oJ-.2, -4 0 8 12 16 20 .04 .08 .12 .16 .2D .24 ,28 O. 1 .2 . 3 .4 .5 .6 .7

_e_ CD CL

(d) Slat i , verticalfins off.

Figure I0.- Concluded


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12 1o0

.o8 Slat configuration .8 , ._.

._ / Nominalsetting / "_

o o ._- [] Largegap(seefig. 3b) s ._ J.o_ of _ Largegapwithoutboard-.oe wingpanelgapsealed .2_

I .0 lS.O

.o ,'," 8.o / _x_/ / -,,,.

, j /. oo/D \o :r 2.0

/ oi.2__ -4 o _ 8 12 is 20 o .m .o8 .12 .Is .so .2_ ._ . .2 .3 ._ .s .s .

_g CD CL

(a)Verticalfins on .

Figure11. - EffectOf Slat Gap. Slat I.


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12 I.O

Slatconfiguration :t'_'_""_

oo "/ "--,_ _ _ "_ 'f o Nominalsetting] Largegap(see fig. 3b) s

0 .... _ Jt_r

o , _ Largegapwith outboard @.0_ .2wing panelgapsealed

-.08 O

0 12.0

8 _f" - 8.0CL / f o.o '_

2 4.0

o = f 51 2.0oi

-'28 -_ 0 tl 8 12 16 20 0 ,0_ .08 .12 .16 .20 ,2_ ,28 01 , 2 .3 ._ .5 .6 .7

_,deg CD CL

(b) Verticalfins off.

Figure 11. - Concluded


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12 .0

_> 5LE,deg g,,.0_ ._ 0 0 ._ _. __--__

o _- 0 40 _ -.Oq .2 []

-.08 0

1.0 _ 12.0

.a -./" Io.o _

CL. 1 _ 6.0 _ "

o %R-'2B I_- _0 q 8 12 16 20 0 .b_I01_ .08 .12 . 16 .20 .2tt .28 01 .2 .3 . q .5 .6 .7

=,deg e D G L

(a)Vert icalfins on, 8f - 0.

Figure12. - EffectOf VariableChord Leading-EdgeDeflectionOn LongitudinalAerodynamicCharacteristicso


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I B

12 1.0

.o, , _ o 0 \[] 20 s -':__

- . OLi .2

-.08 0

P

' i

- 28 -_t 0 U , 8 12 16 20 0 .OLI .D8 .12 .16 .20 .2_ .28 .2 .3 .ti .5 .B ._

a , de g CD CL

(b)Vertical finsoff, 6f - 0. o l--.1

Figure 12. - Continued.


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. :_ I.O

.o8 ._/o 6LE,deg .6 .._. --_.o, _ 0 0 .6 _ f_-'-'_-_-----cm _ [] 200 ,4 /

40 ._-.0

0

-,08

1 . 0 1 2 .0

I0.0

.s .40 8.o

6.0 "/ "

o-'2-8 -4 0 u , 8 12 1 6 20 0 .OU_ .08 . t2 .1 6 .20 . 2u , . 28 0. .2 .3 . . 5 . 6 . ?

_,des' CD' CL

(c) Verticalfins on, 8f 20.



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54

=8

(a) aLE = 20.

Figure 13, Tuft Photographs of the Configuration With Variable Chord Leading Edge.


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55

a =0

(b) aLE = 40.

Figure 13, - Concluded.


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.o, ._ 0 Undeflected _..6 "

[] Simpledeflection, 81F - 30 sO Slat I (seefig . 3b) _>-.Oq .2

A Variablechord,5IF- 2 0-.08 0

1.0

2 L /D "_q.O(

-'2-8 -u. 0 4 B 12 1B 2O 0 .04 ,OB .12 .IS .2 0 .L_ .L>B Ol .2 .3 . q .5 .B , 7

(x , d eg CD CL

(b)Ve rtic alfins o ff, 8f - 0

Figure 14. - C ontinued


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}2 1 .0

o Undeflected.o_ _ _ .s

c,_ ._G _ [] Simpledeflection,6LE=30 s /_

-.o_ _:___""


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12 1.0

.o_ _ 6 deg ._ _p___04 _ .6 o

o _ _, _ [] 10 ..'_


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.12 1.0

.o_ 0 .6 /

o > .v" [] 10

_ _ 20- .OB 0 O

1.0 12.0

10. (

2 _ _.(

o /o _ ,_ _'h 20

-'_-B - 0 u= 8 1 2 16 20 0 .O U= .OB .1 2 .t6 .20 . 2u = .2B O.1 .2 .3 ._ . 5 .6 .7

_x , d eg CD at .

(b) Sla tI.

Figure 15. - Concluded o


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Leading-edgeUndeflected

Simpledeflection ,6LE-"30Slat

Variable chord,6LE- 20

001-

I I I I I I I I I

0 .2 .4 .6 .8 0 4 8 12 I(5

CL o, deg o

Figure16. - InfluenceOf Leading-EdgeConfigurationOn EffectiveDihedral.


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1. Report No. 2. Government Acces s ionNo . 3. ReciPient 's Ca ta log No.NASACR-172531

4. Title and Subtitle 5 . Re port Date

EFFECTSOF LEADING-EDGEDEVICESONTHE LOW-SPEED FP hP ,,_Pv lqg,_AERODYNAMICHARACTERISTICSF A HIGHLY-SWEPT 6. Pe-_o rming _ rgan_ at ionCx)deARROW-WING

7. Author( s ) 8. Perfo ;m' _n'gO;gan _za; ionReport No.

Samuel J. Scott, Oran W. Nicks and P. K. Imbrie10. Wo rk Unit No.

9, PerformingO rganization Name and Address

TEKWORLDompanyDrawer 9005, Briarfield Station 11 .Con trac tr Gran tNo .Hampton, VA 23670 P.O. L-69215B

13 . Typ e of Repo rt and P e riod Covered12. Spo nsoring Agency Name and Addr e s s

Contractor ReportNational Aeronautics and Space Administration 14 . Spo nsoringA ge ncy CodeWashington, DC 20546 505-43-43-01

15. Suppl ementa ry N ote s

Langley Technical Monitors: Samuel M. Dollyhigh and Domenic J. Maglieri

16. Abst ra ct

An inve stigati on was conduc ted in the Tex as A&M Unive rsity 7-by 10-foo t Low-Sp eed Wind Tunne l to prov ide a d irec t com paris on o f the e ffec t o f seve ral le ad ing-ed ge dev ice s on the ae rod ynamic perfo rma nce o f a high ly-swept wing con figura tion.The tests were conducted over an angle-of-attack range of -6 to 16, for a Machnumber o_ 0.21 and a Reynolds number (based on the mean aerodynamic chord) of4.1 x 10U.

Analysis of the data indicates that for the configuration with undeflectedleading edges, vortex separation first occurs on the outboard wing panel forangles of attack of approximately 2, and wing apex vorticies become apparent for

> 4 . However, the occurence of the leading_edge vortex flow may be postponedwit-h leading-edge devices. Of the devices considered, the most promising were asimple leading-edge deflection of 30, and a leading-edge slat system. Thetrailing-edge flap effectiveness was found to be essentially the same for theconfiguration employing either of these more promising leading-edge devices.

Analysis of the lateral-directional data showed that for all of the conceptsconsidered, deflecting leading edge downward in an attempt to postpone leading-edge vortex flows, has the favorable effect of reducing the effective dihedral.

'_7. Key Words ( Su gg es ted by Author(s)) 18 . Distribution Statement

Leading-Edge Devices UNCLASSIFIED- UNLIMITEDSupersonic TransportsLow Speed Aerodynamics STARCATEGORY2 - AERODYNAMICS

19 . Se cu rity Cla=if. (of this report) 20. _=curity Cl as $if.(of this page) 21 . No. of Pages 22 . Dice

UNCLASSFI ED UNCLASSFI ED 66 A04

N-30s Fo rsa lebytheNat ionalechnicaln for mationer vice ,pr ingfield.irg inia2 161


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