analysis of new signalization mastarm structures · assembly loads and capacity check 2 arm...
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Prepared for:FLORIDA DEPARTMENT OF TRANSPORTATION
DISTRICT 5
STRUCTURES REPORTANALYSIS OF NEW SIGNALIZATION MASTARM STRUCTURES
Prepared by:
13940 S.W. 136th STREETSUITE 200
MIAMI, FL 33186Certificate of Authorization 2294
STATE ROAD 492
Metric Engineering, Inc.Metric Engineering, Inc.
I hereby certify that this structures report has been properly prepared by me, or under my responsible charge, in accordance with procedures adopted by the Florida Department of Transportation.
The official record of this package has been electronically signed and sealed using a Digital Signature as required by 61G15-23.004, F.A.C. Printed Copies of this document are not considered signed and sealed and the signature must be verified on any electronic copies.
Prepared By: Peter J. Medico, P.E. Date: 08/31/2018FL License No. 42654Firm Name: Metric Engineering, Inc.Firm Address: 13940 SW 136 Street, Suite 200City, State, Zip: Miami, FL 33186Cert of Authorization: 2294Page(s): 62 (Sections 1 thru 3)
FPID NO. 443669-1-58-01MARION COUNTY
TABLE OF CONTENTS (Project No. 443669-1-58-01
SECTION DESCRIPTION SHEET Nos.
1 Design of Mast Arm No. 1.
a) Mast Arm Analysis with FDOT Excel Template………………………………………………..1 thru 2
b) Geotechnical Parameters for Drilled Shaft Sizing ………………………………………………………1
c) Mast Arm Foundation Design with Mathcad Template, Sand Model……………….1 thru 93
d) Mast Arm Foundation Design with Mathcad Template, Clay Model…………..……1 thru 93
2 Design of Mast Arm No. 2.
a) Mast Arm Analysis with FDOT Excel Template………………………………………………..1 thru 2
b) Geotechnical Parameters for Drilled Shaft Sizing ………………………………..……………………1
c) Mast Arm Foundation Design with Mathcad Template, Sand Model………………….1 thru 93
d) Mast Arm Foundation Design with Mathcad Template, Clay Model………………….1 thru 93
3 Design of Mast Arm No. 3
a) Mast Arm Analysis with FDOT Excel Template………………………………………………..1 thru 3
b) Geotechnical Parameters for Drilled Shaft Sizing ………………………………………………………1
c) Mast Arm Foundation Design with Mathcad Template, Sand Model……………….1 thru 93
d) Mast Arm Foundation Design with Mathcad Template, Clay Model……………….1 thru 93
Appendix
Tabulated Results for Drilled Shaft Lengths
Geotechnical Report
Signal Plans
Structure No. 1 SR- 492
Signal\Sign #10
Signal\Sign #9
Signal\Sign #8
Signal\Sign #7
Signal\Sign #6
Signal\Sign #5
Signal\Sign #4
Signal\Sign #3
Signal\Sign #2
Signal\Sign #1
Dist from Pole (ft.) 31 43 18 11 49 37 26
1 1 1 5 5 5 5 3 2 2
Sign Width (in.) 24 24 12 30 24 96Sign Height (in.) 36 36 18 36 30 24Area (SF) 0.0 0.0 0.0 1.5 7.5 5.0 16.0 12.3 9.8 9.8Mwl. (kip*ft) 0 0 0 3 22 6 12 40 24 17
60 Regular Heavy DutyRegular Heavy Duty 62 68
15 16 64 710.3750 0.3750
300 340 Note: red sign is video detector201 210
Assumptions:
Resistance (Mr= Mn) (kip*ft)Total Moment (Mextreme)
10124
1.1*Sign/Signal Mdl (kip*ft) Sign/Signal Mwl (kip*ft)
Wall Thickness (in)
Arm 1 Loads1.1*Arm Mdl (kip*ft) One Arm Assembly
A60/S-P4/S-DS/14/4.5
Mast Arm Assembly Information
Arm Mwl (kip*ft)
Arm 1 Length (ft)Design Standard Index 17743
Dia. at Arm Base (in)
Arm 1 Length, Signal/Sign Location and Size
Mast Arm Assembly Designation
Back Plates?
Signal Orientation
-5
5
-505101520253035404550556065707580
Arm Signal/Sign 10 Signal/Sign 9 Signal/Sign 8 Signal/Sign 7 Signal/Sign 6
Signal/Sign 5 Signal/Sign 4 Signal/Sign 3 Signal/Sign 2 Signal/Sign 1 Pole
Vertical
Horizontal
YesNo
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
Arm 1 Length
Wind Speed130 mph 150 mph
None
3 Head
4 Head
5 Head
Sign
Luminaire?
No
Yes
170 mph
(ft.) 31 43 18 11 49 37 26
H
5 He
4 H
5 H
4 H
5 H
4 H
5 H
4 H
5 H
4 H
5 H
4 H
5 H
4 H
5 H
He
He
4 H
5 H
Sign Width (in.) 24 24 12 30 24 96Sign Height (in.) 36 36 18 36 30 24Area (SF) 0.0 0.0 0.0 1.5 7.5 5.0 16.0 12.3 9.8 9.8Mwl. (kip*ft) 0 0 0 3 22 6 12 40 24 17
60 Regular Heavy DutyRegular Heavy Duty 62 68
15 16 64 710.3750 0.3750
Note: red sign is video detector300 340
Tube WindPressure(psf)
44.1Fy(ksi)
50
Sign/Sig.Wind
Pressure(psf)
67.0
wall thk(in)
base dia(in)
S(in3)
Z(in3)
Mdl
(kip*ft)Mwl 130 mph
(kip*ft)Mr= Mn
(kip*ft)wall thk(in)
base dia(in)
S(in3)
Z(in3)
Mdl
(kip*ft)Mwl 130mph
(kip*ft)Mr= Mn(kip*ft)
DSIndex #
ID Length Diameter Mn TnMu+
Pu*LshaftTu
CheckMom. &Min Dia.
CheckTorsion
CheckMu+
Pu*LshaftTu
CheckMom. &Min Dia.
CheckTorsion
Check
30 0.25 11 23 29 10 10 107 0.25 12 27 34 11 11 125 1 DS/20/5 20 5 1800 589 430.0 Okay Okay Okay 0.0 0 0 040 0.25 13 32 40 20 20 145 0.25 14 37 47 22 22 166 2 DS/18/5 18 5 1312 477 409.8 Okay Okay Okay 0.0 0 0 050 0.3125 14 46 58 36 33 215 0.3125 15 53 67 40 37 244 3 DS/16/5 16 5 922 377 389.6 Okay Okay Okay 0.0 0 0 060 0.375 15 63 79 56 48 300 0.375 16 72 91 62 53 340 4 DS/16/4.5 16 4.5 829 305 389.6 Okay Okay Okay 0.0 0 0 070 0.375 17 81 103 85 71 380 0.375 18 91 115 100 77 422 5 DS/14/5 14 5 617 289 369.4 Okay Okay Okay 0.0 0 0 078 0.375 18 91 115 110 90 422 0.375 20 113 143 130 106 512 6 DS/14/4.5 14 4.5 556 234 369.4 Okay Okay Okay 0.0 0 0 0
7 DS/12/4.5 12 4.5 350 172 349.2 Okay NoGood NoGood 0.0 0 0 08 DS/12/4 12 4 311 136 349.2 NoGood NoGood NoGood 0.0 0 0 0
Signal/Sign 10
Signal/Sign 9
Signal/Sign 8
Signal/Sign 7
Signal/Sign 6
Signal/Sign 5
Signal/Sign 4
Signal/Sign 3
Signal/Sign 2
Signal/Sign 1 Total
1 Arm DSIndex #
2 Arm DSIndex #
Arm 1Shear
Arm 1Moment
Arm 2Shear
Arm 2Moment
Sign/SigMwl
(kip*ft)0.0 0.0 0.0 3.1 21.6 6.0 11.8 40.3 24.2 17.0 124.0 4.5 7 0 dl att N/A 9.8 N/A 0.0
Sign/Sig1.1*Mdl(kip*ft)
0.0 0.0 0.0 0.2 1.4 0.4 0.8 3.5 2.0 1.4 9.8 6 0 dl arm N/A 61.6 N/A 0.0
Arm 1Mwl
(kip*ft)63.9 70.6
Reg Arm /HD Arm
6 0 wl pole 2.6 52.9 0.0 0.0
Arm 11.1*Mdl(kip*ft)
61.6 68.2Reg Arm /HD Arm
wl att 4.1 91.0 0.0 0.0
201.0 210.1 wl arm 3.3 72.8 0.0 0.0One Arm Two Arms Tor wl att N/A 124.0 N/A 0.071.4 Tor wl arm N/A 63.9 N/A 0.0
Signal/Sign 10
Signal/Sign 9
Signal/Sign 8
Signal/Sign 7
Signal/Sign 6
Signal/Sign 5
Signal/Sign 4
Signal/Sign 3
Signal/Sign 2
Signal/Sign 1 Total 216.7
Sign/SigMwl
(kip*ft)0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 228.1 0.0
Sign/Sig1.1*Mdl(kip*ft)
0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 187.9 0.0Arm 1Length
60Arm 2Length
0
Arm 2Mwl
(kip*ft)0.0 0.0 10.1 0.0 Pole ID P4
Arm 21.1*Mdl(kip*ft)
0.0 0.0Shaft2 ArmFactor
1.1used forOT &Torsion
0.0 0.0
A60 /S P4 /S DSP4/S DS/14/4.5
DS
Note: Poles are designed to have a smaller CFI than Arms
Drilled Shaft
Pole ID
A60/S P4/S DS/14/4.5Arm 1 Arm 2
Design Arm Designation Pole Designation Drilled ShaftUse Regular Arm
Torsion
Forces at Top of DS
ArmWithout Attachments: Dead Load Moment, Wind Load Moment and Moment Capacity at Base Connection
Total ArmLength (ft)
Regular
60 00.98
0.000.000.63
0.68Max Design CFI %
Est. Regular Arm CFIEst. HD Arm CFI
Arm Length(s)
Assembly ID
Required Drilled Shaft Index Number Required (see Table for size)
Load Case
Drilled Shaft Index req'd for Overturning including Min.Diamter
Arm 2 Attachments: Extreme Event Dead Load Moment, Wind Load Moment at Base Connection
Extreme Event Arm Moment (kip*ft)
2 Arm Assembly
Shear
Moment Total
Drilled Shaft Index req'd for Torsion
Drilled Shaft Controlling Load Case
Moment dl
Moment wl
A60/S
Heavy Duty
Min ShaftDiameter
Arm 1 Attachments: Extreme Event Dead Load Moment, Wind Load Moment at Base Connection
0.0187.9
Index 17743 Drilled Shaft Capacities 1 Arm Assembly Loads And Capacity Check 2 Arm Assembly Loads and Capacity Check
assume a 37.5' polewl with lum
Pole Base Shears & Moments
A60/S P4/S DS/14/4.5
Use Regular Arm1 Arm AssemblyDesign Arm Designation Pole Designation Drilled Shaft
Ensuresanchorbolts fitinsiderebarcage
N/A
125
166
244
340
422
512
107145
215
300
380
422
210201
0
100
200
300
400
500
600
25 35 45 55 65 75
Arm
Mom
ent
Arm Lengths (ft)
Arm Loads And ResistancesHD Arm 1 Resistance Reg Arm 1 Resistance HD Arm 1 Load Reg. Arm 1 Load
GEOTECHNICAL PARAMETERS for DRILLED SHAFT SIZING
Definitions:
= phi = soil friction angle [degrees]
= gamma = soil unit weight [pounds per cubic foot]
N = number of blows it takes to drive a standard sampler (1.42” ID & 2” OD) with 140 pound hammer dropped from 30-inches
C = soil cohesion shear strength [pounds per square foot]
Structure #1
0’ to 4’ ……….. = 29º = 43 PSF N =0 C = 0 PSF
4’ to 15’……….. = 0º = 62. PSF N =15 C= 1800 PSF
Pro-rate geotechnical parameters as follow:
average = (4/15) x 29º + (15-4)/15 x 0º = 7.73 º
average = (4/15) 43 PSF + (15-4)/15 x 63 PSF = 57.67 PSF
N average = (4/15) x 0 BPF + (15-4)/15 x 15 BPF = 11 blows per foot
C average = (4/11) 0 PSF + (11-4)/11 x 1800 PSF = 1145 PSF
Note that 15 is used in the denominator for the calculation of average phi, gamma and “N” because the resulting shaft length is 15’ in the last iteration of the computations for the sand model. Note that 11 is used in the denominator for “C” because the resulting shaft length is 11’ in the last iteration of the computation for the clay model.
STRUCTURE NO. 1 SAND MODEL
The new custom file will be a copy of the last file called fromthe program. A ".dat" extension will be added to the file name.Custom File Name (optional)
Add file to file list
Select Data File (required) All data files are in the same directory as the MastArm.xmcd fi
ReferenceThis program works in conjunction with Mastarm Design Standards 17743 and 17745.
References: AASHTO LRFD Specifications for Signs, Luminaires and Traffic Signals, 1st Edition (LRFDLTS).FDOT Structures Manual Vol. 3 (SM V3).
For more information see Reference.xmcd and Changes.xmcd.
Use Control+F9 torecalculate the worksheet,once to write out data, twiceto read in data
mph SM V3 3.8.2
use X to zero out datause 0 to keep current values " Yes" or " No"
use X to zero out datause 0 to keep current values
feet, 40 ft. max. for 1 piece arms
inches, measured flat to flat (FG)
feet, splice distance, for 2 piece arms,length of piece closest to pole,use X to zero out (FE)
set = for NO SPLICE
inches, this value is used for one piece arms (FD)
inches, for 2 piece arms, wall thickness of piece closest to the pole,
use X to zero out (FH)
*Note: for two piece arms (2nd length value greater than 0*ft), the first ArmLength value is entered as the actual length minus a 2 fosplice length. The 2 foot length is added to ArmLength0 at the end of the file. See drawing in reference file for more details.
Note: To model a damping device the weight is approximately the same as a 3 section signal (58 pounds) and the effective areafor wind loading is 2.1 square feet or less than half that of a 3 section signal at around 4.8 square feet
0 = user defined1 = custom design
Custom Design splice length
initial estimate of the tip diameter of the arm extension
base diameter of the arm rounded to the nearest inch
minimum and AASHTO splice length
tip diameter of arm extension
length of arm extension
User Defined splice length
Splice Length Check LTS 5.14.9
(min TipDiameter = 4.7 in. for 7 gage and 7 in. for 3 gage, see reference file)
gust factor LTS 3.8
SM V3 3.8
(min. 16 ft.)
constants that vary with exposure condition(values shown are for Exposure C):
height factor
segments n=1..50 segment 1 segment 2 segment 3 segment 4 segment5 .. segment 50
sections n=0..50 0 1 2 3 4 5 .. 49 50
(coeff drag)
Internally illuminated sign weightsvary from 5-9psf.
(coeff drag)
1. Section Properties (assume a 12 sided section) LTS Appendix Table B.1-1
inside bend radius of arm tube wall plate:
inside bend radius of arm tube wall plate:
effective width determination for use in classification of steel sectionsfor local buckling [LTS-1, Eq. C5.7.2-1]:
shape factor, Kp =Z/S:
[LTS-1, Table B.1-1] Elastic section modulus:
plastic section modulus:
ratio - inside-corner radius to wall thickness:
[see LTS-1 Eq. B.2-1]
stress concentration factor for multi-sided shapes: torsional constant:
[LTS-1, Eq. B.2-1]
2. Bare Arm DL Moment and Shear (divide arm into twenty segments, twenty one sections)
3. Bare Arm WL Moment and Shear (assume a min. ratio of break radius to tube radius of 0.25)
(Divide arm into 20 segments and use the average diameter to calculate the wind loading)
(velocity conversion factor) LTS Table 3.8.3-3
LTS Table 3.8.7-1
[LTS-1, 5.5.3.2]
flexure (bending): shear: torsion: axial compression:
tension, netsection fracture:
tension, grosssection yielding:
[LTS-1, 5.8]
no. of sides providedfor multi-sided pole:
steel modulus ofelasticity:
nominal bending strength for multi-sided tubes shall not exceed nominal bending strength for round tubes of equivalent diam
[LTS-1, 5.8.2]
flexure (bending): factored flexural resistance:
[LTS-1, 5.8]
[LTS-1, 5.10]
Note: HMLTs generally only experience pure axial comp., not pure axial tension; therefore, LTS-1, 5.9 is intentionally omitte
pole (column) totalunbraced length:
radius of gyration(per section):
steel modulus ofelasticity:effective length factor: gross section area:
[LTS-1, C5.10.2.1]
Euler stress:
critical buckling stress, used in determination ofnominal compressive strength:
buckling stress, used in determinationof for with : element effective wid
[LTS-1, Eq. 5.10.2.3-
effective pole tube wallmid-thickness radius: effective area:
local buckling adjustment factor:
section classification: [LTS-1, Tables 5.7.2-1 & Table 5.8.2-1]
torsional buckling: [LTS-1, 5.10.2.5]
Because torsional column buckling is not a common problem with sign andluminaire and signal support members, strength equations are not includedhere. If torsional buckling is of concern, design equations of AISC 14thEdition should be applied.
recalculate based on the refined value for :
critical buckling stress:
nominal compressive strength:
axial compression:
factored compressive resistance:
[LTS-1, Eq. 5.10.1-1]
[LTS-1, 5.11]
distance from max.to zero shear force:
outside distance fromflat side to flat side:
shear area:
:tip
:base
nominal shear stress capacity:
[LTS-1, 5.11.2.1.1 & 5.11.2.1.2]
nominal direct shear strength [LTS-1, 5.11.2]:
nominal torsion stress capacity: torsional constant: nominal torsional strength [LTS-1, 5.11.3]:
[LTS-1, 5.11.3.1.1 & 5.11.3.1.2]
shear: factored direct shear resistance:
[LTS-1, Eq. 5.11.1-1]
torsion: factored torsional shear resistance:
[LTS-1, Eq. 5.11.1-2]
factored flexural resistance:
factored compressive resistance:
factored direct shear resistance:
factored torsional shear resistance:
[LTS-1, 5.12.1]
moment capacity ratio: shear capacity ratio: torsion capacity ratio:
combined force interaction equation:
degree of polynomial tofit
number of data points
polynomialcoefficients
polynomial function
note: origin is the base of the arm
now integrate the curvature function twice to get deflections. Note: assuming pole connection to the foundation is rigid, theconstants of integration are zero for both slope and deflection
evaluates to
use X to zero out datause 0 to keep current values "yes" or "no"
use X to zero outuse 0 to keep current values
feet, 40 ft. max. for 1 piece arms, use X to zero out set = for NO ARM2
inches, measured flat to flat, use X to zero out (SG)
feet, splice distance, for 2 piece arms,length of piece closest to pole,use X to zero out (SE)
set = for NO SPLICE
inches, use X to zero out (SD)
inches, for 2 piece arms, wall thickness of piece closest to the pole,
use X to zero out (SH)
See Design Standards 17743 and 17745 for input values.
set = for NO LUMINAIRE
feet, use X to zero out (Standard LA = 40 feet)
feet, use X to zero out (Standard LB = 10 feet)
inches, use X to zero out (Standard LC = 3 inches)
inches, use X to zero out (Standard LD = 0.125 inches)
rise/run, use X to zero out (Standard LE = 0.5)
feet, use X to zero out (Standard LF = 8 feet)
inches, use X to zero out (Standard LG = 0.5 inches)
inches, use X to zero out (Standard LH = 0.75 inches)
feet (UA) Common wall thicknesses:0.1793 in.0.2391 in.0.25 in.0.313 in.0.375 in.0.5 in.
feet (UB)
inches, measured flat to flat (UD)
inches (UE)
inches, clear distance between connection plate and upright
inches, use X to zero out
Design Criteria: CFI (Combined Force Interation) must be less than 1
(shape factor)
(measured from face of upright to Arm BasePlate, same value is used in the ConnectionFile, a suggested minimum value for two armuprights is 5 1/2 inches to allow forfabrication and erection)
Angle between arms, a 360 degrees (this variable is ignored for single arm structures)
(Mast Arm Loads + Luminaire Loads)For analysis purposes, place the arm with the greater DL Moment as Arm1 on the X axis, and then place Arm2 on an angle a up to360 degrees. When including a Luminaire, add forces to Arm1 (conservative).
arm 1 forces
(Mast Arm only)
(Mast Arm only)
(from Luminaire only) (from Luminaire only
arm 2 forces
Axial Loadon pole
Arm deadand windloads onpole
Total PoleMoments
Wind Load Case 1wind on arm 1 only, wind direction equals 90 or 270 degrees. Note b 0 for one arm uprights
Wind Load Case 2 - calculate the torsion and shear for two arm uprights. Set wind Direction from the X Direction, b androtate the wind in increments of 5 degrees up to 360 degrees.
Wind Direction for Maximum Torsion on Upright
Wind Direction for Maximum Shear on Upright
summary of load case 2 torsion and shears in the x and z directions
Divide pole from the centerline of both arms to base into 10 segments and check each section for capacity
section properties (assume a 12 sided section)
LTS Appendix Table B.1-1
inside bend radius of tube wall plate:
inside bend radius of tube wall plate:
effective width determination for use in classification of steel sectionsfor local buckling [LTS-1, Eq. C5.7.2-1]:
shape factor, Kp =Z/S:
[LTS-1, Table B.1-1] Elastic section modulus:
plastic section modulus:
ratio - inside-corner radius to wall thickness:
[see LTS-1 Eq. B.2-1]
stress concentration factor for multi-sided shapes: torsional constant:
[LTS-1, Eq. B.2-1]
weight per segment
Height Coefficient (Kz) LTS Eqn C 3.8.4-1
height factor
Wind Load and Moments and Shears (assume a min. ratio of break radius to tube radius of 0.25)
(Divide arm into ten segments and use the average diameter to calculate the wind loading)
LTS Table 3.8.3-3
LTS Table 3.8.6-1
for one arm poles, the controlling load case is wind acting perpendicular to the arm, thereforeuse 20% of the Basic Load as the transverse loading component for this loading case. LTS 3.9.3
wind direction for maximum torsion wind direction for maximum overturning
[LTS-1, 5.5.3.2]
flexure (bending): shear: torsion: axial compression:
tension, netsection fracture:
tension, grosssection yielding:
[LTS-1, 5.8]
no. of sides providedfor multi-sided pole:
steel modulus ofelasticity:
nominal bending strength for multi-sided tubes shall not exceed nominal bending strength for round tubes of equivalent diam
[LTS-1, 5.8.2]
flexure (bending): factored flexural resistance:
[LTS-1, 5.8]
[LTS-1, 5.10]
Note: HMLTs generally only experience pure axial comp., not pure axial tension; therefore, LTS-1, 5.9 is intentionally omitte
radius of gyration(per section):
steel modulus ofelasticity:effective length factor: gross section area:
[LTS-1, C5.10.2.1]
Euler stress:
critical buckling stress, used in determination ofnominal compressive strength:
buckling stress, used in determinationof for with : element effective wid
[LTS-1, Eq. 5.10.2.3-
effective pole tube wallmid-thickness radius: effective area:
local buckling adjustment factor:
section classification: [LTS-1, Tables 5.7.2-1 & Table 5.8.2-1]
torsional buckling: [LTS-1, 5.10.2.5]
Because torsional column buckling is not a common problem with sign andluminaire and signal support members, strength equations are not includedhere. If torsional buckling is of concern, design equations of AISC 14thEdition should be applied.
recalculate based on the refined value for :
critical buckling stress:
nominal compressive strength:
axial compression:
factored compressive resistance:
[LTS-1, Eq. 5.10.1-1]
[LTS-1, 5.11]
distance from max.to zero shear force:
shear area:
nominal shear stress capacity:
[LTS-1, 5.11.2.1.1 & 5.11.2.1.2]
nominal direct shear strength [LTS-1, 5.11.2]:
nominal torsion stress capacity: torsional constant: nominal torsional strength [LTS-1, 5.11.3]:
[LTS-1, 5.11.3.1.1 & 5.11.3.1.2]
shear: factored direct shear resistance:
[LTS-1, Eq. 5.11.1-1]
torsion: factored torsional shear resistance:
[LTS-1, Eq. 5.11.1-2]
factored flexural resistance:
factored compressive resistance:
factored direct shear resistance:
factored torsional shear resistance:
[LTS-1, 4.8.1]
pole (column)unbraced length:
pole moment of inertiaat base:
pole moment of inertiaat tip:slenderness factor:
[LTS-1, C4.8.1]
check validity for use of LTS-1 Eq. 4.8.1-1:
[LTS-1, 4.8.1]
factored vertical concentratedload at pole tip:
factored weight of pole:load factors Extreme I:
equivalent axial load for a non-prismaticcantilever with a concentrated load at the tip:
Euler buckling load based upon moment ofinertia at pole bottom:
moment magnification factor for second-order effects:
[LTS-1, Eq. 4.8.1-1]
[LTS-1, 5.12.1]
moment magnification factor, calculatedaccording to AASHTO Section 4.8.1:
axial capacity ratio: moment capacity ratio: shear capacity ratio: torsion capacity ratio:
combined force interaction equation:
to clarify the stresses distributions and load cases for two arm uprights, graph CSR if minimum values for one arm shearand one arm torsion are not used
(for 16 sided pole, conservative)
From the curvature results (M/EI) at each section, curve fit a fourth degree polynomial, then integrate twice to get deflections.To get a function for curvature (M/EI), set the y-axis as curvature and the x-axis as distance along the pole starting atthe base. So the constants of integration are zero, and are calculated with section zero being at the base.
degree of polynomialto fit:
number of data points: polynomial coefficients:
polynomial function:
now integrate the curvature function twice to get deflections. Note: assuming pole connection to the foundation is rigid, the constantsof integration are zero for both slope and deflection
evaluates to:
lateral deflection atpole tip:
deflection as a percent of total pole height: lateral deflectionat pole tip:
[LTS-1, 10.4.2.1]
graph the calculated deflected shape:
inches, for two arm Mast Arms both connection plateheights must be equal (HT)
inches (FL)
inches, use X to zero out (SL)
inches (FP)
inches, use X to zero out (SP)
inches (FK)
inches, use X to zero out (SK)
inches (FJ)
inches, use X to zero out (SJ)
Trial Plate Thicknesses and Bolt Diameter
Design Criteria:performance ratio of bolt), (performance ratio of arm base plate),
& CS (combined stress ratio of vertical plate).
(for the base plate)
From Mast Arm Design
Note: Gap is the distance between the uprightand the Arm Base Plate. (5.5 inches is asuggested minimum for two arm poles)
From Upright Design(at arm connection)
(FO)
(SO)
Total Factored Moment and Shear
AISC LRFD, Vol 1, 6-A4 Specs, 2nd Ed.
Control dimensions
rounded up to the next 1/4 inch dimension
Minimum Mast Arm base plate height
Mast Arm base plate height, rounded up to next 1 inch dimension if necessary
Mast Arm base plate width
Mast Arm base plate width round up to next 1 inch dimension
(FJ)
(SJ)
Bolt spacing
(FS)
(SS)
Calculate Capacities of Connection Elements Based on the AISC LRFD Code, 2nd Edition
(Research Report 1126-4F by the Bureau of Engineering Research at the Univ. of Texas at Austin)(Design of bolts and plates based on "Design Guide for Steel to Concrete Connections by Cook, Doerr &Klingner)
Calculate Capacities of Connection Elements Based on the AISC LRFD Code, 13th Edition
Compute Shear Capacity of Back Truss Bolts (A325) [AISC J3]
Gross Bolt Area used forshear
Bending plane under full dead and wind load
Calculate the bolt moment arm
See Reference file for variable definitions
Shear perBolt
Bolt Shear Stress
Bolt Tensile Stress
AASHTO LTS minimum base plate thickness:
[LTS-1, Table 5.6.3-1] [SM 5.6.3-1]
See Reference file for formula derivations
(if PR <= 1.0 ok)
See Reference file for formula derivations
Round up to next quarter inch dimension.
(FR)
(SR)
round up to next1/8 inch dim.
NOTE: Old fillet welds, not used.
(Design welds of the socket joint to carry 100% of the design load using an E70 electrode.).
Weld Properties
Total Stress on Weld
Max. Bottom WeldSize
(FM)
(SM)
Bottom Weld Stress
AISC Table J2.5
Top Weld Stress
Top Weld Size
Round up tonext 1/16 inch
(FQ)
(SQ)
(Design welds to resist dead load moment , wind load moment, and dead load shear using an E70 electrode)
Weld Properties
Plate/Upright Weld size
AISC Table J2.5
min weld size
AISC Table J2.4
(FN)
(SN)
min weld size
AISC Table J2.4
min weld size
AISC p. 8-119
(FT)
(ST)
Trial Plate Thickness
Controlling Slenderness Parameter
Plastic Moment
Limiting Buckling Moment
Flexural Slenderness Parameters
AISC Table A-F1.1
For < <= Nominal Flex. Strength
AISC Eqn A-F1-3
For <Nominal Flex. Strength
AISC Eqn F1-14
Required Flexural Strength
Column Slenderness Parameter
AISC Eqn E2-4
Nominal Critical Stress
AISC Eqns E2-2 & E2-3
Nominal Compressive Strength
AISC Eqn E2-1
Required Compressive Strength
Combined Stress RatioFlexure and Tension members
AISC Eqns H1-1a & H1-1b (if CSR<1, then ok)
(if PR<1, then ok)
set variables equal to zero if there is no second arm
use 6 bolts minimum
inches (BC)
maximum torsion (Mx & Mz not used)maximum overturning (My not used) maximum CSR
load cases for maximum torsion (T), overturning (OT), and Combined Force Interation (CFI)
Design per AISC J3
Design plate thickness based on yield line theory
minimum base plate thickness
LTS 5.14.3SM V3 5.14.3
Round up to next1/8 inch dim.
final Diameter.tip.poleadjusted for t.baseplate.pole.
NOTE: Old fillet welds, not used.
(Design welds of the socket joint to carry 100% of the design load using an E70 electrode.).
AISC LRFD, Vol 1, 6-A4 Specs, 2nd Ed.
AISC Table J2.5
(BD)
(BE)
0 - clay 1 - sand
degrees, soil friction angle (sand)
psf, soil shear strength (clay)
pcf, soil density (typical design value = 45-50 pcf)
vertical distance between top offoundation and groundline
Number of blows per foot.If N< 5, contact the district geotech Engineer SM V3 13.6
(not used)
LRFD = AASHTO LRFD Bridge Design Specifications
SM V3 = FDOT Structures Manual Volume 3
SDG = FDOT Structures Design Guidelines
Spec = FDOT Standard Specifications
ACI = ACI 318 Structural Concrete Building Code
UF Report = FDOT/University of Florida Report BD545 RPWO #54
(From Arm1 Design)
(from Base Plate Design)
(from Upright Design)
round shaft diameter up to the nearest half foot dimension to accommodate available coring equipment
SM V3 13.6 vertical distance between top offoundation and groundline
short free-head pile in cohesionless soil using Broms method
Guess value
(round up to next foot)
short free-head pile in cohesive soil using Modified Broms method for L < 3b (see reference file forderivation)
Guess value
(round up to next foot)
short free-head pile in cohesive soil using Regular Broms method for L > 3b
(round up to next foot)
(If , use Modified Broms method)
NOTE: and are based upon CONCRETE and soilinteraction. This torsion methodology is not to be used withpermanent casing.
SM V3 13.6
Number of blows per foot. If N< 5, contact the district geotech Engineer
load transfer ratio
coefficient of friction between concrete shaft and soil
short free-head pile in cohesionless soil
Guess value
(round up to next foot)
short free-head pile in cohesive soil
Guess value
(round up to next foot)
short free-head pile in cohesionless soil using Broms method
short free-head pile in cohesive soil using Modified Broms method for L < 3b (see reference file forderivation)
Guess value
short free-head pile in cohesive soil using Regular Broms method for L > 3b
(If , use Modified Broms method)
(this is a Service moment)
Sand Model controls
reinforcing yield strength
concrete strength Spec 346-3
cover SDG Table 1.4.2-1
longitudinal bar area
longitudinal bar diameter
stirrup area SM V3 13.6.2
stirrup diameter
stirrup spacing, depth = 0 ft-2 ft SM V3 13.6.2
stirrup spacing, depth = 2 ft-depth.stir
stirrup spacing, depth > depth.stir
stirrup spacing, depth > depth.stirA
stirrup depth, see s.v2 and s.v3 above
irrup depth, see s.v3 and s.v4 above
shaft diameter
LRFD 5.7.4.2
number of longitudinal bars
SDG 3.6.10
Shear Load Factor
Torsion Load Factor
Shear Resistance Factor LRFD 5.5.4.2.1
Torsion Resistance Factor LRFD 5.5.4.2.1
Area and perimeter of concrete cross-section
Diameter, perimeter and area enclosed by the centerline of the outermost closed transverse torsion reinforcement
LRFD C5.8.2.1
Effective shear depth
LRFD C5.8.2.1
Check Shear Strength
LRFD Eqn 5.8.3.3-3LRFD 5.8.3.4.1
ACI 11.3.3
LRFD Eqn 5.8.3.3-4
Check Torsion Strength
LRFD Eqn 5.8.3.6.2-1
LRFD 5.8.3.4.1
LRFD Eqn 5.8.2.1-4
LRFD Eqn 5.8.2.1-3
Check Maximum Spacing Transverse Reinforcement
LRFD Eqn 5.8.2.9-1
LRFD Eqn 5.8.2.7-1
LRFD Eqn 5.8.2.7-2
Check Longitudinal Reinforcement for Combined Shear and Torsion LRFD Eqn 5.8.3.6.3-1
LRFD 5.8.3.4.1
Use a maximum of three rebarper anchor bolt (conservative)
2015 AASHTO Development Length of Deformed Bars in Tension 5.11.2.1
= the smaller of the distance from center of bar or wire being developed to the nearest concretesurface and one half the center-to-center spacing of the bars or wires being developed
. assume no transverse bars:
LRFD Eqn 5.11.2.1.3-1
tension development length LRFD Eqn 5.11.2.1.1-2
Note: minimum embedment was in old AASHTO LTS, 2nd Ed. 1985 and 3rd Ed. 1994 in Section 3 - 1.3.4. It was removedin the 4th Ed., but is still a good rule of thumb.
References:ACI 318-05 Appendix D.FDOT/University of Florida Report BD545 RPWO #54,Anchor Embedment Requirements for Signal/Sign Structures, July 2007.
number of anchor bolts
anchor bolt diameter
anchor bolt circle diameter
anchor bolt embedment
shaft diameter
adjusted cover
UF Report Eqn 3-2
load bearing length of anchor for shear
ACI D.6.2.2
shear break-out strength (single anchor)
UF Report Eqn 2-11
UF Report Fig 3-7
UF Report Fig 3-7
projected concrete failure area (single anchor)
ACI Eqn D-23
projected concrete failure area (group)
ACI D.6.2.1
eccentric load modifier ACI D.6.2.5
edge effect modifier ACI D.6.2.6
cracked section modifier ACI D.6.2.7 (stirrup spacing <= 4")
member thickness modifier ACI D.6.2.8
strength reduction factor ACI D.4.4.c.i ( shear breakout, condition A)
concrete breakout strength - shear
ACI Eqn D-22 Shear force | to edge
ACI D.6.2.1.c Shear force || to edge
concrete breakout strength - torsion
maximum torsion (Mx & Mz not used)maximum overturning (My not used) maximum CSR
0 - clay1 - sand
Use the member cross section adjacent to the weld toe to compute the nominal stress range. LTS 11.9
SM V3 11.6
Arm and Pole Welds
A325 Connection Bolts
Anchor Bolts
zero out initial header row for signal/sign information
(use MC10x33.6 channel for connection)
Compare Mast Arm deflection of each arm to a proposed camber
(for Two Arm Structures only)
(if Clearance equals 0, then Connection Plates intersect and redesign is required.
STRUCTURE NO. 1 CLAY MODEL
FDOT Mast Arm Analysis ProgramThe new custom file will be a copy of the last file called fromthe program. A ".dat" extension will be added to the file name.Custom File Name (optional)
Refresh File ListAdd file to file list
A60DH-A50DH-P4DL-DS165A60DH-A60D-P5DL-DS165A60DH-A60DH-P5DL-DS165A60S-P4SL-DS145A60SH-P4SL-DS145A70D-A30D-P5DL-DS165A70D-A30DH-P5DL-DS165
Select Data File (required) All data files are in the same directory as the MastArm.xmcd fi
Path "C:\Users\Peter Medico\Documents\Projects\Structural E
DataFile "A60S-P4SL-DS145.dat"
ReferenceThis program works in conjunction with Mastarm Design Standards 17743 and 17745.
References: AASHTO LRFD Specifications for Signs, Luminaires and Traffic Signals, 1st Edition (LRFDLTS).FDOT Structures Manual Vol. 3 (SM V3).
For more information see Reference.xmcd and Changes.xmcd.
Reference:C:\Users\Peter Medico\Documents\Projects\Structural Engineering Projects\SR-492 at NE 30th Mast Arm Design Update\M5\Mast
Read In Data
General Information DataFile "A60S-P4SL-DS145.dat"
Current Values New ValuesSubject "A60/S-P4/S/L-DS5.0/16/4.5"
ProjectNo "Design Standard"
PoleLocation "Index 17743"
Date "09/28/2016"Use Control+F9 torecalculate the worksheet,once to write out data, twiceto read in data
DesignedBy "FDOT"
CheckedBy "FDOT"
Wind Speed DataFile "A60S-P4SL-DS145.dat"
Current Value New Value
WindSpeed 170 mph mph SM V3 3.8.2
Kd 0.85
VService 90mph
Arm 1 Analysis DataFile "A60S-P4SL-DS145.dat" WindSpeed 170 mph
11/2/2018 S-1 Clay Model.xmcd 1
Arm 1 Loads
SignalDataarm1
"SignalNumber"
1
2
3
4
5
6
7
8
9
10
"DistanceToSignal(ft)"
28
43
58
0
0
0
0
0
0
0
"NumberOfSignalHeads"
3
3
3
3
0
0
0
0
0
0
"BackPlate"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
use X to zero out datause 0 to keep current values " Yes" or " No"
"SignalNumber" "DistToSignal(ft)" "#SignalHeads" "BackPlate"1 26 3 "yes"2 37 3 "yes"3 49 4 "yes"4 0 "x" "yes"5 0 0 "yes"6 0 0 "yes"7 0 0 "yes"8 0 0 "yes"9 0 0 "yes"
10 0 0 "yes"
New Values
SignDataarm1
"PanelNumber"
1
2
3
4
5
"DistanceToPanelCentroid(ft)"
35
0
0
0
0
"PanelArea(sf)"
15
0
0
0
0
"Panel#" "DistToCentroid(ft)" "PanelArea(sf)"1 11 162 18 53 31 1.54 43 7.55 0 0
New Values use X to zero out datause 0 to keep current values
Arm 1 Loads
11/2/2018 S-1 Clay Model.xmcd 2
Arm 1 Properties
Current Values New Values
Ltotal.arm1 60 ft feet, 40 ft. max. for 1 piece arms
Diameterbase.arm1 14 in inches, measured flat to flat (FG)
feet, splice distance, for 2 piece arms,length of piece closest to pole,use X to zero out (FE)
Distsplice.from.base.arm1 27.5 ft set Distsplice.from.base.arm1 = 0ft for NO SPLICE
inches, this value is used for one piece arms (FD)twall.arm1
0.25
0.375
ininches, for 2 piece arms, wall thickness of piece closest to the pole,use X to zero out (FH)
Arm 1 Properties
Analyze Arm 1
Switch values, set values for DataOutz 0 1
fSwitchData orig new unit( ) if new "x"=( ) new "X"=( ) 0 unit if new 0= orig new unit( )[ ]
ZeroSignSignalData old new( )
valuen1 n2 0 newn1 n2 "x"=if
valuen1 n2 0 newn1 n2 "X"=if
valuen1 n2 oldn1 n2 otherwise
n2 0 cols new( ) 1for
n1 0 rows new( ) 1for
value
out 1
out out 1 out 0
Ltotal.arm1 fSwitchData Ltotal.arm1 newLtotal.arm1 ft dataoutLtotal.arm1
ftdataout 60
out out 1 out 1
Diameterbase.arm1 fSwitchData Diameterbase.arm1 newDiameterbase.arm1 in dataoutDiameterbase.arm1
indataout 14
out out 1 out 2
Distsplice.from.base.arm1 fSwitchData Distsplice.from.base.arm1 newDistsplice.from.base.arm1 ft
dataoutDistsplice.from.base.arm1
ftdataout 27.5
out out 1 out 3
twall.arm1zfSwitchData twall.arm1z
newtwall.arm1zin dataout
twall.arm1
indataout
0.25
0.375
twall.arm11if Distsplice.from.base.arm1 0 ft= 0 in twall.arm11
11/2/2018 S-1 Clay Model.xmcd 3
out out 1 out 4
WindSpeed fSwitchData WindSpeed newWindSpeed mph( ) dataoutWindSpeed
mphdataout 150
out out 1 out 5
i 1 rows newSignalDataarm1 1 j 0 cols newSignalDataarm1 1
SignalDataarm1i jif SignalDataarm1i j
newSignalDataarm1i jnewSignalDataarm1i j
0 newSignalDataarm1i j
SignalDataarm1
SignalDataarm1 ZeroSignSignalData SignalDataarm1 newSignalDataarm1dataout SignalDataarm1
dataout
"SignalNumber"
1
2
3
4
5
6
7
8
9
10
"DistanceToSignal(ft)"
26
37
49
0
0
0
0
0
0
0
"NumberOfSignalHeads"
3
3
4
0
0
0
0
0
0
0
"BackPlate"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
out out 1 out 6
i 1 rows newSignDataarm1 1 j 0 cols newSignDataarm1 1
SignDataarm1i jif SignDataarm1i j
newSignDataarm1i jnewSignDataarm1i j
0 newSignDataarm1i j
SignDataarm1i j SignDataarm1 ZeroSignSignalData SignDataarm1 newSignDataarm1
dataout SignDataarm1
dataout
"PanelNumber"
1
2
3
4
5
"DistanceToPanelCentroid(ft)"
11
18
31
43
0
"PanelArea(sf)"
16
5
1.5
7.5
0
Sort Signal and Sign Data
#Signalsarm1 match 0 submatrix SignalDataarm1 1 10 0 2 0 0 0 0
i1 1 #Signalsarm1
Xsignal.arm1i1SignalDataarm1i1 1
ft
11/2/2018 S-1 Clay Model.xmcd 4
Sectionssignal.arm1i1SignalDataarm1i1 2
Backplatesignal.arm1i1if SignalDataarm1i1 3
"yes"= 1 0
i1
12
3
Xsignal.arm1i1
2637
49
ft
Sectionssignal.arm1i1
33
4
Backplatesignal.arm1i1
11
1
#Panelsarm1 match 0 submatrix SignDataarm1 1 5 0 2 0 0 0 0
temp#Panelsarm1 #Panelsarm1
#Panelsarm1 if #Panelsarm1 0= 1 #Panelsarm1
j1 1 #Panelsarm1
Xpanel.arm1j1SignDataarm1j1 1
ft
Areapanel.arm1j1SignDataarm1j1 2
ft2
Xpanel.arm11if temp#Panelsarm1 0= 0.1 ft Xpanel.arm11
Areapanel.arm11if temp#Panelsarm1 0= 0.1 ft2 Areapanel.arm11
j1
12
3
4
Xpanel.arm1j1
1118
31
43
ft
Areapanel.arm1j1
165
1.5
7.5
ft2
*Note: for two piece arms (2nd length value greater than 0*ft), the first ArmLength value is entered as the actual length minus a 2 fosplice length. The 2 foot length is added to ArmLength0 at the end of the file. See drawing in reference file for more details.
Note: To model a damping device the weight is approximately the same as a 3 section signal (58 pounds) and the effective areafor wind loading is 2.1 square feet or less than half that of a 3 section signal at around 4.8 square feet
11/2/2018 S-1 Clay Model.xmcd 5
Drawsignals count 1
startSectionssignal.arm1k
20.5
ft
sd 0
zcount 0 Xsignal.arm1 k
zcount 1 start j ft
count count 1
j 1 Sectionssignal.arm1kfor
k 1 #Signalsarm1for
z
Areapanel.arm10if #Panelsarm1 0 0 ft2 Areapanel.arm10
Xpanel.arm1.nounitsXpanel.arm1
ftApanel.arm1.nounits
Areapanel.arm1
ft2
Drawsigns count 0
pd 0
pd0 0 Xpanel.arm1.nounits k
Apanel.arm1.nounitsk
2
pd0 1
Apanel.arm1.nounitsk
2
pd1 0 Xpanel.arm1.nounits k
Apanel.arm1.nounitsk
2
pd1 1
Apanel.arm1.nounitsk
2
pd2 0 Xpanel.arm1.nounits k
Apanel.arm1.nounitsk
2
pd2 1
Apanel.arm1.nounitsk
2
pd3 0 Xpanel.arm1.nounits k
Apanel.arm1.nounitsk
2
pd3 1
Apanel.arm1.nounitsk
2
pd4 0 pd0 0
pd4 1 pd0 1
arrayk pd
k 1 if #Panelsarm1 1 1 #Panelsarm1for
array
Drawsigns
0
{5,2}
{5,2}
{5,2}
{5,2}
Placeholder
0
0
0
0
0
0
0
0
0
0
11/2/2018 S-1 Clay Model.xmcd 6
xsignals Drawsignals0 ysignals Drawsignals
1
testvalj1 if #Panelsarm1 0 j1 1 1
Drawsign1 if max testval( ) 1 Drawsigns1Placeholder
Drawsign2 if max testval( ) 2 Drawsigns2Placeholder
Drawsign3 if max testval( ) 3 Drawsigns3Placeholder
Drawsign4 if max testval( ) 4 Drawsigns4Placeholder
50 40 30 20 10
5
5
Location of Signs and Signals
Taper 0.14inft
SpliceType 0 0 = user defined1 = custom design
Lsplice.user 24 in
Custom Design splice length
Diametertemp.arm1 Diameterbase.arm1
Diameterbase.arm11Diameterbase.arm1 Diameterbase.arm11
14 in
initial estimate of the tip diameter of the arm extension
11/2/2018 S-1 Clay Model.xmcd 7
estDiatip.arm11Diameterbase.arm11
Distsplice.from.base.arm1 Taper estDiatip.arm1110.15 in
base diameter of the arm rounded to the nearest inch
estDiabase.arm10estDiatip.arm11
2 ft Taper 2 twall.arm10estDiabase.arm10
10.93 in
Diameterbase.arm10round
estDiabase.arm10
in0
in Diameterbase.arm1011 in
Diameterbase.arm11if Diameterbase.arm10
Diameterbase.arm11= Distsplice.from.base.arm1 0 ft= 0 ft Diameterbase.arm11
Diameterbase.arm1114 in
minimum and AASHTO splice length
Lsplice.min 24 in
Lsplice.aashto 1.5 Diameterbase.arm102 twall.arm10
Lsplice.aashto 15.75 in
Lsplice.aashto Ceil Lsplice.aashto in Lsplice.aashto 16 in
Lsplice.addtl if Ltotal.arm1 50 ft 3 in 0 in Lsplice.addtl 3 in
Lsplice.arm1 if Lsplice.min Lsplice.aashto Lsplice.min Lsplice.aashto Lsplice.addtl Lsplice.arm1 27 in
Lsplice.arm1 if Diameterbase.arm110 ft= 0 ft Lsplice.arm1 Lsplice.arm1 27 in
tip diameter of arm extension
estDiatip.arm11Diameterbase.arm10
2 twall.arm10Lsplice.arm1 Taper estDiatip.arm11
10.185 in
length of arm extension
Larm11
Diameterbase.arm11estDiatip.arm11
TaperLarm11
27.25 ft
Larm11if Diameterbase.arm11
0 ft= 0 ft Ceil Larm11.01 in 6 in Larm11
27.5 ft
Lsplice.provided Larm11
Diameterbase.arm11Diameterbase.arm10
2 twall.arm10
Taper
Lsplice.provided 30 in
Lsplice.provided if Diameterbase.arm110 ft= 0 ft Lsplice.provided Lsplice.provided 30 in
Diametertip.arm11if Diameterbase.arm10
0 ft= 0 ft Diameterbase.arm11Larm11
tbaseplate.arm0Taper
Diametertip.arm1110.185 in
11/2/2018 S-1 Clay Model.xmcd 8
Larm10Ltotal.arm1 Larm11
Lsplice.provided Larm1035 ft
Larm10Ceil Larm10
.01 in 3 in Larm1035 ft
Lsplice.provided.arm1 Larm10Larm11
Ltotal.arm1 Lsplice.provided.arm1 30 in
Lsplice.provided.arm1 if Distsplice.from.base.arm1 0 ft= 0 in Lsplice.provided.arm1 Lsplice.provided.arm1 30 in
Diametertip.arm10Diameterbase.arm10
Larm10tbaseplate.arm0
Taper Diametertip.arm106.135 in
CheckLtotal Larm10if Diameterbase.arm11
0 ft= 0 ftDiameterbase.arm11
Diameterbase.arm102 twall.arm10
Taper
CheckLtotal 60 ft
User Defined splice length
Larm1.user1Distsplice.from.base.arm1 Larm1.user1
27.5 ft
Larm1.user0Ltotal.arm1 Distsplice.from.base.arm1 Lsplice.user Larm1.user0
34.5 ft
Diameterbase.arm1.user1Diametertemp.arm1 Diameterbase.arm1.user1
14 in
Diametertip.arm1.user1Diameterbase.arm1.user1
Larm1.user1tbaseplate.arm0
Taper Diametertip.arm1.user110.185 in
Diameterbase.arm1.user0Diametertip.arm1.user1
Lsplice.user Taper 2 twall.arm10Diameterbase.arm1.user0
10.965 in
Diametertip.arm1.user0Diameterbase.arm1.user0
Larm1.user0Taper Diametertip.arm1.user0
6.135 in
Larm1.user1if Distsplice.from.base.arm1 0 ft= 0 ft Larm1.user1
Larm1.user127.5 ft
Larm1.user0if Distsplice.from.base.arm1 0 ft= Ltotal.arm1 Larm1.user0
Larm1.user034.5 ft
Diameterbase.arm1.user1if Distsplice.from.base.arm1 0 ft= 0 ft Diameterbase.arm1.user1
Diameterbase.arm1.user114 in
Diametertip.arm1.user1if Distsplice.from.base.arm1 0 ft= 0 ft Diametertip.arm1.user1
Diametertip.arm1.user110.185 in
Diameterbase.arm1.user0if Distsplice.from.base.arm1 0 ft= Diametertemp.arm1 Diameterbase.arm1.user0
Diameterbase.arm1.user010.965 in
Diametertip.arm1.user0if Distsplice.from.base.arm1 0 ft= Diameterbase.arm1.user0
Larm1.user0tbaseplate.arm0
Taper Diametertip.arm1.user0
Diametertip.arm1.user06.135 in
Lsplice.provided if SpliceType 0= Lsplice.user Lsplice.provided Lsplice.provided 24 in
11/2/2018 S-1 Clay Model.xmcd 9
Lsplice.provided.arm1 if SpliceType 0= Lsplice.user Lsplice.provided.arm1 Lsplice.provided.arm1 24 in
Larm11if SpliceType 0= Larm1.user1
Larm11Larm11
27.5 ft
Larm10if SpliceType 0= Larm1.user0
Larm10Larm10
34.5 ft
Diameterbase.arm11if SpliceType 0= Diameterbase.arm1.user1
Diameterbase.arm11Diameterbase.arm11
14 in
Diametertip.arm11if SpliceType 0= Diametertip.arm1.user1
Diametertip.arm11Diametertip.arm11
10.185 in
Diameterbase.arm10if SpliceType 0= Diameterbase.arm1.user0
Diameterbase.arm10Diameterbase.arm10
10.965 in
Diametertip.arm10if SpliceType 0= Diametertip.arm1.user0
Diametertip.arm10Diametertip.arm10
6.135 in
Splice Length Check LTS 5.14.9
Lsplice.provided.arm1 24 in Lsplice.aashto 16 in
CheckSpliceLengtharm1 if Lsplice.provided.arm1 Lsplice.aashto "OK" "No Good" CheckSpliceLengtharm1 "OK"
Ltotal.arm1 60 ft Larm134.5
27.5
ft Diametertip.arm16.135
10.185
in Diameterbase.arm110.965
14
in
(min TipDiameter = 4.7 in. for 7 gage and 7 in. for 3 gage, see reference file) Diametertip.arm106.13 in
G 1.14 gust factor LTS 3.8
SM V3 3.8
Pressure 0.00256 psf( )WindSpeed
mph
2G Kd Pressure 55.8 psf
PService 0.00256 psf( )VService
mph
2
G Kd PService 20.1 psf
heightarm 24.4 ft (min. 16 ft.)
constants that vary with exposure condition(values shown are for Exposure C):
zg 900 ft 9.5
Kz.arm fKz heightarm zg height factor Kz.arm 0.94
11/2/2018 S-1 Clay Model.xmcd 10
segments n=1..50 segment 1 segment 2 segment 3 segment 4 segment5 .. segment 50
sections n=0..50 0 1 2 3 4 5 .. 49 50
Signal DL and WL Moments and Shears
Weightsignal.head 14 lbf Weightbackplate 2 lbf Weightbracket 5.3 lbf Cd.signal 1.2 (coeff drag)
Areasignal.head 1.36 ft2 Areabackplate 5.67 ft2 Areabracket 0.29 ft2 Cd.backplate 1.2
Weightsignal.section.arm1 if #Signalsarm1 0= 0 lbf( ) Weightsignal.head
Areasignal.section.arm1 if #Signalsarm1 0= 0 ft2 Cd.signal Areasignal.head
Weightbackplate.arm1 if #Signalsarm1 0= 0 lbf( ) Weightbackplate
Areabackplate.arm1i1if #Signalsarm1 0= 0 ft2 Cd.backplate Areabackplate
Areabackplate.arm1i1if Sectionssignal.arm1i1
4= Cd.backplate 6.83 ft2 Areabackplate.arm1i1
Areabackplate.arm1i1if Sectionssignal.arm1i1
5= Cd.backplate 8.00 ft2 Areabackplate.arm1i1
Weightbracket.arm1 if #Signalsarm1 0= 0 lbf( ) Weightbracket
Areabracket if #Signalsarm1 0= 0 ft2 Areabracket
Weightsignal.arm1i1Sectionssignal.arm1i1
Weightsignal.section.arm1 Weightbackplate.arm1 Backplatesignal.arm1i1if Xsignal.arm1i1
0 ft= 0
Pressuresignal.arm1i1Sectionssignal.arm1i1
Areasignal.section.arm1 Backplatesignal.arm1i1Areabackplate.arm1i1
Areabracket Pressure Kz.arm
Weightsignal.arm1
0
49.3
49.3
63.3
lbf Pressuresignal.arm1
0
626.2
626.2
784.2
lbf
PServicesignal.arm1i1Sectionssignal.arm1i1
Areasignal.section.arm1 Backplatesignal.arm1i1Areabackplate.arm1i1
Areabracket PService Kz.arm
11/2/2018 S-1 Clay Model.xmcd 11
PServicesignal.arm1
0
225.4
225.4
282.3
lbf
NumberOfSections 20 n 0 NumberOfSections
Xsection.arm1nLtotal.arm1 Ltotal.arm1
nNumberOfSections
Mdl.signal.arm1ni1
Weightsignal.arm1i1if Xsignal.arm1i1
Xsection.arm1n0 ft 0 ft Xsignal.arm1i1
Xsection.arm1n
Mwl.signal.arm1ni1
Pressuresignal.arm1i1if Xsignal.arm1i1
Xsection.arm1n0 ft 0 ft Xsignal.arm1i1
Xsection.arm1n
Vdl.signal.arm1ni1
Weightsignal.arm1i1if Xsignal.arm1i1
Xsection.arm1n0 ft 0 1
Vwl.signal.arm1ni1
Pressuresignal.arm1i1if Xsignal.arm1i1
Xsection.arm1n0 ft 0 1
MS.wl.signal.arm1ni1
PServicesignal.arm1i1if Xsignal.arm1i1
Xsection.arm1n0 ft 0 ft Xsignal.arm1i1
Xsection.arm1n
VS.wl.signal.arm1ni1
PServicesignal.arm1i1if Xsignal.arm1i1
Xsection.arm1n0 ft 0 1
Sign Panel DL and WL Moments and Shears
UnitWeightpanel 4.0lbf
ft2Internally illuminated sign weightsvary from 5-9psf.
Cd.panel 1.2 (coeff drag)
Areapanel.arm1j1if #Panelsarm1 0= 0 ft2 Areapanel.arm1j1
j1
12
Xpanel.arm1j1
11 ft
Areapanel.arm1j1
16 ft2
11/2/2018 S-1 Clay Model.xmcd 12
2
3
4
18
31
43
5
1.5
7.5Weightpanel.arm1j1Areapanel.arm1j1
UnitWeightpanel Weightpanel.arm1
0
64
20
6
30
lbf
Pressurepanel.arm1j1Areapanel.arm1j1
Pressure Cd.panel Kz.arm Pressurepanel.arm1
0
1 103
313.4
94
470.1
lbf
PServicepanel.arm1j1Areapanel.arm1j1
PService Cd.panel Kz.arm PServicepanel.arm1
0
361
112.8
33.8
169.2
lbf
Mdl.panel.arm1nj1
Weightpanel.arm1j1if Xpanel.arm1j1
Xsection.arm1n0 ft 0 ft Xpanel.arm1j1
Xsection.arm1n
Mwl.panel.arm1nj1
Pressurepanel.arm1j1if Xpanel.arm1j1
Xsection.arm1n0 ft 0 ft Xpanel.arm1j1
Xsection.arm1n
Vdl.panel.arm1nj1
Weightpanel.arm1j1if Xpanel.arm1j1
Xsection.arm1n0 ft 0 1
Vwl.panel.arm1nj1
Pressurepanel.arm1j1if Xpanel.arm1j1
Xsection.arm1n0 ft 0 1
MS.wl.panel.arm1nj1
PServicepanel.arm1j1if Xpanel.arm1j1
Xsection.arm1n0 ft 0 ft Xpanel.arm1j1
Xsection.arm1n
VS.wl.panel.arm1nj1
PServicepanel.arm1j1if Xpanel.arm1j1
Xsection.arm1n0 ft 0 1
Mast Arm Bare Steel Section Properties, Moments, and Shears
1. Section Properties (assume a 12 sided section) Sides 12 LTS Appendix Table B.1-1
Rodn
12
Diameterbase.arm11
Ltotal.arm1 NumberOfSections n( )
NumberOfSectionsTaper
if Larm10
Ltotal.arm1
NumberOfSectionsn 0 in twall.arm10
12
Diameterbase.arm10
Ltotal.arm1 NumberOfSections n( )
NumberOfSectionsTaper
otherwise
tarm1nif Xsection.arm1n
Larm110 in twall.arm11
twall.arm10
11/2/2018 S-1 Clay Model.xmcd 13
RidnRodn
tarm1nRmidn
Rodn
tarm1n
2
Aarm1n6.43 Rmidn
tarm1nIarm1n
3.29 Rmidn
3 tarm1nrgn
0.715 Rmidn
fRInsideBend t( ) 0.63 in t 0.1196 inif
1.31 in 0.1196 in t 0.1875 inif
1.75 in 0.1875 in t 0.25 inif
1.94 in 0.25 in t 0.3125 inif
2.13 in 0.3125 in t 0.375 inif
2.56 in 0.375 in t 0.4375 inif
3.0 in 0.4375 in t 0.5 inif
"N.G." otherwise
rb.arm1iifRInsideBend twall.arm1ii
rb.arm11.75
2.13
in
inside bend radius of arm tube wall plate:
rb.arm1iifRInsideBend twall.arm1ii
rb.arm11.75
2.13
in
inside bend radius of arm tube wall plate:
rbb.arm1nif Xsection.arm1n
Larm110 in rb.arm11
rb.arm10
rc.arm1n
rbb.arm1nif Xsection.arm1n
Larm110 in twall.arm11
twall.arm10 Ridn
rs.arm1n
rbb.arm1n
Rodn
effective width determination for use in classification of steel sectionsfor local buckling [LTS-1, Eq. C5.7.2-1]:
barm1nfb Rodn
Ridnrbb.arm1n
tarm1nSides
min barm1 0.965 in max barm1 2.746 in
11/2/2018 S-1 Clay Model.xmcd 14
shape factor, Kp =Z/S:
[LTS-1, Table B.1-1] Elastic section modulus:
Sarm1n3.29 Rmidn
2 tarm1nKpnfKp Sides( )
Sarm1.rdn3.14 Rmidn
2 tarm1n
plastic section modulus:
Zarm1nfZ Kpn
Sarm1n
Zarm1.rdnfZ 1.27 Sarm1.rdn
ratio - inside-corner radius to wall thickness:
n'arm1nfn' rbb.arm1n
tarm1n[see LTS-1 Eq. B.2-1]
stress concentration factor for multi-sided shapes: torsional constant:
kt.arm1nfkt tarm1n
Rmidnn'arm1n
[LTS-1, Eq. B.2-1] Ct.arm1nfCt Rmidn
tarm1nkt.arm1n
Sides
60 40 20 0
20
10
10
20
Outside Wall FaceInside Wall FaceOutside Wall FaceInside Wall Face
Wall Thickness and Splice Transition
Length in feet
Dia
met
er in
inch
es
Larm1 1
ft
2. Bare Arm DL Moment and Shear (divide arm into twenty segments, twenty one sections)
Lsplice.provided 24 in11/2/2018 S-1 Clay Model.xmcd 15
SpliceIndexn if Larm10
Ltotal.arm1
NumberOfSectionsn
NumberOfSections n
min SpliceIndex( ) 12
Weightsplice if min SpliceIndex( ) NumberOfSections=( ) 0 lbf Aarm1min SpliceIndex( )Lsplice.provided 490
lbf
ft3
Weightsplice 84.224 lbf
n 1 NumberOfSections
Weightsegmentn
Aarm1n 1Aarm1n
2
Ltotal.arm1
NumberOfSections
490lbf
ft3
max Weightsegment 165.1 lbf
Weightsegmentmin SpliceIndex( )Weightsegmentmin SpliceIndex( )
Weightsplice max Weightsegment 211.1 lbf
Weightsegment 2144 lbf
XsegmentnXsection.arm1n 1
Ltotal.arm1
NumberOfSections
2 Aarm1nAarm1n 1
3 Aarm1nAarm1n 1
Mdl.tube.arm1n1
n
k
WeightsegmentkXsegmentk
Xsection.arm1n Vdl.tube.arm1n1
n
k
Weightsegmentk
3. Bare Arm WL Moment and Shear (assume a min. ratio of break radius to tube radius of 0.25)
(Divide arm into 20 segments and use the average diameter to calculate the wind loading)
n 1 NumberOfSections DiametersegmentnRodn 1
Rodndn Diametersegmentn
V WindSpeed
Cv 0.8 (velocity conversion factor) LTS Table 3.8.3-3
LTS Table 3.8.7-1Cd.segment.arm1n
fCd CvWindSpeed
mph
dn
ftrc.arm1n
rs.arm1nSides
max Cd.segment.arm1 0.79
Cd.S.segment.arm1nfCd 1.0
VService
mph
dn
ftrc.arm1n
rs.arm1nSides
max Cd.S.segment.arm1 0.93
Psegmentn
Larm1NumberOfSections
DiametersegmentnCd.segment.arm1n
Pressure Kz.arm
Mwl.tube.arm1n1
n
k
PsegmentkXsegmentk
Xsection.arm1n Vwl.tube.arm1n1
n
k
Psegmentk
11/2/2018 S-1 Clay Model.xmcd 16
PS.segmentn
Larm1NumberOfSections
DiametersegmentnCd.S.segment.arm1n
PService Kz.arm
MS.wl.tube.arm1n1
n
k
PS.segmentkXsegmentk
Xsection.arm1n VS.wl.tube.arm1n1
n
k
PS.segmentk
Total DL and WL Moments and Shears
DC.Ext1 1.1 W.Ext1 1.0
n 0 NumberOfSections
Mdl.arm1n DC.Ext1 Mdl.signal.arm1nMdl.panel.arm1n
Mdl.tube.arm1nVdl.arm1n DC.Ext1 Vdl.signal.arm1n
Vdl.panel.arm
Mwl.arm1nMwl.signal.arm1n
Mwl.panel.arm1nMwl.tube.arm1n
Vwl.arm1nVwl.signal.arm1n
Vwl.panel.arm1nVwl.
MS.wl.arm1nMS.wl.signal.arm1n
MS.wl.panel.arm1nMS.wl.tube.arm1n
VS.wl.arm1nVS.wl.signal.arm1n
VS.wl.panel.arm1n
base1 last Mdl.arm1 base1 20 Mwl.arm120171.191 kip ft MS.wl.arm120
64.2
0 5 10 15 200
50
100
150
Moments due to Dead and Wind Loads
Mdl.arm1n
kip ft
Mwl.arm1n
kip ft
n
11/2/2018 S-1 Clay Model.xmcd 17
0 5 10 15 200
2
4
6
Shears due to Dead and Wind Loads
Vdl.arm1n
kip
Vwl.arm1n
kip
n
0 5 10 15 200
20
40
60
Moments due to Dead and Wind Loads
Mdl.arm1n
kip ft
MS.wl.arm1n
kip ft
n
11/2/2018 S-1 Clay Model.xmcd 18
0 5 10 15 200
1
2
Shears due to Dead and Wind Loads
Vdl.arm1n
kip
VS.wl.arm1n
kip
n
Total Arm Bending Force on the Section
Mu.arm1nMdl.arm1n
2 Mwl.arm1n
2
Mu.arm120183.1 kip ft
Total Arm Shear force on the Section
Vu.arm1nVdl.arm1n
2 Vwl.arm1n
2 Vu.arm1206.58 kip
Factored Resistance - Extreme Event I
Resistance Factors [LTS-1, 5.5.3.2]
flexure (bending): shear: torsion: axial compression:f 0.9 v 0.9 t 0.95 c 0.9
tension, netsection fracture:
tension, grosssection yielding:
u 0.75 y 0.9
Bending Strength [LTS-1, 5.8]
no. of sides providedfor multi-sided pole:
steel modulus ofelasticity:
11/2/2018 S-1 Clay Model.xmcd 19
Fy 50 ksi E 29000 ksi
nominal bending strength for multi-sided tubes shall not exceed nominal bending strength for round tubes of equivalent diam
Mn.arm1nfMn Zarm1n
Zarm1.rdnFy 2 Ridn
barm1ntarm1n
E Sides
[LTS-1, 5.8.2] min Mn.arm1 35.5 kip ft max Mn.arm1 289.2 k
flexure (bending): factored flexural resistance:
f 0.9 Mr.arm1n f Mn.arm1n[LTS-1, 5.8] min Mr.arm1 32 kip ft max Mr.arm1 260.3 k
Compressive Strength [LTS-1, 5.10]
Note: HMLTs generally only experience pure axial comp., not pure axial tension; therefore, LTS-1, 5.9 is intentionally omitte
pole (column) totalunbraced length:
radius of gyration(per section):
steel modulus ofelasticity:effective length factor: gross section area:
K 2.1 L Ltotal.arm1 rn rgnE 29000 ksi Agn
Aarm1n[LTS-1, C5.10.2.1]
L 60 ft
Euler stress:
Fe.arm1 fFe E K Ltotal.arm1 r20
critical buckling stress, used in determination ofnominal compressive strength:
buckling stress, used in determinationof be for AEFF with Q 1.0= : element effective wid
Fcr.arm1 fFcr 1.0 Fy Fe.arm1 K Ltotal.arm1 r20 E farm1 Fcr.arm1 be.arm1nfbe E farm
[LTS-1, Eq. 5.10.2.3-
effective pole tube wallmid-thickness radius: effective area:
Rb.EFF.arm1n
be.arm1ntarm1n
2AEFF.arm1n
fA Rb.EFF.arm1ntarm1n
Sides
local buckling adjustment factor:
Qarm1nfQ barm1n
barm1ntarm1n
E Fy AEFF.arm1nAgn
Sides
max Qarm1 1 min Qarm1 1
11/2/2018 S-1 Clay Model.xmcd 20
section classification: [LTS-1, Tables 5.7.2-1 & Table 5.8.2-1]
Classn fClass barm1nbarm1n
tarm1nE Fy Sides
torsional buckling: [LTS-1, 5.10.2.5]
Because torsional column buckling is not a common problem with sign andluminaire and signal support members, strength equations are not includedhere. If torsional buckling is of concern, design equations of AISC 14thEdition should be applied.
recalculate Fcr based on the refined value for Q :
critical buckling stress:
Fcr.arm1nfFcr Qarm1n
Fy Fe.arm1 K Ltotal.arm1 r20 E
min Fcr.arm1 2.605 ksi
max Fcr.arm1 2.605 ksinominal compressive strength:
Pnc.arm1nAgn
Fcr.arm1nmin Pnc.arm1 12.249 kip
max Pnc.arm1 42.79 kipClass
0
01
2
3
4
5
6
7
8
9
10
11
12
13
14
15
"Compact""Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
...
axial compression:
c 0.9
factored compressive resistance:
Prc.arm1n c Pnc.arm1n[LTS-1, Eq. 5.10.1-1] min Prc.arm1 11 kip
max Prc.arm1 38.5 kip
11/2/2018 S-1 Clay Model.xmcd 21
Shear and Torsion Strength [LTS-1, 5.11]
distance from max.to zero shear force:
outside distance fromflat side to flat side:
shear area:
Lv.arm1 Ltotal.arm1 d1 6.310 in :tip Av.arm1n
Agn
2Lv.arm1 60 ft max d( ) 13.79 in :base
nominal shear stress capacity:
Fnv.arm1nfFnv E Lv.arm1 2 Ridn
tarm1nFy Sides
[LTS-1, 5.11.2.1.1 & 5.11.2.1.2]
nominal direct shear strength [LTS-1, 5.11.2]:
Vn.arm1nAv.arm1n
Fnv.arm1nmin Vn.arm1 70.529 kip
max Vn.arm1 246.4 kip
nominal torsion stress capacity: torsional constant: nominal torsional strength [LTS-1, 5.11.3]:
Fnt.arm1nfFnt E Lv.arm1 2 Ridn
tarm1nFy Sides min Ct.arm1 13.753 in3 Tn.arm1n
Ct.arm1nFnt.arm1n
[LTS-1, 5.11.3.1.1 & 5.11.3.1.2]max Ct.arm1 108.754 in3 min Tn.arm1 34.4 kip ft
max Tn.arm1 271.9 kip ft
shear: factored direct shear resistance:
v 0.9 Vr.arm1n v Vn.arm1n[LTS-1, Eq. 5.11.1-1] min Vr.arm1 63.5 kip max Vr.arm1 221
torsion: factored torsional shear resistance:
t 0.95 Tr.arm1n t Tn.arm1n[LTS-1, Eq. 5.11.1-2] min Tr.arm1 32.7 kip ft max Tr.arm1 258
Factored Resistance Summaryfactored flexural resistance:
min Mr.arm1 32 kip ft max Mr.arm1 260.3 kip ft
factored compressive resistance:
min Prc.arm1 11 kip max Prc.arm1 38.5 kip
factored direct shear resistance:
min Vr.arm1 63.5 kip max Vr.arm1 221.8 kip
factored torsional shear resistance:
min Tr.arm1 32.7 kip ft max Tr.arm1 258.3 kip ft
11/2/2018 S-1 Clay Model.xmcd 22
Combined Force/Resistance Interaction - Extreme Event I
Check Combined Force Interaction < 1.00 [LTS-1, 5.12.1]
moment capacity ratio: shear capacity ratio: torsion capacity ratio:
CRMn
Mu.arm1n
Mr.arm1n
CRVn
Vu.arm1n
Vr.arm1n
2
max CRM 0.704 max CRV 8.839 10 4
combined force interaction equation:
CFIarm1nfCFIsimple 0 0 1.0 Mu.arm1n
Mr.arm1nChk5.12.1.arm1n
fCheck5.12.1 CFIarm1n
max CFIarm1 0.704 min Chk5.12.1.arm1 "OK"
0 5 10 15 200
0.16
0.32
0.48
0.64
0.8Combined Stress Ratio
CFIarm1n
n
Dead Load Deflection
11/2/2018 S-1 Clay Model.xmcd 23
Curvaturen
Mdl.arm1n
E Iarm1n
xn Xsection.arm1n n Curvaturen in
degree of polynomial tofit
k 3 number of data points Z regressxin
k
polynomialcoefficients coeffs submatrix Z 3 length Z( ) 1 0 0( ) coeffs( )T 6.87 10 5 6.64 10 8 1.4 10 11 4.72 10
polynomial function curve x( ) coeffs0 coeffs1 x coeffs2 x2 coeffs3 x3 Armn curvexn
in
note: origin is the base of the arm
60 40 20 02 10 5
0
2 10 5
4 10 5
6 10 5
8 10 5Calculated Curvature vs. Curve Fit
n
Armn
xn
ft
now integrate the curvature function twice to get deflections. Note: assuming pole connection to the foundation is rigid, theconstants of integration are zero for both slope and deflection
xxcoeffs0 coeffs1 x coeffs2 x2 coeffs3 x3 d d evaluates to 12
coeffs0 x2 16
coeffs1 x3 112
coeffs2 x4 120
coeff
curve x( )12
coeffs0 x2 16
coeffs1 x3 112
coeffs2 x4 120
coeffs3 x5
arm1ncurve
xn
in
in max arm1 12.90 in
60 40 20 0
20
10
0Arm Deflection
arm1 n
in
xn
ft
11/2/2018 S-1 Clay Model.xmcd 24
Mdl.arm1base164.956 kip ft
Vdl.arm1base12.669 kip
Mwl.arm1base1171.191 kip ft
Vwl.arm1base16.015 kip
Larm134.5
27.5
fttwall.arm1
0.25
0.375
in
Diametertip.arm16.135
10.185
inDiameterbase.arm1
10.965
14
in
Analyze Arm 1
Summary - Arm 1 Geometry and Loading
50 40 30 20 10
5
5
Location of Signs and Signals
WindSpeed 150 mph Ltotal.arm1 60 ft
Diametertip.arm16.13
10.18
in Diameterbase.arm110.965
14
in Larm134.5
27.5
ft twall.arm10.25
0.375
in
Xsignal.arm1i1
26 ft
Sectionssignal.arm1i1
3
Xpanel.arm1j1
11 ft
Areapanel.arm1j1
16 211/2/2018 S-1 Clay Model.xmcd 25
2637
49
ft 33
4
1118
31
43
ft 165
1.5
7.5
ft2
Arm 1 Combined Stress Ratio and Deflectionmax CFIarm1 0.704 max arm1 12.9 in 2 deg Larm1 Lsplice.provided 24.29 in
Arm 2 Analysis DataFile "A60S-P4SL-DS145.dat" WindSpeed 150 mph
Arm 2 Loads
SignalDataarm2
"SignalNumber"
1
2
3
4
5
6
7
8
9
10
"DistanceToSignal(ft)"
0
0
0
0
0
0
0
0
0
0
"NumberOfSignalHeads"
3
3
3
3
0
0
0
0
0
0
"BackPlate"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
"yes"
use X to zero out datause 0 to keep current values "yes" or "no"
"SignalNumber" "DistToSignal(ft)" "#SignalHeads" "BackPlate"1 0 "x" "yes"2 0 "x" "yes"3 0 "x" "yes"4 0 "x" "yes"5 0 0 "yes"6 0 0 "yes"7 0 0 "yes"8 0 0 "yes"9 0 0 "yes"
10 0 0 "yes"
New Values
SignDataarm2
"PanelNumber"
1
2
3
4
5
"DistanceToPanelCentroid(ft)"
0
0
0
0
0
"PanelArea(sf)"
15
0
0
0
0
11/2/2018 S-1 Clay Model.xmcd 26
"Panel#" "DistToCentroid(ft)" "PanelArea(sf)"1 0 "x"2 0 03 0 04 0 05 0 0
New Values use X to zero outuse 0 to keep current values
Arm 2 Loads
Arm 2 Properties
Current Values New Values
Ltotal.arm2 0 ft feet, 40 ft. max. for 1 piece arms, use X to zero out set Ltotal.arm2 = 0ft for NO ARM2
Diameterbase.arm2 18 in inches, measured flat to flat, use X to zero out (SG)
feet, splice distance, for 2 piece arms,length of piece closest to pole,use X to zero out (SE)
Distsplice.from.base.arm2 40 ft set Distsplice.from.base.arm2 = 0ft for NO SPLICE
inches, use X to zero out (SD)twall.arm2
0.25
0
ininches, for 2 piece arms, wall thickness of piece closest to the pole,use X to zero out (SH)
Arm 2 Properties
Analyze Arm 2
0.3 0.2 0.1
5
5
Location of Signs and Signals
Summary - Arm 2 Geometry and Loading
WindSpeed 150 mph Ltotal.arm2 0 ft
Diametertip.arm20
0
in Diameterbase.arm20
0
in Larm20
0
ft twall.arm20
0
in
Xsignal.arm2i2
00
ft
Sectionssignal.arm2i2
00
Xpanel.arm2j2
0.1 ft
Areapanel.arm2j2
0.1 ft2
11/2/2018 S-1 Clay Model.xmcd 27
0 0
Arm 2 Combined Stress Ratio and Deflection
max CFIarm2 0 max arm2 0 in 2 deg Larm2 Lsplice.provided 1.68 in
Luminaire Arm Analysis DataFile "A60S-P4SL-DS145.dat" WindSpeed 150 mph
Luminaire Properties
See Design Standards 17743 and 17745 for input values.
Current Values New Values set Yluminaire = 0ft for NO LUMINAIRE
Yluminaire 40 ft feet, use X to zero out (Standard LA = 40 feet)
Xluminaire 10 ft feet, use X to zero out (Standard LB = 10 feet)
Diameterbase.lumarm 3 in inches, use X to zero out (Standard LC = 3 inches)
twall.lumarm 0.125 in inches, use X to zero out (Standard LD = 0.125 inches)
Slopelumarm 0.5 rise/run, use X to zero out (Standard LE = 0.5)
rlumarm 8 ft feet, use X to zero out (Standard LF = 8 feet)
dbolt.lum 0.5 in inches, use X to zero out (Standard LG = 0.5 inches)
tbaseplate.lum 0.75 in inches, use X to zero out (Standard LH = 0.75 inches)
Luminaire Properties
Analyze Luminaire
Summary - Luminaire Arm GeometryYluminaire 0 ft Xluminaire 0 ft Diameterbase.lumarm 0 in twall.lumarm 0 in
Slopelumarm 0 rlumarm 0 ft dbolt.lum 0 in tbaseplate.lum 0 in
wbase.lum inwbase.lum wchannel.lum 0 in
Luminaire Arm Ratios
CFIbase.lumarmCFIbase.lumarm CheckBoltLumBoltCheckBoltLumBolt PRbaseplate.lum 0 PRconn.plate.lum 0
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Upright Analysis DataFile "A60S-P4SL-DS145.dat" WindSpeed 150 mph
Pole Properties
Current Values New ValuesYpole 39 ft feet (UA) Common wall thicknesses:
0.1793 in.0.2391 in.0.25 in.0.313 in.0.375 in.0.5 in.
Yarm.conn 22 ft feet (UB)
Diameterbase.pole 22 in inches, measured flat to flat (UD)
twall.pole 0.375 in inches (UE)
inches, clear distance between connection plate and uprightGap
7.5
0
ininches, use X to zero out
Pole Properties
Analyze Pole
Switch values, set values for DataOut
out out 1 out 21
dataoutwbase.lum
in
wbase.lumdataoutdata
out out 1 out 22
dataoutwchannel.lum
indataout 0
out out 1 out 23
Ypole fSwitchData Ypole newYpole ft dataoutYpole
ftdataout 23
out out 1 out 24
Yarm.conn fSwitchData Yarm.conn newYarm.conn ft dataoutYarm.conn
ftdataout 20
out out 1 out 25
Diameterbase.pole fSwitchData Diameterbase.pole newDiameterbase.pole in dataoutDiameterbase.pole
indataout 22
out out 1 out 26
twall.pole fSwitchData twall.pole newtwall.pole in dataouttwall.pole
indataout 0.375
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out out 1 out 27
Gap fSwitchData3 Gap newGap in( ) dataoutGapin
dataout7.5
0
Gap1 if Ltotal.arm2 0 ft= 0 in Gap1
out out 1 out 28 dataoutYlum.conn
ftdataout 0
Design Parameters
Design Criteria: CFI (Combined Force Interation) must be less than 1
WindSpeed 150 mph Taper 0.14inft
Kp 1.26 (shape factor)
Diametertip.pole Diameterbase.pole Ypole 2.5 in Taper Diametertip.pole 18.81 in
Diameterconn.pole Diametertip.pole Taper Ypole Yarm.conn Diameterconn.pole 19.23 in
(measured from face of upright to Arm BasePlate, same value is used in the ConnectionFile, a suggested minimum value for two armuprights is 5 1/2 inches to allow forfabrication and erection)
Gap7.5
0
in i 0 1
90 deg Angle between arms, a <= 360 degrees (this variable is ignored for single arm structures)
E 29000 ksi Fy 50 ksi NumberOfSections 10 n 0 NumberOfSections
WindSpeed 150 mph Pressure 55.81lbf
ft2
Applied Loads
(Mast Arm Loads + Luminaire Loads)For analysis purposes, place the arm with the greater DL Moment as Arm1 on the X axis, and then place Arm2 on an angle a up to360 degrees. When including a Luminaire, add forces to Arm1 (conservative).
arm 1 forces
Mdl0Mdl.arm1base1
Mdl.luminaire Mdl065.0 kip ft Vdl.arm1base1
2.7 kip (Mast Arm only)
Mwl0Mwl.arm1base1
My.wl.luminaire Mwl0171.2 kip ft Vwl.arm1base1
6.0 kip (Mast Arm only)
Mx.wl.luminaire 0.0 kip ft (from Luminaire only) Vwl.luminaire 0.0 kip (from Luminaire only
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Mx.wl.tip Mx.wl.luminaire Vwl.luminaire Ypole 1.0 ft Yarm.conn Mx.wl.tip 0.0 kip ft
arm 2 forces 90 deg
Mdl1Mdl.arm2base2
Mdl10.0 kip ft
Mwl1Mwl.arm2base2
Mwl10.0 kip ft
Vdl.arm2base20 kip Vwl.arm2base2
0 kip
Vdl.arm
Vdl.arm1base1
Vdl.arm2base2
Vwl.arm
Vwl.arm1base1
Vwl.arm2base2
VS.wl.arm
VS.wl.arm1base1
VS.wl.arm2base2
MS.wl
MS.wl.arm1base1MS.y.upright
MS.wl.arm2base2
MS.x.wl.tip MS.x.upright VS.wl.lumarm Ypole 1.0 ft Yarm.conn MS.x.wl.tip 0.1 kip ft
Combined Applied Pole Loads
if Ltotal.arm2 0 ft= 0
Axial Loadon pole Axialtop Vdl.arm1base1
Vdl.arm2base2Vdl.lum Axialtop 2.7 kip
Arm deadand windloads onpole
Mdl.poletipiMdli
Vdl.armiGapi
Diameterconn.pole
2
Mdl.poletip68.8
0
kip ft
Mwl.poletipiMwli
Vwl.armiGapi
Diameterconn.pole
2
Mwl.poletip179.8
0
kip ft
Mz.poletip Mdl.poletip0sin 90 deg( ) Mdl.poletip1
Mz.poletip 68.8 kip ftTotal PoleMoments
Mx.poletip cos 90 deg( ) Mdl.poletip1Mx.poletip 0.0 kip ft
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MS.wl.poletipiMS.wli
VS.wl.armiGapi
Diameterconn.pole
2
MS.wl.poletip
67.4
2 10 3
kip
MS.z.poletip
Mdl.poletip0sin 90 deg( ) Mdl.poletip1
DC.Ext1
MS.z.poletip 62.5 kip ft
MS.x.poletip cos 90 deg( )Mdl.poletip1
DC.Ext1MS.x.poletip 0.0 kip ft
Wind Load Case 1wind on arm 1 only, wind direction equals 90 or 270 degrees. Note b = 90 for one arm uprights. i 0 2 0 5 360
WindDirection2 if Mdl10 kip ft= 90 deg if 180 deg( ) 90 deg 270 deg[ ]
WindDirection2 90 deg
Torsiononearm sin deg( ) Mwl.poletip0
TorsionS.onearm sin deg( ) MS.wl.poletip0
Vx.poletip.onearm 0 kip Vz.poletip.onearm Vwl.arm0sin deg( )
VS.x.poletip.onearm 0 kip VS.z.poletip.onearm VS.wl.arm0sin deg( )
Wind Load Case 2 - calculate the torsion and shear for two arm uprights. Set wind Direction from the X Direction, b = 0, androtate the wind in increments of 5 degrees up to 360 degrees.
Torsion sin deg( ) Mwl.poletip0sin deg( ) Mwl.poletip1
TorsionS sin deg( ) MS.wl.poletip0sin deg( ) MS.wl.poletip1
0 45 90 135 180 225 270 315 360
200
100
100
200Upright Torsion (1 & 2 arms)
Torsion
kip ft
Torsiononearm
kip ft
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0 45 90 135 180 225 270 315 360
100
50
50
100Upright Torsion (1 & 2 arms)
TorsionS
kip ft
TorsionS.onearm
kip ft
Shear sin deg( ) Vwl.arm0sin deg( ) Vwl.arm1
cos( ) 2 sin deg( ) Vwl.arm1sin( ) 2
ShearS sin deg( ) VS.wl.arm0sin deg( ) VS.wl.arm1
cos( ) 2 sin deg( ) VS.wl.arm1sin( ) 2
0 45 90 135 180 225 270 315 360
10
5
5
10Shear at Arm Connection
Shear
kip
Vz.poletip.onearm
kip
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0 45 90 135 180 225 270 315 360
10
6.25
2.5
1.25
5Shear at Arm Connection
ShearS
kip
VS.z.poletip.onearm
kip
Wind Direction for Maximum Torsion on Upright
0 5 180 Mypoletip Torsion
My.max if min Mypoletip max Mypoletip min Mypoletip max Mypoletip My.max 179.8 kip ft
FindDirection if My.max Mypoletip= 0
WindDirection0 if Mdl10 kip ft= 90 deg max FindDirection( ) deg
WindDirection0 90 deg
WindDirection0 if 180 deg( ) WindDirection0 WindDirection0 180 deg WindDirection0 270 deg
Wind Direction for Maximum Shear on Upright
0 5 360 Vpoletip Shear max Vpoletip 6.0 kip
FindDirection if max Vpoletip Vpoletip= 0
WindDirection1 if Mdl10 kip ft= 90 deg max FindDirection( ) deg
WindDirection1 90 deg
WindDirection1 if WindDirection1 360 deg= 270 deg WindDirection1 WindDirection1 90 deg
WindDirection1 if 180 deg( ) WindDirection1 WindDirection1 180 deg WindDirection1 90 deg
summary of load case 2 torsion and shears in the x and z directions
Axialtop 2.7 kip Mx.poletip 0.0 kip ft Mz.poletip 68.8 kip ft My.poletip Torsion
Vx.poletip sin deg( ) Vwl.arm1sin( ) Vz.poletip sin deg( ) Vwl.arm0
sin deg( ) Vwl.arm1cos( )
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VS.x.poletip sin deg( ) VS.wl.arm1sin( ) VS.z.poletip sin deg( ) VS.wl.arm0
sin deg( ) VS.wl.arm1cos( )
My.poletipT 0 1 2 3 4 5 6 7
0 0.0 0.0 0.0 0.0 0.0 -15.7 0.0 ...kip ft
Vx.poletipT 0 1 2 3 4 5 6 7 8 9
0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 ...kip
Vz.poletipT 0 1 2 3 4
0 0.0 0.0 0.0 0.0 ...kip
Divide pole from the centerline of both arms to base into 10 segments and check each section for capacity
NumberOfSections 10
YsectionnYarm.conn Yarm.conn
nNumberOfSections
Upright Bare Steel Section Properties, Moments and Shears
section properties (assume a 12 sided section) sides 12
LTS Appendix Table B.1-1
Rodn
Diameterbase.poleYarm.conn NumberOfSections n( )
NumberOfSectionsTaper
2
RidnRodn
twall.pole RmidnRodn
twall.pole
2
Apolen6.43 Rmidn
twall.pole Ipolen3.29 Rmidn
3 twall.pole rgn0.715 Rmidn
Rod.lum.tipDiametertip.pole
2
Ipole.lum 3.29 Rod.lum.tip3 twall.pole
inside bend radius of tube wall plate:
rb.pole fRInsideBend twall.pole
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rb.pole 2.13 in
inside bend radius of tube wall plate:
rbb.pole rb.pole
rc.polen
rb.pole twall.pole
Ridn
rs.polen
rb.pole
Rodn
effective width determination for use in classification of steel sectionsfor local buckling [LTS-1, Eq. C5.7.2-1]:
bpolenfb Rodn
Ridnrbb.pole twall.pole Sides
min bpole 4.14 in max bpole 4.89 in
shape factor, Kp =Z/S:
[LTS-1, Table B.1-1] Elastic section modulus:
Spolen3.29 Rmidn
2 twall.poleKp.pole fKp Sides( )
Spole.rdn3.14 Rmidn
2 twall.pole
plastic section modulus:
ZpolenfZ Kp.pole Spolen
Zpole.rdnfZ 1.27 Spole.rdn
ratio - inside-corner radius to wall thickness:
n'pole fn' rbb.pole twall.pole [see LTS-1 Eq. B.2-1]
stress concentration factor for multi-sided shapes: torsional constant:
kt.polenfkt twall.pole Rmidn
n'pole [LTS-1, Eq. B.2-1] Ct.polenfCt Rmidn
twall.pole kt.polenSides
weight per segment n 1 NumberOfSections
Weightsegmentn
Apolen 1Apolen
2
Yarm.conn
NumberOfSections
490lbf
ft3
j 1 NumberOfSections
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Weightsegment.top Apole0Ypole Yarm.conn 490
lbf
ft3
SegmentAxialLoadn Weightsegment.top Axialtop
1
n
j
Weightsegmentj
SegmentAxialLoad0 Weightsegment.top Axialtop
Height Coefficient (Kz) LTS Eqn C 3.8.4-1
YsegmentnYarm.conn
n( ) 2 12 NumberOfSections
Yarm.conn
height 9.5
Kz.polenfKz Ysegmentn
zg height height factormax Kz.pole 0.89
Kz.pole.top fKzYpole Yarm.conn
2zg height
Kz.pole.top 0.911
Wind Load and Moments and Shears (assume a min. ratio of break radius to tube radius of 0.25)
(Divide arm into ten segments and use the average diameter to calculate the wind loading)
n 1 NumberOfSectionsSegmentDiametertopDiametertip.pole Diameterconn.pole
2
SegmentDiametern Diameterconn.polen( ) 2 1
2 NumberOfSectionsYarm.conn Taper V WindSpeed dpolen
SegmentDiameter
Cv 0.80 LTS Table 3.8.3-3
Cd.segment.polenfCd Cv
WindSpeedmph
dpolen
ftrc.polen
rs.polenSides
LTS Table 3.8.6-1
rc.pole.toprb.pole twall.pole
SegmentDiametertop
2twall.pole
rs.pole.top2rb.pole
SegmentDiametertop
Cd.segment.pole.top fCd CvWindSpeed
mph
SegmentDiametertop
ftrc.pole.top rs.pole.top Sides
Cd.segment.pole.top 0
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Cd.S.segment.polenfCd 1.0
VService
mph
dpolen
ftrc.polen
rs.polenSides
Cd.S.segment.pole.top fCd CvVService
mph
SegmentDiametertop
ftrc.pole.top rs.pole.top Sides
Cd.S.segment.pole.top 0
SectionForcenYarm.conn
NumberOfSectionsSegmentDiametern Cd.segment.polen
Pressure Kz.polen
SectionForcetip Ypole Yarm.conn SegmentDiametertop Cd.segment.pole.top Pressure Kz.pole.top
SectionForceSnYarm.conn
NumberOfSectionsSegmentDiametern Cd.S.segment.polen
PService Kz.polen
SectionForceStip Ypole Yarm.conn SegmentDiametertop Cd.S.segment.pole.top PService Kz.pole.top
Mwl.polen0
n
p
SectionForcep YsegmentpYsectionn
SectionForcetipYpole Yarm.conn
2Ysectionn
Mx.wl.luminaire
Vwl.luminaire Ypole 1.0 ft Ysectionn
Mwl.pole0SectionForcetip
Ypole Yarm.conn
2Mx.wl.tip
MS.wl.polen0
n
p
SectionForceSp YsegmentpYsectionn
SectionForceStipYpole Yarm.conn
2Ysectionn
Mx.upright
VS.wl.lumarm Ypole 1.0 ft Ysectionn
MS.wl.pole0SectionForceStip
Ypole Yarm.conn
2MS.x.wl.tip
Vwl.polenSectionForcetip
0
n
p
SectionForcep Vwl.pole0SectionForcetip n 0 NumberOfSections
Mx.wl.pole nMwl.polen
cos deg 90 deg( ) Mz.wl.pole nMwl.polen
sin deg 90 deg( )( )
Vx.wl.pole nVwl.polen
cos deg( )( ) Vz.wl.pole nVwl.polen
sin deg( )
VS.wl.polenSectionForceStip
0
n
p
SectionForceSp VS.wl.pole0SectionForceStip
MS.x.wl.pole nMS.wl.polen
cos deg 90 deg( ) MS.z.wl.pole nMS.wl.polen
sin deg 90 deg( )( )
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VS.x.wl.pole nVS.wl.polen
cos deg( )( ) VS.z.wl.pole nVS.wl.polen
sin deg( )
for one arm poles, the controlling load case is wind acting perpendicular to the arm, thereforeuse 20% of the Basic Load as the transverse loading component for this loading case. LTS 3.9.3
Mz.wl.pole nif Mdl1
0 kip ft= 0 kip ft Mz.wl.pole n min Mz.wl.pole 0.0 kip ft
Vx.wl.pole nif Mdl1
0 kip ft= 0 kip ft Vx.wl.pole n max Vx.wl.pole 0.0 kip
MS.z.wl.pole nif Mdl1
0 kip ft= 0 kip ft MS.z.wl.pole n min MS.z.wl.pole 0.0 kip ft
VS.x.wl.pole nif Mdl1
0 kip ft= 0 kip ft VS.x.wl.pole n max VS.x.wl.pole 0.0 kip
Total Forces at a Section
My nMy.poletip
My nmax
Torsiononearm
My.poletip
Mx nMx.poletip Vz.poletip Yarm.conn Ysectionn
Mx.wl.pole n
Mz nMz.poletip Vx.poletip Yarm.conn Ysectionn
Mz.wl.pole n
MS.y nTorsionS
MS.y nmax
TorsionS.onearm
TorsionS
MS.x nMS.x.poletip VS.z.poletip Yarm.conn Ysectionn
MS.x.wl.pole n
MS.z nMS.z.poletip VS.x.poletip Yarm.conn Ysectionn
MS.z.wl.pole n
AxialForce n SegmentAxialLoadn Vx nVx.poletip Vx.wl.pole n
Vwl.luminaire
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Vz nVz.poletip Vz.wl.pole n Vz n
maxVz.poletip Vz.wl.pole n
Vz.poletip.onearm
VS.x nVS.x.poletip VS.x.wl.pole n
VS.wl.lumarm
VS.z nVS.z.poletip VS.z.wl.pole n VS.z n
maxVS.z.poletip VS.z.wl.pole n
Vz.poletip.onearm
wind direction for maximum torsion wind direction for maximum overturning
wd0WindDirection0
deg wd0 270 wd1WindDirection1
degwd1 90
0 2 4 6 8 100
50
100
150
X, Y, & Z Moments
Mzwd0 n
kip ft
Mywd0 n
kip ft
Mxwd0 n
kip ft
Mzwd1 n
kip ft
Mywd1 n
kip ft
Mxwd1 n
kip ft
n
6
Axial and Shear Forces
AxialForcewd0 n
kip
Vzwd0 n
ki11/2/2018 S-1 Clay Model.xmcd 40
0 2 4 6 8 100
2
4
kip
Vxwd0 n
kip
AxialForcewd1 n
kip
Vzwd1 n
kip
Vxwd1 n
kip
n
0 2 4 6 8 100
20
40
60
X, Y, & Z Moments
MS.zwd0 n
kip ft
MS.ywd0 n
kip ft
MS.xwd0 n
kip ft
MS.zwd1 n
kip ft
MS.ywd1 n
kip ft
MS.xwd1 n
kip ft
n
6
Axial and Shear Forces
AxialForcewd0 n
DC.Ext1 kip
VS.zwd0 n11/2/2018 S-1 Clay Model.xmcd 41
0 2 4 6 8 100
2
4
kip
VS.xwd0 n
kip
AxialForcewd1 n
DC.Ext1 kip
VS.zwd1 n
kip
VS.xwd1 n
kip
n
Total Bending Moments on the Section
Mu.pole nMx n
2 Mz n
2
max Mu.pole 152.743 kip ft
Total Shear Force on a Section
Vu.pole nVx n
2 Vz n
2 max Vu.pole 7.326 kip
Total Axial Stress on a Section
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Pu.pole nAxialForce n max Pu.pole 4.56 kip
Factored Resistance - Extreme Event I
Resistance Factors [LTS-1, 5.5.3.2]
flexure (bending): shear: torsion: axial compression:f 0.9 v 0.9 t 0.95 c 0.9
tension, netsection fracture:
tension, grosssection yielding:
u 0.75 y 0.9
Bending Strength [LTS-1, 5.8]
no. of sides providedfor multi-sided pole:
steel modulus ofelasticity:
Fy 50 ksi E 29000 ksi
nominal bending strength for multi-sided tubes shall not exceed nominal bending strength for round tubes of equivalent diam
Mn.polenfMn Zpolen
Zpole.rdnFy 2 Rodn
bpolentwall.pole E Sides [LTS-1, 5.8.2]
min Mn.pole 525.1 kip ft max Mn.pole 676.1 kip
flexure (bending): factored flexural resistance:
f 0.9 Mr.polen f Mn.polen[LTS-1, 5.8] min Mr.pole 472.6 kip ft max Mr.pole 608.5 kip
Compressive Strength [LTS-1, 5.10]
Note: HMLTs generally only experience pure axial comp., not pure axial tension; therefore, LTS-1, 5.9 is intentionally omitte
radius of gyration(per section):
steel modulus ofelasticity:effective length factor: gross section area:
K 2.1 rn rgnE 29000 ksi Agn
Apolen[LTS-1, C5.10.2.1]
Euler stress:
Fe.pole fFe E K Ypole r10
critical buckling stress, used in determination ofnominal compressive strength:
buckling stress, used in determinationof be for AEFF with Q 1.0= : element effective wid
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Fcr.pole fFcr 1.0 Fy Fe.pole K Ypole r10 E fpole Fcr.pole be.polenfbe E fpole
[LTS-1, Eq. 5.10.2.3-
effective pole tube wallmid-thickness radius: effective area:
Rb.EFF.polen
be.polentwall.pole
2AEFF.polen
fA Rb.EFF.polentwall.pole Sides
local buckling adjustment factor:
QpolenfQ bpolen
bpolentwall.pole E Fy AEFF.polen
AgnSides
max Qpole 1 min Qpole 1
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section classification: [LTS-1, Tables 5.7.2-1 & Table 5.8.2-1]
Classn fClass bpolenbpolen
twall.pole E Fy Sides
torsional buckling: [LTS-1, 5.10.2.5]
Because torsional column buckling is not a common problem with sign andluminaire and signal support members, strength equations are not includedhere. If torsional buckling is of concern, design equations of AISC 14thEdition should be applied.
recalculate Fcr based on the refined value for Q :
critical buckling stress:
Fcr.polenfFcr Qpolen
Fy Fe.pole K Ypole r10 E min Fcr.pole 33.15 ksi
max Fcr.pole 33.15 ksi
nominal compressive strength:
Pnc.polenAgn
Fcr.polenmin Pnc.pole 752.375 kip
max Pnc.pole 864.28 kipClass
0
01
2
3
4
5
6
7
8
9
10
11
12
13
14
15
"Compact""Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"Compact"
"N/A"
"N/A"
"N/A"
"N/A"
...
axial compression:
c 0.9
factored compressive resistance:
Prc.polen c Pnc.polen[LTS-1, Eq. 5.10.1-1] min Prc.pole 677.1 kip
max Prc.pole 777.9 kip
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Shear and Torsion Strength [LTS-1, 5.11]
distance from max.to zero shear force:
shear area:
Lv.pole Ypole Av.polen
Agn
2Lv.pole 23 ft
nominal shear stress capacity:
Fnv.polenfFnv E Lv.pole 2 Rodn
twall.pole Fy Sides
[LTS-1, 5.11.2.1.1 & 5.11.2.1.2]
nominal direct shear strength [LTS-1, 5.11.2]:
Vn.polenAv.polen
Fnv.polenmin Vn.pole 340.438 kip
max Vn.pole 391.075 kip
nominal torsion stress capacity: torsional constant: nominal torsional strength [LTS-1, 5.11.3]:
Fnt.polenfFnt E Lv.pole 2 Rodn
twall.pole Fy Sides min Ct.pole 204.496 in3 Tn.polenCt.polen
Fnt.polen
[LTS-1, 5.11.3.1.1 & 5.11.3.1.2]max Ct.pole 268.488 in3 min Tn.pole 511.2 kip ft
max Tn.pole 671.2 kip ft
shear: factored direct shear resistance:
v 0.9 Vr.polen v Vn.polen[LTS-1, Eq. 5.11.1-1] min Vr.pole 306.4 kip max Vr.pole 352
torsion: factored torsional shear resistance:
t 0.95 Tr.polen t Tn.polen[LTS-1, Eq. 5.11.1-2] min Tr.pole 485.7 kip ft max Tr.pole 637.
Factored Resistance Summaryfactored flexural resistance:
min Mr.pole 472.6 kip ftmax Mr.pole 608.5 kip ft
factored compressive resistance:
min Prc.pole 677.1 kip max Prc.pole 777.9 kip
factored direct shear resistance:
min Vr.pole 306.4 kip max Vr.pole 352 kip
factored torsional shear resistance:
min Tr.pole 485.7 kip ft max Tr.pole 637.7 kip ft
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Combined Force/Resistance Interaction - Extreme Event I
Moment Magnification [LTS-1, 4.8.1]
pole (column)unbraced length:
pole moment of inertiaat base:
pole moment of inertiaat tip:slenderness factor:
k 2.0 Ypole 23 ft IB Ipolelast IpoleIT Ipole0
[LTS-1, C4.8.1]IB 1559.6 in4 IT 1028.8 in4
check validity for use of LTS-1 Eq. 4.8.1-1:
ChkEq4.8.1nfCheck4.8.1 E Fy k Ypole rgn
min ChkEq4.8.1 "NG" [LTS-1, 4.8.1]
factored vertical concentratedload at pole tip:
factored weight of pole:load factors Extreme I:
DC.Ext1 1.1 PT DC.Ext1 Axialtop DP DC.Ext1 SegmentAxialLoadlast IpoleAxial
PT 2.936 kip DP 2.08 kip
equivalent axial load for a non-prismaticcantilever with a concentrated load at the tip:
Euler buckling load based upon moment ofinertia at pole bottom:
Pequivalent fPequivalent IB IT PT DP PEuler.bottom fPEuler.bottom E IB k L
Pequivalent 4.163 kip PEuler.bottom 215.267 kip
moment magnification factor for second-order effects:
B2 fB2 Pequivalent PEuler.bottom B2 1.02
[LTS-1, Eq. 4.8.1-1]
Check Combined Force Interaction < 1.00 [LTS-1, 5.12.1]
moment magnification factor, calculatedaccording to AASHTO Section 4.8.1:
B B2 B 1.02
axial capacity ratio: moment capacity ratio: shear capacity ratio: torsion capacity ratio:
CRP n
Pu.pole n
Prc.polenCRM n
Mu.pole n
Mr.polen
CRVT n
Vu.pole n
Vr.polen
My n
Tr.polen
2
CRT n
My n
Tr.polen
max CRP 5.862 10 3max CRM 0.251 max CRVT 0.152 max CRT 0.37
combined force interaction equation:
CFIpole nfCFI Pu.pole n
Prc.polenB Mu.pole n
Mr.polenVu.pole n
Vr.polenMy n
Tr.polen
11/2/2018 S-1 Clay Model.xmcd 48
max CFIpole 0.353
Chk5.12.1.pole nfCheck5.12.1 CFIpole n
ChkMin
Min min Chk5.12.1.pole n
n 1 10for
0 5 360for
MinChkMin "OK"
LoadCase n if max CFIpole CFIpole n= 1 LoadCase max LoadCase( ) LoadCase 270
CFIpoleLoadCase 00.305 CFIpoleLoadCase last Ipole
0.353 CFIpolewd0 last Ipole0.353 CFIpolewd1 last Ipole
0.353
0 2 4 6 80.28
0.296
0.312
0.328
0.344
0.36Maximum Combined Force Interaction
CFIpoleLoadCase n
n
0 5 100
0.1
0.2
0.3
Combined Force Interation
CFIpole n
n
11/2/2018 S-1 Clay Model.xmcd 49
to clarify the stresses distributions and load cases for two arm uprights, graph CSR if minimum values for one arm shearand one arm torsion are not used
My nMy.poletip Vz n
Vz.poletip Vz.wl.pole n
Vu.pole nVx n
2 Vz n
2 max Vu.pole 7.326 kip
CFIpole.TWO nfCFI Pu.pole n
Prc.polenB Mu.pole n
Mr.polenVu.pole n
Vr.polenMy n
Tr.polen
max CFIpole 0.353
0 5 100
0.1
0.2
0.3
CFI Ignoring One Arm
CFIpole.TWO n
n
Dead Load Deflection at the Arms
C 3.22 (for 16 sided pole, conservative)
TTaper
2RarmDiametertip.pole Taper Ypole Yarm.conn
2
twall.pole
2L Yarm.conn
x.dlMz.poletip
2L2
Rarm T L( )2 C E twall.pole Rarm
x.dl 0.6 in
z.dlMx.poletip
2L2
Rarm T L( )2 C E twall.pole Rarm
z.dl 0 in
SlopexMz.poletip L
22 Rarm T L
Rarm T L( )2 C E twall.pole Rarm2
Slopex 0.315 deg
11/2/2018 S-1 Clay Model.xmcd 50
SlopezMx.poletip L
22 Rarm T L
Rarm T L( )2 C E twall.pole Rarm2
Slopez 0 deg
MzLoadCase last Ipole68.76 kip ft VzLoadCase last Ipole
7.33 kip Diameterconn.pole 19 in
MxLoadCase last Ipole136.39 kip ft VxLoadCase last Ipole
0 kip Diameterbase.pole 22 in
MyLoadCase last Ipole179.77 kip ft AxialForceLoadCase last Ipole
4.56 kip twall.pole 0.38 in
Mx.polebase00 kip ft Mz.polebase0
0 kip ft My.polebase0Mywd0 last Ipole
Vx.polebase00 kip Vz.polebase0
0 kip AxialForcepolebase0AxialForcewd0 last Ipole
Mx.polebase1Mxwd1 last Ipole
Mz.polebase1Mzwd1 last Ipole
My.polebase10 kip ft
Vx.polebase1Vxwd1 last Ipole
Vz.polebase1Vzwd1 last Ipole
AxialForcepolebase1AxialForcewd1 last Ipole
Mx.polebase2MxLoadCase last Ipole
Mz.polebase2MzLoadCase last Ipole
My.polebase2MyLoadCase last Ipole
Vx.polebase2VxLoadCase last Ipole
Vz.polebase2VzLoadCase last Ipole
AxialForcepolebase2AxialForceLoadCase last Ipole
dbase.pole Diameterbase.poletarm
tarm1base1
tarm2base2
dbase.arm
max Diameterbase.arm1
max Diameterbase.arm2
Service I Load Deflection at the Pole
MSnMax 0 kip ft
M MS.x n
2 MS.z n
2
Max M M Maxif
0 5 360for
Max
From the curvature results (M/EI) at each section, curve fit a fourth degree polynomial, then integrate twice to get deflections.To get a function for curvature (M/EI), set the y-axis as curvature and the x-axis as distance along the pole ysect starting atthe base. So the constants of integration are zero, and Y are calculated with section zero being at the base.
xplot 0.5 Diameterbase.pole 0.5 Diameterbase.pole 0.5 Diametertip.pole 0.5 Diametertip.pole 0.5 Diameterbase.poleT
yplot 0 in 0 in Ypole Ypole 0 in T
11/2/2018 S-1 Clay Model.xmcd 51
Ylum0Ypole
lum0
MS.lum
E Ipole.lumft
Ylumn 1Ysectionn
lumn 1
MSn
E Ipolen
ft
lim reverse lum Ylumreverse Ylum
ftnn 0 1 11
degree of polynomialto fit:
number of data points: polynomial coefficients:
k 4 nz regress Ylum lum k
coeffs submatrix nz 3 length nz( ) 1 0 0( ) coeffs
3.64 10 5
1.27 10 4
1.91 10 5
1.07 10 6
2.03 10 8
polynomial function: curve x( ) coeffs0 coeffs1 x coeffs2 x2 coeffs3 x3 coeffs4 x4
Polenn curve Ylumnn
1 10 4 1 10 4 3 10 4
10
20
30
poleX-Y dataCurve
Calculated Curvature vs. Curve Fitnow integrate the curvature function twice to get deflections. Note: assuming pole connection to the foundation is rigid, the constantsof integration are zero for both slope and deflection
xxcoeffs0 coeffs1 x coeffs2 x2
coeffs3 x3 coeffs4 x4
d d
evaluates to:
12
coeffs0 x2 16
coeffs1 x3 112
coeffs2 x4
120
coeffs3 x5 130
coeffs4 x6
11/2/2018 S-1 Clay Model.xmcd 52
curve x( )12
coeffs0 x2 16
coeffs1 x3 112
coeffs2 x4 120
coeffs3 x5 130
coeffs4 x6
lateral deflection atpole tip:
Polenn curve Ylumnnft tip max Pole( ) tip 0.8 in
conn Pole10 conn 0.604 in
11/2/2018 S-1 Clay Model.xmcd 53
deflection as a percent of total pole height: lateral deflectionat pole tip:
Deflection%conn
Yarm.conntip 0.8 inDeflection% 0.252 %
conn 0.604 inCheckDeflec10.4.2.1 conn Yarm.conn "OK"
Deflection%tip
Ypole Deflection% 0.291 %
Chk10.4.2.1 Check10.4.2.1 Deflection%( )
Chk10.4.2.1 "OK" [LTS-1, 10.4.2.1]
fSlope x( ) coeffs0 x12
coeffs1 x2 13
coeffs2 x3 14
coeffs3 x4 15
coeffs4 x5
Slope fSlope Ylum110.072
inft
CheckSlope10.4.2.1 Slope( ) "OK"
graph the calculated deflected shape:
10
20
30poleDeflection (in)
Deflection
maxPole
in
11/2/2018 S-1 Clay Model.xmcd 54
1 0.5 0 0.5 1
Analyze Pole
Summary - Upright Geometry
Gap7.5
0
in
Ypole 23 ft Yarm.conn 20 ft 0 deg
Diameterbase.pole 22 in twall.pole 0.375 in
Upright Combined Stress Ratio and Deflectionsmax CFIpole 0.353 max x.dl 0.61 in max z.dl 0 in
Chk10.4.2.1 "OK" CheckDeflec10.4.2.1 tip Yarm.conn "OK" CheckSlope10.4.2.1 Slope( ) "OK"
Mast Arm Connection(s) Analysis DataFile "A60S-P4SL-DS145.dat" WindSpeed 150 mph
Connection Properties
Current Values New Values
hconn.plate 30 in inches, for two arm Mast Arms both connection plateheights must be equal (HT)
tvertical.plate0.75
0
in inches (FL)
inches, use X to zero out (SL)
dbolt.conn1.25
0
in inches (FP)
inches, use X to zero out (SP)
tbaseplate.arm3
0
in inches (FK)
inches, use X to zero out (SK)
inches (FJ)bconn.plate.pv
36
36
ininches, use X to zero out (SJ)
Connection Properties
Analyze Connection
Switch values, set values for DataOut11/2/2018 S-1 Clay Model.xmcd 55
out out 1 out 29
hconn.plate fSwitchData hconn.plate newhconn.plate in dataouthconn.plate
indataout 30
out out 1 out 30
tvertical.plate fSwitchData3 tvertical.plate newtvertical.plate in dataouttvertical.plate
indataout
0.75
0
tvertical.plate1if Ltotal.arm2 0 ft= 0 in tvertical.plate1
out out 1 out 31
dbolt.conn fSwitchData3 dbolt.conn newdbolt.conn in dataoutdbolt.conn
indataout
1.25
0
dbolt.conn1if Ltotal.arm2 0 ft= 0 in dbolt.conn1
out out 1 out 32
tbaseplate.arm fSwitchData3 tbaseplate.arm newtbaseplate.arm in dataouttbaseplate.arm
indataout
3
0
tbaseplate.arm1if Ltotal.arm2 0 ft= 0 in tbaseplate.arm1
out out 1 out 33
bconn.plate.pv fSwitchData3 bconn.plate.pv newbconnplate.arm in dataoutbconn.plate.pv
indataout
36
36
bconn.plate.pv1if Ltotal.arm2 0 ft= 0 in bconn.plate.pv1
Design ParametersTrial Plate Thicknesses and Bolt Diameter j 0 1
Design Criteria:PRbolt <1 (performance ratio of bolt), PRt.baseplate.arm <1 (performance ratio of arm base plate), & CSRt.vert.plate <1 (combined stress ratio of vertical plate).
#ConnBoltsj
66
Fy.baseplate 36 ksi (for the base plate)
Applied Loads From Mast Arm Design
Mdl65.0
0.0
kip ft Vdl.arm2.7
0.0
kip tarm0.375
0
in dbase.arm14
0
in
Note: Gap is the distance between the uprightand the Arm Base Plate. (5.5 inches is asuggested minimum for two arm poles)
Mwl171.2
0.0
kip ft Vwl.arm6.0
0.0
kip Gap7.5
0
in
11/2/2018 S-1 Clay Model.xmcd 56
Diameterconn.pole 19.229 in From Upright Design(at arm connection)
(FO)
(SO)Offsetconn Gap
Diameterconn.pole
2 Offsetconn17.115
9.615
in
Total Factored Moment and Shear
AISC LRFD, Vol 1, 6-A4 Specs, 2nd Ed.Mu.connj
Mdlj
2 Mwlj
2 Mu.conn183.1
0.0
kip ft
Vu.connjVdl.armj
2 Vwl.armj
2 Vu.conn6.6
0.0
kip
Mu.pole nmax 0.732 Mz n
Mx nMz n
0.268 Mx n0.268 Mz n
Mx n
m
Arm Base Plate Dimensions
Control dimensions
Distancebolt.edgejCeil 2 dbolt.connj
14
in
rounded up to the next 1/4 inch dimension Distancebolt.edge2.5
0
in
ControlDimj if dbase.armjDiameterconn.pole Ceil dbase.armj
12
in
Ceil Diameterconn.pole12
in
ControlDim19.5
19.5
in
Minimum Mast Arm base plate height tvertical.plate1if tvertical.plate1
0 in= .1 in tvertical.plate1
hmin.conn.platejmax
dbase.armj3 in
3dbase.armj
2
3
tarmj
12tvertical.platej
hmin.conn.plate18.6
3.0
in
hconn.plate 30 in
Mast Arm base plate height, rounded up to next 1 inch dimension if necessary
hconn.plate if hconn.plate max hmin.conn.plate hconn.plate Ceil max hmin.conn.plate in hconn.plate 30 in
Mast Arm base plate width
11/2/2018 S-1 Clay Model.xmcd 57
bconn.platejControlDimj 2 Distancebolt.edgej
4 dbolt.connj2 tvertical.platej bconn.plate
31
19.7
in
Mast Arm base plate width round up to next 1 inch dimension
(FJ)
(SJ)bconn.platej
if tvertical.platej0 in= 0 in Ceil bconn.platej
in bconn.plate31
20
in
checkconn.plate.widthjif bconn.plate.pvj
bconn.platej"OK" "NG"
checkconn.plate.width"OK"
"NG"
Bolt spacing
Spacingbolts.connjif tvertical.platej
0 in= 0 inhconn.plate 2 Distancebolt.edgej
0.5 #ConnBoltsj 1
(FS)
(SS)Spacingbolts.conn
12.5
15
in
D. Calculate Bolt Loads
Calculate Capacities of Connection Elements Based on the AISC LRFD Code, 2nd Edition
(Research Report 1126-4F by the Bureau of Engineering Research at the Univ. of Texas at Austin)(Design of bolts and plates based on "Design Guide for Steel to Concrete Connections by Cook, Doerr &Klingner)
Calculate Capacities of Connection Elements Based on the AISC LRFD Code, 13th Edition
Compute Shear Capacity of Back Truss Bolts (A325) [AISC J3]
bolt 0.75
Fnv.bolt 48 ksi
Fnt.bolt 90 ksi Fnt.bolt 90 ksi
Gross Bolt Area used forshear
Agross.boltjif dbolt.connj
0 in= 0.01 in2dbolt.connj
2
2
Agross.bolt
1.227
0.01
in2
Tn.boltsjAgross.boltj
Fnt.bolt
#ConnBoltsj
2Tn.bolts
331.3
2.7
kip
Bending plane under full dead and wind load
11/2/2018 S-1 Clay Model.xmcd 58
j atanMdlj
Mwlj
20.8
0.0
deg
Calculate the bolt moment arm
RCj
bconn.plate.pvj
2Distancebolt.edgej
cos j
dbase.armj
2
RC23.6
0
in
dbase
Diametertemp.arm1
Diametertemp.arm2
dbase14
18
in bconn.plate.pv36
0
in hconn.plate 30 in20.8
0.0
de
Yieldangletestjatan
bconn.plate.pvj
2
dbasej
2
dbasej
21 cos j
hconn.plate
2
dbasej
2sin j
Yieldangletest33.23
30.96
Yieldlinej
bconn.plate.pvj
2
dbasej
2
dbasej
21 cos j tan j
hconn.plate
2
dbasej
2sin j
if sin j 0= 1 sin j Yieldline
45.678
9
in
Yieldlinej if Yieldangletestj j Yieldlinejhconn.plate
cos j
Yieldline
32.087
9
in
Mp.platejYieldlinej Fy.baseplate
tbaseplate.armj
2
4Mp.plate
216.6
0
kip
See Reference file for variable definitions
CompForceOffsetj if 0.5bconn.plate.pvj
cos j0.5 in
Mp.platej
Tn.boltsj
0.5bconn.plate.pvj
cos j0.5 in
Mp.platej
Tn.boltsj
CompForceOffset7.8
0.
Tu.connj
Mu.connj
RCj CompForceOffsetj tarmjTu.conn
69.1
0.0
kip
DistAj
bconn.plate.pvj
2Distancebolt.edgej
DistA15.5
0
in
11/2/2018 S-1 Clay Model.xmcd 59
Tu.bolt.maxj
Tu.connj
0.5 #ConnBoltsj
DistAj tan j Tu.connj#ConnBoltsj 0.25 0.5 Spacingbolts.connj
0
floor 0.25 #ConnBoltsj
n
#ConnBoltsj 0.5 1 2 n
2Spacingbolts.connj
2
2
Tu.bolt.max39.3
0.0
kip
Vu.boltj
Vu.connj
#ConnBoltsjShear perBolt
Vu.bolt1.10
0.00
kip
fvj
Vu.boltj
Agross.boltj
Bolt Shear Stress fv0.89
0.00
ksi
ftj
Tu.bolt.maxj
Agross.boltj
Bolt Tensile Stress ft32.0
0.0
ksi
F'nt.Boltj1.3Fnt.bolt
Fnt.bolt
bolt Fnv.boltfvj
F'nt.Bolt114.766
117
ksi
F'nv.Boltj1.3Fnv.bolt
Fnv.bolt
bolt Fnt.boltftj
F'nv.Bolt39.633
62.4
ksi
Rr.Boltj bolt
Ft Fnt.bolt
Fv Fnv.bolt ftj20% Fnt.boltif
Fv F'nv.Boltjotherwise
fvj20% Fnv.boltif
Ft F'nt.Boltj
Fv Fnv.bolt ftj20% Fnt.boltif
Fv F'nv.Boltjotherwise
otherwise
Ft
Fv
Rr.Bolt0
67.5
29.725
ksi Rr.Bolt1
67.5
36
ksi
11/2/2018 S-1 Clay Model.xmcd 60
CheckBoltConnBoltjK1 fCheckStress ftj
Rr.Boltj 0
K2 fCheckStress fvjRr.Boltj 1
"OK" K1 "OK"= K2 "OK"=if
"NG" otherwiseCheckBoltConnBolt
"OK"
"OK"
Check Arm Base Plate Thickness
AASHTO LTS minimum base plate thickness:
tmin.bpl.LTS 2 in [LTS-1, Table 5.6.3-1] tmin.bpl.SM 2.5 in [SM 5.6.3-1]
See Reference file for formula derivations 0.90
tbaseplate.arm.reqdjif Vu.connj
0= 0 in4 Tu.bolt.maxj
DistAj
dbase.armj
2
Fy.baseplate hconn.plate
tbaseplate.arm.reqd
1.17
0.00
in
tbaseplate.arm.reqdjif Vu.connj
0= 0 in max tmin.bpl.LTS tmin.bpl.SM tbaseplate.arm.reqdj
tbaseplate.arm.reqdj
2.50000.0000
in tbaseplate.arm3.000
0.000
in
PRt.baseplate.armj
tbaseplate.arm.reqdj
tbaseplate.armj
PRt.baseplate.arm0.83
0
(if PR <= 1.0 ok)
Upright Connection Plate Thickness
See Reference file for formula derivations
tconn.plate.reqdjif Vu.connj
0= 0 in4 Tu.bolt.maxj
bconn.plate.pvjDiameterconn.pole 2 tvertical.platej
2 Distancebolt.edgej
2
Fy.baseplate hconn.plate
tconn.plate.reqdjif Vu.connj
0= 0 in max tmin.bpl.LTS tconn.plate.reqdj
tconn.plate.reqdj
2.00000 0000
in
11/2/2018 S-1 Clay Model.xmcd 61
0.0000
Round up to next quarter inch dimension. tconn.plate.reqd2.00
0.00
in
(FR)
(SR)tconn.platej
Ceil tconn.plate.reqdj
18
in
round up to next1/8 inch dim. tconn.plate
2.000
0.000
in
PRt.connplate.armj
tconn.plate.reqdj
tconn.platej
PRt.connplate.arm1
0
Weld Size of Arm to Plate Connection
NOTE: Old fillet welds, not used.
(Design welds of the socket joint to carry 100% of the design load using an E70 electrode.).
Sweldj
dbase.armj
2
2
Lweldjdbase.armj
Weld Properties
Total Stress on Weldfweldj
Mu.connj
Sweldj
2 Vu.connj
Lweldj
2
fweld14.27
0.00
kipin
Max. Bottom WeldSize
(FM)
(SM)wbot.armj
if tarmj0 in= 0 in tarmj
116
in
wbot.armjCeil wbot.armj
116
in
wbot.arm
0.3125
0
in
Bottom Weld Stressfbot.weldj
wbot.armj0.75( ) 0.6( ) 70 ksi( )
1
2
fbot.weld6.96
0.00
kipinAISC Table J2.5
ftop.weldjfweldj
fbot.weldjTop Weld Stress ftop.weld
7.31
0.00
kipin
wtop.armj
ftop.weldj
0.75( ) 0.6( ) 70 ksi( )1
2
Top Weld Size wtop.armjCeil wtop.armj
116
in
wtop.arm0.3750
0.0000
in
Round up tonext 1/16 inch
(FQ)
(SQ)wtop.armj
if wtop.armjtarmj
wtop.armjCeil tarmj
116
in
wtop.arm
0.3750
0.0000
in
Size of Vertical Welds to Upright
(Design welds to resist dead load moment , wind load moment, and dead load shear using an E70 electrode)
11/2/2018 S-1 Clay Model.xmcd 62
Sdl.momhconn.plate
2
3Weld Properties Swl.mom Diameterconn.pole hconn.plate
Adl.shr 2 hconn.plate ruprightDiameterconn.pole
2
fweldj
MdljVdl.armj
rupright Gapj Sdl.mom
2 MwljVwl.armj
rupright Gapj Swl.mom
2 Vdl.armj
Adl.shr
2
fweld4.6
0.0
kipin
Plate/Upright Weld size
AISC Table J2.5wvert.platej
fweldj
0.75 0.6 70 ksi( )1
2
wvert.platejCeil wvert.platej
116
in
wvert.plate0.2500
0.0000
in
min weld sizewp.minj
if tvertical.platej
12
in
14
in316
in
AISC Table J2.4
wp.minjif tvertical.platej
0 in= 0 in wp.minj wp.min
0.25
0.1875
in
(FN)
(SN)wvertical.platej
if wvert.platejwp.minj
wvert.platejwp.minj wvertical.plate
0.25
0.1875
in
Size of Vertical Welds to Connection Plate
wconn.platejwvert.platej
wconn.plate0.2500
0.0000
in
min weld sizewc.minj
if tconn.platej
34
in
516
in14
in
wc.min0.3125
0.2500
inAISC Table J2.4
min weld sizewc.minj
if wc.minjtvertical.platej
tvertical.platejwc.minj
wc.min0.3125
0.1000
inAISC p. 8-119
(FT)
(ST)wconn.platej
if wconn.platejwc.minj
wconn.platejwc.minj wconn.plate
0.3125
0.1
in
Check Thickness of Vertical Plates
tvertical.plate0.750
0.100
in Trial Plate Thickness
hvertical.plate hconn.plate Avertical.platejtvertical.platej
hvertical.plate Avertical.plate22.5
3
in2
11/2/2018 S-1 Clay Model.xmcd 63
Lbj
Diameterconn.pole
2Gapj tconn.platej
Lb15.1
9.6
in
ryj
tvertical.platej
12ry
0.2
0.0
in
j if tvertical.platej0 in= 0
Lbj
ryj
Controlling Slenderness Parameter
69.8
333.1
Plastic MomentMpj
hvertical.plate2 tvertical.platej
4Fy.baseplate Mp
506.2
67.5
kip ft
Limiting Buckling MomentMrj
hvertical.plate2 tvertical.platej
6Fy.baseplate Mr
337.5
45.0
kip ft
Jj 0.3 tvertical.platej
3 hvertical.plate Aj Avertical.platejE 29000 ksi
pj
3750 ksi( ) Jj Aj
Mpj
Flexural Slenderness Parameters p5.7
0.8
rj
57000 ksi( ) Jj Aj
Mrj
AISC Table A-F1.1 r130.1
17.3
For lp < l<= l
r
\Nominal Flex. StrengthMnj
MpjMpj
Mrj
j pj
rj pj
Mn
419
383
kip ftAISC Eqn A-F1-3
For lr< l
Nominal Flex. StrengthMcrj
57000 ksi( ) Jj Aj
jMcr
629
2
kip ftAISC Eqn F1-14
Mnjif pj j 0.9 Mnj
0.9 Mpj Mn
377.3
345.0
kip ft
Mnjif rj j 0.9 Mcrj
Mnj Mn
377.3
2.1
kip ft
Muj
MdljVdl.armj
rupright Gapj
2Required Flexural Strength Mu
34.4
0.0
kip ft
11/2/2018 S-1 Clay Model.xmcd 64
Column Slenderness Parametercj
if tvertical.platej0 in
Lbj
ryj
Fy.baseplate
E.0
c
0.783
3.735
AISC Eqn E2-4
Nominal Critical StressFcrj
if cj1.5 0.658
cj2
Fy.baseplate
0.877
cj
2
Fy.baseplate
Fcr27.9
2.3
ksiAISC Eqns E2-2 & E2-3
Pnj0.85 Aj Fcrj
Nominal Compressive Strength Pn532.7
5.8
kip
AISC Eqn E2-1
Puj
MwljVwl.armj
rupright Gapj Diameterconn.pole
Required Compressive Strength Pu112.2
0
kip
Combined Stress RatioFlexure and Tension members
CFIt.vert.platejfCFIsimple Puj
Pnj1.0 Muj
Mnj CFIt.vert.plate0.292
0.000
AISC Eqns H1-1a & H1-1b (if CSR<1, then ok)
PR0 max
PRt.baseplate.arm0
PRt.connplate.arm0
CFIt.vert.plate0
PR1 if Mdl10 kip ft= 0 max
PRt.baseplate.arm1
PRt.connplate.arm1
CFIt.vert.plate1
PR1.000
0.000
(if PR<1, then ok)
j 0 1 vertplt.widthjrupright Gapj tconn.platej
vertplt.width1if Mdl1
0 kip ft= 0 in vertplt.width1 set variables equal to zero if there is no second arm
bconn.plate.pv1fSetZero bconn.plate.pv1
in tvertical.plate1fSetZero tvertical.plate1
in
Gap1 fSetZero Gap1 in dbolt.conn1fSetZero dbolt.conn1
in
tconn.plate1fSetZero tconn.plate1
in #ConnBolts1 fSetZero #ConnBolts1 1
tbaseplate.arm1fSetZero tbaseplate.arm1
in wbot.arm1fSetZero wbot.arm1
in
wconn.plate1fSetZero wconn.plate1
in Spacingbolts.conn1fSetZero Spacingbolts.conn1
in
wtop.arm1fSetZero wtop.arm1
in wvertical.plate1fSetZero wvertical.plate1
in
Offsetconn1fSetZero Offsetconn1
in
PRbolt1if Ltotal.arm2 0 ft= newLtotal.arm2 "x"= newLtotal.arm2 "X"= 0 PRbolt1
11/2/2018 S-1 Clay Model.xmcd 65
PRt.baseplate.arm1if Ltotal.arm2 0 ft= newLtotal.arm2 "x"= newLtotal.arm2 "X"= 0 PRt.baseplate.arm1
CSRt.vert.plate1if Ltotal.arm2 0 ft= newLtotal.arm2 "x"= newLtotal.arm2 "X"= 0 CSRt.vert.plate1
PRt.connplate.arm1if Ltotal.arm2 0 ft= newLtotal.arm2 "x"= newLtotal.arm2 "X"= 0 PRt.connplate.arm1
Analyze Connection
Summary - Connection Geometry
hconn.plate 30 in Gap7.5
0
in Offsetconn17.1146
0
in
dbolt.conn1.25
0
in #ConnBolts6
0
Spacingbolts.conn12.5
0
in
tconn.plate2
0
in bconn.plate.pv36
0
in tvertical.plate0.75
0
in tbaseplate.arm3
0
in
wconn.plate0.3125
0
in wvertical.plate0.25
0
in
Connection Ratios
CheckBoltConnBolt"OK"
"OK"
CFIt.vert.plate0.292
0
PRt.baseplate.arm0.833
0
PRt.connplate.arm1
0
Base Plate Analysis DataFile "A60S-P4SL-DS145.dat" WindSpeed 150 mph
Base Plate Properties
Current Values New Values#AnchorRods 6 use 6 bolts minimum
dbolt.pole 2 in inches (BC)
Base Plate Properties
Analyze Base Plate & Anchors
Switch values, set values for DataOut
out out 1 out 34
#AnchorRods fSwitchData #AnchorRods new#AnchorRods 1( ) dataout #AnchorRods dataout 6
out out 1 out 35
dbolt.pole fSwitchData dbolt.pole newdbolt.pole in dataoutdbolt.pole
indataout 2
Applied Loads (from Upright Design)
11/2/2018 S-1 Clay Model.xmcd 66
maximum torsion (Mx & Mz not used)maximum overturning (My not used) maximum CSR
My.polebase
179.8
0.0
179.8
kip ft Mz.polebase
0.0
68.8
68.8
kip ftMx.polebase
0.0
136.4
136.4
kip ft
Diameterbase.pole 22 in
twall.pole 0.3750 inVx.polebase
0.0
0.0
0.0
kip AxialForcepolebase
4.6
4.6
4.6
kip Vz.polebase
0.0
7.3
7.3
kipB 1.02
load cases for maximum torsion (T), overturning (OT), and Combined Force Interation (CFI)
LoadCaseT 0 LoadCaseOT 1 LoadCaseCFI 2
Mx.polebaseLoadCaseT0.0 kip ft My.polebaseLoadCaseT
179.8 kip ft Mz.polebaseLoadCaseT0.0 kip ft
Mx.polebaseLoadCaseOT136.4 kip ftMy.polebaseLoadCaseOT
0.0 kip ft Mz.polebaseLoadCaseOT68.8 kip ft
Mx.polebaseLoadCaseCFI136.4 kip ftMy.polebaseLoadCaseCFI
179.8 kip ft Mz.polebaseLoadCaseCFI68.8 kip ft
Base Plate Size
Diameterbaseplate.pole Diameterbase.pole 8 dbolt.pole Diameterbaseplate.pole 38 in
Diameterboltcircle.pole Diameterbase.pole 2 2 dbolt.pole Diameterboltcircle.pole 30 in
Irod.groupDiameterboltcircle.pole
2
8#AnchorRods Irod.group 675 in2
Srod.groupIrod.group
Diameterboltcircle.pole
2
Srod.group 45 in
Anchor Rod Strength
Mcsr.pole Mx.polebaseLoadCaseCFI
2 Mz.polebaseLoadCaseCFI
2
Mcsr.pole 152.7 kip ft
Tu.rodMcsr.pole
Srod.groupTu.rod 40.7 kip
Vcsr.pole Vx.polebaseLoadCaseCFI
2 Vz.polebaseLoadCaseCFI
2 Vcsr.pole 7.3 kip
11/2/2018 S-1 Clay Model.xmcd 67
Vu.rodVcsr.pole
#AnchorRods
My.polebaseLoadCaseCFI
Diameterboltcircle.pole
2
#AnchorRods
Vu.rod 25.2 kip
AAnchor Dbolt dbolt.pole
nthreads 8 Dbolt 1 in=if
7 Dbolt 1.125 in= Dbolt 1.25 in=if
6 Dbolt 1.5 in=if
5 Dbolt 1.75 in=if
4.5 Dbolt 2 in= Dbolt 2.25 in=if
4 Dbolt 2.5 inif
A4
Dbolt0.9743 in
nthreads
2
Areturn
dbolt.pole 2 in
AAnchor 2.498 in2
ft.rodTu.rod
AAnchorft.rod 16.304 ksi
fv.rodVu.rod
AAnchorfv.rod 10.083 ksi
Design per AISC J3
Fy.Anchor 55 ksi Fy.Anchor 55 ksi
Fu.Anchor 75 ksi Fu.Anchor 75 ksi
bolt 0.75
Fnv.Anchor 0.5 Fu.Anchor Fnv.Anchor 37.5 ksi
Fnt.Anchor 0.75 Fu.Anchor Fnt.Anchor 56.25 ksi
F'nt.Anchor 1.3Fnt.AnchorFnt.Anchor
bolt Fnv.Anchorfv.rod
F'nt.Anchor 52.958 ksi
11/2/2018 S-1 Clay Model.xmcd 68
F'nv.Anchor 1.3Fnv.AnchorFnv.Anchor
bolt Fnt.Anchorft.rod
F'nv.Anchor 34.257 ksi
Rr.Anchor bolt
Ft Fnt.Anchor
Fv Fnv.Anchor ft.rod 20% Fnt.Anchorif
Fv F'nv.Anchor otherwise
fv.rod 20% Fnv.Anchorif
Ft F'nt.Anchor
Fv Fnv.bolt ft.rod 20% Fnt.Anchorif
Fv F'nv.Anchor otherwise
otherwise
Ft
Fv
Rr.Anchor39.719
25.693
ksi
CheckAnchor.Bolt.Capacity K1 fCheckStress ft.rod Rr.Anchor0
K2 fCheckStress fv.rod Rr.Anchor1
"OK" K1 "OK"= K2 "OK"=if
"NG" otherwise
CheckAnchor.Bolt.Capacity "OK"
Base Plate Thickness
Design plate thickness based on yield line theory 0.90
tbaseplate.pole.reqdMcsr.pole
Diameterboltcircle.pole
2
Diameterbase.pole
2
Fy.baseplateDiameterboltcircle.pole
2
Diameterbase.pole
2
1
2
tbaseplate.pole.reqd 1.171 in
minimum base plate thickness
11/2/2018 S-1 Clay Model.xmcd 69
tbaseplate.pole.reqd if tbaseplate.pole.reqd dbolt.pole dbolt.pole tbaseplate.pole.reqd LTS 5.14.3SM V3 5.14.3
tbaseplate.pole.reqd if tbaseplate.pole.reqd 2.5 in 2.5 in tbaseplate.pole.reqd
tbaseplate.pole Ceil tbaseplate.pole.reqd18
in
Round up to next1/8 inch dim.
tbaseplate.pole 2.500 in
PRplate.poletbaseplate.pole.reqd
tbaseplate.polePRplate.pole 1
final Diameter.tip.poleadjusted for t.baseplate.pole.Diametertip.pole Diameterbase.pole Ypole tbaseplate.pole Taper Diametertip.pole 18.81 in
Weld Sizes of Upright to Base Plate Connection
NOTE: Old fillet welds, not used.
(Design welds of the socket joint to carry 100% of the design load using an E70 electrode.).
Sweld.poleDiameterbase.pole
2
2
Lweld.pole Diameterbase.pole
AISC LRFD, Vol 1, 6-A4 Specs, 2nd Ed.
fweld.poleMcsr.pole
Sweld.pole
2 Vcsr.pole
Lweld.pole
My.polebaseLoadCaseCFI
0.5 Diameterbase.pole2
2
fweld.pole 5.6kipin
wbot.pole twall.pole116
in
wbot.pole Ceil wbot.pole116
in
wbot.pole 0.3125 in
fbot.weld.pole wbot.pole 0.75( ) 0.6 70 ksi( )1
2
fbot.weld.pole 7kipinAISC Table J2.5
ftop.weld.pole fweld.pole fbot.weld.pole ftop.weld.pole 1.3kipin
wtop.poleftop.weld.pole
0.75( ) 0.6( ) 70 ksi1
2
wtop.pole Ceil wtop.pole116
in
wtop.pole 0.0000 in (BD)
(BE)wtop.pole if wtop.pole twall.pole wtop.pole Ceil twall.pole116
in
wtop.pole 0.3750 in
11/2/2018 S-1 Clay Model.xmcd 70
Analyze Base Plate & Anchors
Summary - Upright Base Plate Geometry
#AnchorRods 6 dbolt.pole 2 in tbaseplate.pole 2.5 in Diameterbaseplate.pole 38 in
Upright Base Plate Performance Ratios
CheckAnchor.Bolt.Capacity "OK" PRplate.pole 1 checkconn.plate.width"OK"
"NG"
Foundation Analysis Cohesionless or Cohesive Soil DataFile "A60S-P4SL-DS145.dat"
Soil Properties
Current Values New Values
SoilType 1 0 - clay 1 - sand
soil 30 deg degrees, soil friction angle (sand)
csoil 2000 psf psf, soil shear strength (clay)
soil 50 pcf pcf, soil density (typical design value = 45-50 pcf)
vertical distance between top offoundation and groundlineOffset 0 ft
Nblows 15 Number of blows per foot.If N< 5, contact the district geotech Engineer SM V3 13.6
Soil Properties
Analyze Foundation
Switch values, set values for DataOut, and Write Out Data to DataFile and Temp.dat
out out 1 out 36
SoilType if newSoilType 0= 0 1( ) dataout SoilType dataout 0
out out 1 out 37
soil fSwitchData soil new soil deg dataoutsoil
degdataout 7.73
out out 1 out 38
csoil fSwitchData csoil newcsoil psf dataoutcsoil
psfdataout 1145
out out 1 out 39
soil fSwitchData soil new soil pcf dataoutsoil
pcfdataout 57.67
out out 1 out 40
11/2/2018 S-1 Clay Model.xmcd 71
water 62.4 pcf dataoutwater
pcfdataout 62.4(not used)
out out 1 out 41
Offset fSwitchData Offset newOffset ft( ) dataoutOffset
ftdataout 0
out out 1 out 42
Nblows fSwitchData Nblows newNblows 1 dataoutNblows
1dataout 11
out out 1 out 43
Subject if newSubject 0= Subject newSubject( ) dataout Subject
dataout "A60/S-P4/S/L-DS5.0/16/4.5"
out out 1 out 44
ProjectNo if newProjectNumber 0= ProjectNo newProjectNumber( ) dataout ProjectNo
dataout "Design Standard"
out out 1 out 45
PoleLocation if newPoleLocation 0= PoleLocation newPoleLocation( ) dataout PoleLocation
dataout "Index 17743"out out 1 out 46Date if newDate 0= Date newDate( ) dataout Date
dataout "09/28/2016"
out out 1 out 47
DesignedBy if newDesignedBy 0= DesignedBy newDesignedBy( ) dataout DesignedBy
dataout "FDOT"out out 1 out 48
CheckedBy if newCheckedBy 0= CheckedBy newCheckedBy( ) dataout CheckedBy
dataout "FDOT"
WRITEPRN DataFile( ) data WRITEPRN "temp.dat"( ) data
Foundation Design References
LRFD = AASHTO LRFD Bridge Design Specifications
SM V3 = FDOT Structures Manual Volume 3
SDG = FDOT Structures Design Guidelines
Spec = FDOT Standard Specifications
ACI = ACI 318 Structural Concrete Building Code
UF Report = FDOT/University of Florida Report BD545 RPWO #54
11/2/2018 S-1 Clay Model.xmcd 72
Applied Loads (From Arm1 Design)
WindSpeed 150 mph
(from Base Plate Design)
#AnchorRods 6 dbolt.pole 2 in Diameterboltcircle.pole 30 in Tu.rod 40.7 kip
(from Upright Design)
LoadCaseT 0
Mx.polebase
0
136.4
136.4
kip ft My.polebase
179.8
0
179.8
kip ft Mz.polebase
0
68.8
68.8
kip ft LoadCaseOT 1
LoadCaseCFI 2
Vx.polebase
0
0
0
kip AxialForcepolebase
4.6
4.6
4.6
kip Vz.polebase
0
7.3
7.3
kip
Foundation Diameter
Diametershaft Diameterboltcircle.pole 12 in 12 in Diametershaft 4.5 ft
round shaft diameter up to the nearest half foot dimension to accommodate available coring equipment
11/2/2018 S-1 Clay Model.xmcd 73
Diametershaft Ceil Diametershaft12
ft
Diametershaft 4.5 ft
Diametershaft.custom 0 ft
Diametershaft if Diametershaft.custom 0 ft Diametershaft.custom Diametershaft 1.372
b Diametershaft
Shaft Depth Required to Resist Overturning
ot 0.6 SM V3 13.6 Offset 0 ft vertical distance between top offoundation and groundline
Mtotal Mx.polebaseLoadCaseOT
2 Mz.polebaseLoadCaseOT
2 Mtotal 152.7 kip ft
Ptotal Vx.polebaseLoadCaseOT
2 Vz.polebaseLoadCaseOT
2 Ptotal 7.3 kip
short free-head pile in cohesionless soil using Broms method
Kp tan 45 degsoil
2
2
esand Offset
Guess value LotSand 8 ft
Given ot3 soil Kp b LotSand LotSand
213
LotSand
Ptotal esand LotSand Mtotal 0 kip ft=
Temp Find LotSand LotSand Temp LotSand 13.512 ft
(round up to next foot) LotSand ceilLotSand
ft
ft LotSand 14 ft
DCRatiootSandMtotal Ptotal esand LotSand
ot soil b LotSand3 Kp
2
DCRatiootSand 0.912
short free-head pile in cohesive soil using Modified Broms method for L < 3b (see reference file forderivation)
csoil if csoil 0 ksf= 0.1 ksf csoil Slope 8csoil
3 beclay
Mtotal
PtotalOffset
nforce M N( ) Slope 2 M N( ) 2 csoil Nb2
mforce M( ) 2 csoil M Slope Mb2
11/2/2018 S-1 Clay Model.xmcd 74
m_arm M( ) eclayM3
2 M Slope csoil csoil
M Slope 2 csoil
n_arm M N( ) eclay MN3
2 N Slope M Slope csoil M Slope csoil
Slope 2 M N( ) 2 csoil
Guess value M 4.0 ft N 4.0 ft
Given Ptotal ot nforce M N( ) ot mforce M( )= mforce M( ) m_arm M( ) nforce M N( ) n_arm(=
M
N
Find M N( ) Lot1Clay.temp M N Lot1Clay.temp 8.925 ft
(round up to next foot) Lot1Clay ceilLot1Clay.temp
ft
ft Lot1Clay 9 ft
short free-head pile in cohesive soil using Regular Broms method for L > 3b
fclayPtotal
9 ot csoil bMmaxtemp Ptotal eclay 1.5 b 0.5 fclay g
Mmaxtemp
2.25 ot csoil b
Lot2Clay 1.5 b fclay g Lot2Clay 12.418 ft
(round up to next foot) Lot2Clay ceilLot2Clay
ft
ft Lot2Clay 13 ft
LotClay if Lot1Clay 3 b Lot1Clay Lot2Clay LotClay 9 ft
(If Lot < 3b, use Modified Broms method)
DCRatiootClay if LotClay 3 bLot1Clay.temp
Lot1Clay
Mmaxtemp
2.25 ot csoil b
Ptotal
9 ot csoil b
Lot2Clay 1.5 b
DCRatiootClay 0.992
LreqdOT if SoilType 1= LotSand LotClay LreqdOT 9 ft
DCRatioot if SoilType 1= DCRatiootSand DCRatiootClay DCRatioot 0.992
Shaft Depth Required to Resist Torsion
11/2/2018 S-1 Clay Model.xmcd 75
NOTE: fdot and are based upon CONCRETE and soilinteraction. This torsion methodology is not to be used withpermanent casing.
torDS 0.9 SM V3 13.6
Nblows 11 Number of blows per foot. If N< 5, contact the district geotech Engineer
fdot if Nblows 5 0 if Nblows 15 1.5 1.5Nblows
15
1.1 load transfer ratio
tan soil 0.136 coefficient of friction between concrete shaft and soil
concrete 150 pcf concrete concrete water concrete 87.6 pcf
CohesionFactor 0.55 fse CohesionFactor csoil
Torsion My.polebaseLoadCaseTTorsion 179.8 kip ft
short free-head pile in cohesionless soil
Guess value LtorSand LreqdOT
Given
Torsion torDS b LtorSand soilLtorSand
2
fdotb2
=
Temp Find LtorSand LtorSand Temp LtorSand 14.1 ft
(round up to next foot) LtorSand ceilLtorSand
ft
ft LtorSand 15 ft
DCRatiotorSandTorsion
torDS b LtorSand soilLtorSand
2
fdotb2
DCRatiotorSand 0.88
short free-head pile in cohesive soil
Guess value LtorClay LreqdOT
GivenTorsion
torDSfse b( ) LtorClay 1.5 ft
b2
fseb2
2 b3
=
Temp Find LtorClay LtorClay Temp LtorClay 10.72 ft
11/2/2018 S-1 Clay Model.xmcd 76
(round up to next foot) LtorClay ceilLtorClay
ft
ft LtorClay 11 ft
DCRatiotorClay
Torsion
torDS
fse b( ) LtorClay 1.5 ftb2
fseb2
2 b3
DCRatiotorClay 0.973
LreqdTor if SoilType 1= LtorSand LtorClay LreqdTor 11 ft
DCRatiotor if SoilType 1= DCRatiotorSand DCRatiotorClay DCRatiotor 0.973
Lembedded if LreqdTor LreqdOT LreqdTor LreqdOT Lembedded 11 ft
Lshaft Lembedded Offset Lshaft 11 ft
DCRatiofoundation if LreqdTor LreqdOT DCRatiotor DCRatioot DCRatiofoundation 0.973
Unfactored Maximum Moment in Shaft
short free-head pile in cohesionless soil using Broms method
fsand2 Ptotal
3 soil b Kp otfsand 4.892 ft
MmaxSand Ptotal esand fsandPtotal fsand
3Mtotal MmaxSand 176.6 kip ft
short free-head pile in cohesive soil using Modified Broms method for L < 3b (see reference file forderivation)
Guess value fmod 4.0 ft
Given Ptotalfmod b
22 ot csoil fmod Slope=
fmod Find fmod fmod 1.401 ft
MmodBroms Ptotal eclay fmodot csoil b fmod
2
2
b fmod3 Slope
6MmodBroms 158.6 kip ft
short free-head pile in cohesive soil using Regular Broms method for L > 3b
MBroms Ptotal eclay 1.5 b 0.5 fclay MBroms 203.2 kip ft
11/2/2018 S-1 Clay Model.xmcd 77
MmaxClay if Lot1Clay 3 b MmodBroms MBroms MmaxClay 158.6 kip ft
(If Lot < 3b, use Modified Broms method)
Mmax if SoilType 1= MmaxSand MmaxClay (this is a Service moment) Mmax 158.6 kip ft
Minimum Reinforcing and Spacing
Fy.rebar 60 ksi reinforcing yield strength
fc 4.0 ksi concrete strength Spec 346-3
cover 6 in cover SDG Table 1.4.2-1
Abar 1.56 in2 longitudinal bar area
dbar 1.41 in longitudinal bar diameter
Av.bar 0.31 in2 stirrup area SM V3 13.6.2
dv.bar 0.625 in stirrup diameter
sv1 4 in stirrup spacing, depth = 0 ft-2 ft SM V3 13.6.2
sv2 8 in stirrup spacing, depth = 2 ft-depth.stir
sv3 12 in stirrup spacing, depth > depth.stir
sv4 12 in stirrup spacing, depth > depth.stirA
depthstir 9.7 ft stirrup depth, see s.v2 and s.v3 above
depthstirA 14.5 ft irrup depth, see s.v3 and s.v4 above
b 4.5 ft shaft diameter
BarsProv10.01Abar
b2
4BarsProv1 14.681 LRFD 5.7.4.2
BarsProv20.135
Abar Fy.rebar
b2
4fc
BarsProv2 13.213
BarsProv ceil max BarsProv1 BarsProv2 BarsProv 15 number of longitudinal bars
NumSpacesv.bar rounddepthstir 2 ft
sv2
NumSpacesv.bar 12
11/2/2018 S-1 Clay Model.xmcd 78
ReinfClearSpacing b 2 cover dv.bardbar
2
BarsProv
dbar ReinfClearSpacing 6.83 in
CheckReinfClearSpacing if ReinfClearSpacing 6in "OK" "No Good"( ) CheckReinfClearSpacing "OK"
SDG 3.6.10
Check Shear and TorsionLFshr 1.0 Shear Load Factor
LFtor 1.0 Torsion Load Factor
shr 0.90 Shear Resistance Factor LRFD 5.5.4.2.1
tor 0.90 Torsion Resistance Factor LRFD 5.5.4.2.1
Vu LFshr Vx.polebaseLoadCaseOT
2 Vz.polebaseLoadCaseOT
2 Vu 7.3 kip
Tu LFtor Torsion Tu 179.769 kip ft
Area and perimeter of concrete cross-section
Acpb2
2Acp 2290.2 in2
pcp 2b2
pcp 169.6 in
Diameter, perimeter and area enclosed by the centerline of the outermost closed transverse torsion reinforcement
doh b 2 coverdv.bar
2
doh 41.4 in
ph doh ph 130 in
Aohdoh
2
2
Aoh 1344.5 in2
Ao 0.85 Aoh Ao 1142.8 in2 LRFD C5.8.2.1
Effective shear depth
Dr b 2 cover dv.bardbar
2
deb2
Dr3.294 ft
LRFD C5.8.2.1dv max 0.9 de 0.72 b 3.24 ft
Check Shear Strength
11/2/2018 S-1 Clay Model.xmcd 79
Vc 0.0316 2.0( )fc
ksi
dv
in
bin
kip Vc 265.4 kip LRFD Eqn 5.8.3.3-3LRFD 5.8.3.4.1
ACI 11.3.3
VsAv.bar Fy.rebar dv
max sv1 sv2 sv3Vs 60.3 kip LRFD Eqn 5.8.3.3-4
shr 0.9 Vu 7.3 kip
ShearRatioVu shr Vc
shr VsShearRatio 4.269
ShearRatio if ShearRatio 0 0 ShearRatio( ) ShearRatio 0
Check Torsion Strength
Tn12 Ao Av.bar Fy.rebar
sv1Tn1 885.7 kip ft LRFD Eqn 5.8.3.6.2-1
LRFD 5.8.3.4.1
Tn22 Ao Av.bar Fy.rebar
sv2Tn2 442.8 kip ft
Tn32 Ao Av.bar Fy.rebar
sv3Tn3 295.2 kip ft
Tn42 Ao Av.bar Fy.rebar
sv4Tn4 295.2 kip ft
tor 0.9 Tu 179.769 kip ft LreqdTor 11 ft
Tor2sand Tu if 2 ft Offset b 2 ft Offset( ) soil2 ft Offset
2
fdotb2
0 kip ft
175.733 kip ft
Tor3sand Tu if depthstir Offset b depthstir Offset soildepthstir Offset
2
fdotb2
0 kip ft
84.839 kip ft
Tor4sand Tu if depthstirA Offset b depthstirA Offset soildepthstirA Offset
2
fdotb2
0 kip ft
32.357 kip ft
Tor2clay Tu if 2 ft 1.5 ft Offset fse b( ) 2.0 ft Offset 1.5 ft( )b2
0 kip ft
169.753 kip ft
Tor3clay Tu if depthstir 1.5 ft Offset fse b( ) depthstir Offset 1.5 ftb2
0 kip ft
15.511 kip ft
Tor4clay Tu if depthstirA 1.5 ft Offset fse b( ) depthstirA Offset 1.5 ftb2
0 kip ft
80.64 kip ft
11/2/2018 S-1 Clay Model.xmcd 80
Tor2 if SoilType 1= Tor2sand Tor2clay Tor2 169.753 kip ft
Tor3 if SoilType 1= Tor3sand Tor3clay Tor3 15.511 kip ft
Tor4 if SoilType 1= Tor4sand Tor4clay Tor4 80.64 kip ft
TorsionRation1Tu
tor Tn1TorsionRation1 0.23
TorsionRation2Tor2
tor Tn2TorsionRation2 0.43
TorsionRation3Tor3
tor Tn3TorsionRation3 0.06
TorsionRation4Tor4
tor Tn4TorsionRation4 0.3
TorsionRatio max TorsionRation1 TorsionRation2 TorsionRation3 TorsionRation4 TorsionRatio 0.426
Tcr 0.125fc
ksi
Acp2
pcp in3
kip in Tcr 644.1 kip ft LRFD Eqn 5.8.2.1-4
TorsionRatio if Tu 0.25 tor Tcr 0 TorsionRatio TorsionRatio 0.426 LRFD Eqn 5.8.2.1-3
ShearRatio 0
CheckShearTorsion if ShearRatio TorsionRatio 1 "OK" "No Good"( ) CheckShearTorsion "OK"
Check Maximum Spacing Transverse Reinforcement
vuVu
shr b 0.8 b( ) vu 0.00349 ksi LRFD Eqn 5.8.2.9-1
0.125 fc 0.5 ksi
smax1 if 0.8 dv 24 in 0.8 dv 24 in smax1 24 in LRFD Eqn 5.8.2.7-1
smax2 if 0.4 dv 12 in 0.4 dv 12 in smax2 12 in LRFD Eqn 5.8.2.7-2
smax if vu 0.125 fc smax1 smax2 smax 24 in
max sv1 sv2 sv3 12 in
CheckMaxSpacingTransvReinf if max sv1 sv2 sv3 smax "OK" "No Good" CheckMaxSpacingTransvReinf "OK"
11/2/2018 S-1 Clay Model.xmcd 81
Check Longitudinal Reinforcement for Combined Shear and Torsion LRFD Eqn 5.8.3.6.3-1
LRFD 5.8.3.4.1Mu LFtor Mx.polebaseLoadCaseOT
2 Mz.polebaseLoadCaseOT
2
Mu 152.7 kip ft
Vtemp ifVu
shr0.5 Vs 0 kip
Vu
shr0.5 Vs 0 kip
Vtemp 0 kip
LongReinfshr.tor
Mu
tor 0.8 b( )
Vtemp
kip
2 0.45 ph Tu
2 Ao tor kip
2
kip
Fy.rebarLongReinfshr.tor 1.808 in2
BarsProv Abar 23.4 in2
CheckLongReinfshr.tor if BarsProv Abar LongReinfshr.tor "OK" "No Good" CheckLongReinfshr.tor "OK"
Anchor Bolt Embedment
Gapshaftb 2 cover 2 dv.bar Diameterboltcircle.pole dbar
2
Gapshaft 4.67 in
Diameterrebar.circle b 2 cover dbar 2 dv.bar
Diameterrebar.circle 39.3 in
#BarsProvided BarsProv #BarsProvided 15
Use a maximum of three rebarper anchor bolt (conservative)#BarsProvidedPerRod min
#BarsProvided#AnchorRods
3
#BarsProvidedPerRod 2.5
0.9 #BarsReqdPerRodTu.rod
Abar Fy.rebar
Diameterboltcircle.pole
Diameterrebar.circle #BarsReqdPerRod 0.37
11/2/2018 S-1 Clay Model.xmcd 82
AreaRatio#BarsReqdPerRod
#BarsProvidedPerRodAreaRatio 0.15
AreaRatio if AreaRatio 1 AreaRatio 1( ) AreaRatio 0.15
2015 AASHTO Development Length of Deformed Bars in Tension 5.11.2.1
cover 6 in
cb= the smaller of the distance from center of bar or wire being developed to the nearest concretesurface and one half the center-to-center spacing of the bars or wires being developed
cb min cover dv.bardbar
2
ReinfClearSpacing dbar
2
4.12 in
ktr 0 in. assume no transverse bars:
rc min 1 max 0.4dbar
cb ktr
LRFD Eqn 5.11.2.1.3-1
rc 0.4
Ld.bar max 12in rc 2.4 dbarFy.rebar
fc ksi
tension development length LRFD Eqn 5.11.2.1.1-2
SpacingFactor max#BarsProvidedPerRod 0.5 0.5
0.5
SpacingFactor 0.75
Lembedment.added ReinfClearSpacing SpacingFactor( )2 Gapshaft2 Lembedment.added 6.9 in
Lembedment.rod maxLd.bar AreaRatio( ) 12 in Lembedment.added
20 dbolt.pole
11/2/2018 S-1 Clay Model.xmcd 83
Note: 20danchor minimum embedment was in old AASHTO LTS, 2nd Ed. 1985 and 3rd Ed. 1994 in Section 3 - 1.3.4. It was removedin the 4th Ed., but is still a good rule of thumb.
Lembedment.rod Ceil Lembedment.rod in Lembedment.rod 40 in
Lanchor.rod Ceil Lembedment.rod 8 in in Lanchor.rod 48 in
Anchor Bolt Shear Break-Out Strength
References:ACI 318-05 Appendix D.FDOT/University of Florida Report BD545 RPWO #54,Anchor Embedment Requirements for Signal/Sign Structures, July 2007.
#AnchorRods 6 number of anchor bolts
dbolt.pole 2 in anchor bolt diameter
Diameterboltcircle.pole 30 in anchor bolt circle diameter
Lembedment.rod 40 in anchor bolt embedment
b 54 in shaft diameter
rbDiameterboltcircle.pole
2rb 15 in
rb2
r 27 in
ca1rb
2 3.25 r2 rb2
rb
3.25ca1 8.67 in adjusted cover
UF Report Eqn 3-2
Le min 8 dbolt.pole Lembedment.rod Le 16 in load bearing length of anchor for shear
ACI D.6.2.2
Vb 13Le
dbolt.pole
0.2 dbolt.pole
in
fc
psi
ca1
in
1.5
lbf shear break-out strength (single anchor)
UF Report Eqn 2-11Vb 45 kip
11/2/2018 S-1 Clay Model.xmcd 84
bolt.sector360 deg( )
#AnchorRods60 deg UF Report Fig 3-7
alpha 2 asin1.5 ca1
r
57.6 deg
OverlapTest if bolt.sector alpha "Overlap of Failure Cones" "No Overlap of Failure Cones"
OverlapTest "No Overlap of Failure Cones"
chord 2 r sinbolt.sector
2
chord 27 in UF Report Fig 3-7
AVco 4.5 ca12 AVco 337.9 in2 projected concrete failure area (single anchor)
ACI Eqn D-23
AVc chord 1.5 ca1 AVc 350.9 in2 projected concrete failure area (group)
ACI D.6.2.1
AVc if AVc AVco AVco AVc AVc 337.9 in2
ecV 1.0 eccentric load modifier ACI D.6.2.5
edV 1.0 edge effect modifier ACI D.6.2.6
cV 1.4 cracked section modifier ACI D.6.2.7 (stirrup spacing <= 4")
hV 1.0 member thickness modifier ACI D.6.2.8
breakout 0.75 strength reduction factor ACI D.4.4.c.i ( shear breakout, condition A)
Vcbg #AnchorRodsAVc
AVco
ecV edV cV hV Vb Vcbg 377.6 kip concrete breakout strength - shear
ACI Eqn D-22 Shear force | to edge
Vcbg_parallel 2 Vcbg Vcbg_parallel 755.3 kip ACI D.6.2.1.c Shear force || to edge
Tn.breakout Vcbg_parallel rb Tn.breakout 944.1 kip ft concrete breakout strength - torsion
breakout Tn.breakout 708.1 kip ft
Tu 179.8 kip ft
11/2/2018 S-1 Clay Model.xmcd 85
BreakoutTest if breakout Tn.breakout Tu "OK" "No Good" BreakoutTest "OK"
OverlapDesign if bolt.sector alpha "Based on Overlap of Failure Cones" "Based on No Overlap of Failure Cones"
OverlapDesign "Based on No Overlap of Failure Cones"
maximum torsion (Mx & Mz not used)maximum overturning (My not used) maximum CSR
Mx.polebase
0.0
136.4
136.4
kip ftMy.polebase
179.8
0.0
179.8
kip ftMz.polebase
0.0
68.8
68.8
kip ft
Analyze Foundation
Summary - Soil Properties and Drilled Shaft Geometry0 - clay1 - sandSoilType 0 soil 7.73 deg csoil 1145 psf soil 57.67 pcf Offset 0 ft
Diametershaft 4.5 ft Lshaft 11 ft Lanchor.rod 48 in
#BarsProvided 15 dbar 1.41 in'BF'= Lembedment.rod 40 in
Foundation Performance Ratios
DCRatiofoundation 0.973 CheckReinfClearSpacing "OK" CheckShearTorsion "OK"
CheckLongReinfshr.tor "OK" CheckMaxSpacingTransvReinf "OK"
OverlapTest "No Overlap of Failure Cones" OverlapDesign "Based on No Overlap of Failure Cones"
BreakoutTest "OK"
Fatigue Analysis DataFile "A60S-P4SL-DS145.dat" WindSpeed 150 mph
Use the member cross section adjacent to the weld toe to compute the nominal stress range. LTS 11.9
FatigueCategory 2 SM V3 11.6Analyze Structure for Fatigue
Arm and Pole Welds
fgalloping.arm1 4.565 ksi CAFTfullpengroove.weld.arm1 7 ksi Checkgalloping.arm1 "OK"
11/2/2018 S-1 Clay Model.xmcd 86
fgalloping.arm2 0 ksi CAFTfullpengroove.weld.arm2 "NA" ksi Checkgalloping.arm2 "NA"
fgalloping.pole 1.812 ksi CAFTfullpengroove.weld.pole 4.5 ksi Checkgalloping.pole "OK"
fnwg.arm1 2.823 ksi Checknwg.arm1 "OK"
fnwg.arm2 0 ksi Checknwg.arm2 "NA"
fnwg.pole 2.286 ksi Checknwg.pole "OK"
A325 Connection Bolts
ft.g.bolt3.8
0.0
ksi CAFTconn.bolt 16 ksi Checkg.conn.bolt"OK"
"OK"
ft.nwg.bolt2.4
0.0
ksi Checknwg.conn.bolt"OK"
"OK"
Anchor Bolts
ft.g.rod 2.325 ksi CAFTanchor.rods 7 ksi Checkg.rod "OK"
ft.nwg.rod 2.933 ksi Checknwg.rod "OK"
Summary
zero out initial header row for signal/sign information
removezero a max( ) max 1 max 0=if
bi 1 ai
i 1 maxfor
b
Xsignal.arm1 removezero Xsignal.arm1 #Signalsarm1 Xsignal.arm2 removezero Xsignal.arm2 #Signalsarm2
Sectionssignal.arm1 removezero Sectionssignal.arm1 #Signalsarm1 Sectionssignal.arm2 removezero Sectionssignal.arm2 #Signalsarm2
Backplatesignal.arm1 removezero Backplatesignal.arm1 #Signalsarm1 Backplatesignal.arm2 removezero Backplatesignal.arm2 #Signals
Xpanel.arm1 removezero Xpanel.arm1 #Panelsarm1 Xpanel.arm2 removezero Xpanel.arm2 #Panelsarm2
Areapanel.arm1 removezero Areapanel.arm1 #Panelsarm1 Areapanel.arm2 removezero Areapanel.arm2 #Panelsarm2
Summary
Mast Arm Design and Analysis Summary DataFile "A60S-P4SL-DS145.dat" WindSpeed 150 mph
11/2/2018 S-1 Clay Model.xmcd 87
Subject "A60/S-P4/S/L-DS5.0/16/4.5" DesignedBy "FDOT" PoleLocation "Index 17743"
ProjectNo "Design Standard" CheckedBy "FDOT" Date "09/28/2016"
1st Mast Arm#Signalsarm1 3 #Panelsarm1 4
Xsignal.arm1
26
37
49
ft Sectionssignal.arm1
3
3
4
Backplatesignal.arm1
1
1
1
Xpanel.arm1
11
18
31
43
ft Areapanel.arm1
16
5
1.5
7.5
ft2
Ltotal.arm1 60 ft Lsplice.provided.arm1 24 in
'FA'= 'FB'= 'FC'=Larm1
34.5
27.5
ft Diametertip.arm16.135
10.185
in Diameterbase.arm110.965
14
in'FE'= 'FF'= 'FG'=
'FD'=twall.arm1
0.25
0.375
in'FH'= max arm1 12.9 in max CFIarm1 0.704
2nd Mast Arm#Signalsarm2 0 #Panelsarm2 1
Xsignal.arm2 0( ) ft Sectionssignal.arm2 0( ) Backplatesignal.arm2 0( )
Xpanel.arm2 0.1( ) ft Areapanel.arm2 0.1( ) ft2
Ltotal.arm2 0 ft Lsplice.provided.arm2 24 in'UF'= 0 deg (Angle Between Arms)
'SA'= 'SB'= 'SC'=Larm2
0
0
ft Diametertip.arm20
0
in Diameterbase.arm20
0
in'SE'= 'SF'= 'SG'=
'SD'=twall.arm2
0
0
in max arm2 0 in max CFIarm2 0'SH'=
11/2/2018 S-1 Clay Model.xmcd 88
Luminaire Arm and Connection DataFile "A60S-P4SL-DS145.dat"WindSpeed 150 mph
(use MC10x33.6 channel for connection)
'LA'= Yluminaire 0 ft 'LB'= Xluminaire 0 ft 'LC'= Diameterbase.lumarm 0 in
'LD'= twall.lumarm 0 in 'LE'= Slopelumarm 0 'LF'= rlumarm 0ft
'LG'= dbolt.lum 0 in 'LH'= tbaseplate.lum 0 in
'LJ'= wbase.lum inwbase.lum 'LK'= wchannel.lum 0 in
CFIbase.lumarmCFIbase.lumarm CheckBoltLumBoltCheckBoltLumBolt PRbaseplate.lum 0 PRconn.plate.lum 0
Upright
'UA'= Ypole 23 ft'UB'= Yarm.conn 20 ft 'UC'=
Diametertip.pole 18.8092 in'UD'= Diameterbase.pole 22 in
'UE'= twall.pole 0.375 in 'UF'= 0 deg
'UG'= Ylum.conn 0ftx.dl 0.61 in Slopex 0.31 deg
z.dl 0 in Slopez 0 deg B 1.02
max CFIpole 0.353
1st Arm/Upright Connection
#ConnBolts0 6 'HT'= hconn.plate 30 in 'FJ'= bconn.plate.pv036 in
'FK'= tbaseplate.arm03 in 'FL'= tvertical.plate0
0.75 in
'FN'= wvertical.plate00.25 in 'FO'= Offsetconn0
17.1146in
'FP'= dbolt.conn01.25 in 'FR'= tmin.bpl.LTS 2 in
PRt.baseplate.arm0
PRt.connplate.arm0
CFIt.vert.plate0
0.833
1
0.292
'FS'= Spacingbolts.conn012.5 in 'FT'= wconn.plate0
0.3125 in
2nd Arm/Upright Connection
#ConnBolts1 0 'HT'= hconn.plate 30 in 'SJ'= bconn.plate.pv10 in
'SK'= tbaseplate.arm10 in 'SL'= tvertical.plate1
0 in
'SN'= wvertical.plate10 in 'SO'= Offsetconn1
0 in
'SP'= dbolt.conn10 in 'SR'= tmin.bpl.LTS 2 in
'SS'= Spacingbolts.conn10 in 'ST'= wconn.plate1
0 in
PRt.baseplate.arm1
PRt.connplate.arm1
CFIt.vert.plate1
0
0
0
11/2/2018 S-1 Clay Model.xmcd 89
CheckBoltConnBolt"OK"
"OK"
Pole Baseplate DataFile "A60S-P4SL-DS145.dat"WindSpeed 150 mph
#AnchorRods 6 'BA'= Diameterbaseplate.pole 38 in 'BB'= tbaseplate.pole 2.5 in
'BC'= dbolt.pole 2 in 'BF'= Lembedment.rod 40 in
Diameterboltcircle.pole 30 in
CheckAnchor.Bolt.Capacity "OK" CheckAnchorAlter "OK" PRplate.pole 1
Foundation'DA'= Lshaft 11 ft 'DB'= Diametershaft 4.5 ft dbar 1.41 in Offset 0 ft
'RA'= rounddbar
0.125in
11 'RB'= #BarsProvided 15 Diameterrebar.circle 3.2783 ft
'RC'= NumSpacesv.bar 12 'RD'= sv2 8 in DCRatiofoundation 0.973
WRITEPRN to Line 1-2-3
Mast Arm Tip DeflectionCompare Mast Arm deflection of each arm to a proposed camber
Camberarm1 2 deg Camberarm2 2 deg
Larm1 Larm1 if Larm110 ft= 0 ft 2 ft
Larm2 Larm2 if Larm210 ft= 0 ft 2 ft
Deflectionarm1 Slopex Larm1 max arm1 Deflectionarm1 16.86 in
CamberArm1upward sin Camberarm1 Larm1 CamberArm1upward 25.13 in
Deflectionarm2 Slopez Larm2 sin( )( ) Slopex Larm2 cos( ) max arm2 Deflectionarm2 0 in
CamberArm2upward sin Camberarm2 Larm2 CamberArm2upward 0 in
11/2/2018 S-1 Clay Model.xmcd 90
Check Clearance Between Connection Plates (for Two Arm Structures only)
0 deg if 180 deg( ) 360 deg( )[ ]
Offsetconn017.115 in bconn.plate.pv0
36 in hconn.plate 30 in 0 deg
Offsetconn10 in bconn.plate.pv1
0 in
x1 Offsetconn0tconn.plate0
hconn.platesin Camberarm1
2 y1
bconn.plate.pv0
2x1 14.59 in y1 18 in
x2 Offsetconn1tconn.plate1
hconn.platesin Camberarm2
2
cos( )bconn.plate.pv1
2sin( )
y2 Offsetconn1tconn.plate1
hconn.platesin Camberarm2
2
sin( )bconn.plate.pv1
2cos( ) x2 0.52 iny2 0 in
Clearance x1 x22 y1 y2
2 Clearance if y2 y1 if x1 x2 Clearance 0 in Clearance Clearance 23.5 in
(if Clearance equals 0, then Connection Plates intersect and redesign is required.
Plan View - Connection Plate Clearance for Two Arm Connections
Coordinates for Drawings
20 15 10 5 0 5 10 15 20 25
20
15
10
5
5
10
15
20
25
Connection Plate 1Connection Plate 2Pole Section
Connection Plate Clearance Clearance 23.5 in
Diameterconn.pole 19.2292 in
tconn.plate02 in
bconn.plate.pv036 in
tvertical.plate00.75 in
Offsetconn017.1146 in
Gap0 7.5 in
tconn.plate10 in
bconn.plate.pv10 in
tvertical.plate10 in
Offsetconn10 in
Gap1 0 in
Plan View - Drilled Shaft, Base Plate, Anchor Bolts, & Reinforcing Steel
Diameterbase.pole 22 in
11/2/2018 S-1 Clay Model.xmcd 91
20 0 20
20
20
ShaftReinforcementBase PlateBase PlateAnchor Bolts
Dimensions in Inches
Dim
ensi
ons i
n In
ches
Diameterbaseplate.pole 38 in
Diametershaft 54 in
Diameterboltcircle.pole 30 in
Diameterrebar.circle 39.34 in
#AnchorRods 6
#BarsProvided 15
11/2/2018 S-1 Clay Model.xmcd 92
Elevation View - Drilled Shaft, Base Plate, Anchor Bolts, & Reinforcing Steel
33 22 11 0 11 22 3333
22
11
0
11
22
33
ShaftBase PlateReinf. BarAnchor BoltPole
Dimensions in Inches
Dim
ensi
ons i
n In
ches
Diameterbase.pole 22 in
Diameterbaseplate.pole 38 in
tbaseplate.pole 2.5 in
Diametershaft 4.5 ft
Diameterboltcircle.pole 30 in
Diameterrebar.circle 39.3 in
11/2/2018 S-1 Clay Model.xmcd 93
Structure No. 2, SR 492
Signal\Sign#10
Signal\Sign#9
Signal\Sign#8
Signal\Sign#7
Signal\Sign#6
Signal\Sign#5
Signal\Sign#4
Signal\Sign#3
Signal\Sign#2
Signal\Sign#1
Dist from Pole (ft.) 32 42 22 14 46 38 27
1 1 1 5 5 5 5 3 2 2
Sign Width (in.) 24 24 24 18 30 24 96 12 120 120Sign Height (in.) 36 36 36 12 36 30 24 18 24 24Area (SF) 0.0 0.0 0.0 1.5 7.5 5.0 16.0 12.3 9.8 9.8Mwl. (kip*ft) 0 0 0 3 21 7 15 38 25 18
50 Regular Heavy DutyRegular Heavy Duty 40 44
14 15 44 490.3125 0.3125215 244
178 185
Assumptions:
Resistance (Mr= Mn) (kip*ft)Total Moment (Mextreme)
10127
1.1*Sign/Signal Mdl (kip*ft)Sign/Signal Mwl (kip*ft)
Wall Thickness (in)
Arm 1 Loads1.1*Arm Mdl (kip*ft) One Arm Assembly
A50/S P3/S DS/12/4.5
Mast Arm Assembly Information
Arm Mwl (kip*ft)
Arm 1 Length (ft)Design Standard Index 17743
Dia. at Arm Base (in)
Arm 1 Length, Signal/Sign Location and Size
Mast Arm Assembly Designation
5Back Plates?
Signal Orientation
5
5
505101520253035404550556065707580
Arm Signal/Sign 10 Signal/Sign 9 Signal/Sign 8 Signal/Sign 7 Signal/Sign 6
Signal/Sign 5 Signal/Sign 4 Signal/Sign 3 Signal/Sign 2 Signal/Sign 1 Pole
Vertical
Horizontal
YesNo
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
1
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
33
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
Arm 1 Length
Wind Speed130 mph 150 mph
None
3 Head
4 Head
5 Head
Sign
Luminaire?
No
Yes
170 mph
) 32 42 22 14 46 38 27
H
5 He
4 H
5 H
4 H
5 H
4 H
5 H
4 H
5 H
4 H
5 H
4 H
5 H
4 H
5 H
He
He
4 H
5 H
Sign Width (in.) 24 24 24 18 30 24 96 12 120 120Sign Height (in.) 36 36 36 12 36 30 24 18 24 24Area (SF) 0.0 0.0 0.0 1.5 7.5 5.0 16.0 12.3 9.8 9.8Mwl.. (kip*ft) 0 0 0 3 21 7 15 38 25 18
50 Regular Heavy
Tube WindPressure(psf)
44.1Fy(ksi)
50
Sign/Sig.Wind
Pressure(psf)
67.0
wall thk(in)
base dia(in)
S(in3)
Z(in3)
Mdl
(kip*ft)Mwl 130 mph
(kip*ft)Mr= Mn
(kip*ft)wall thk(in)
base dia(in)
S(in3)
Z(in3)
Mdl
(kip*ft)Mwl 130mph
(kip*ft)Mr= Mn(kip*ft)
DSIndex #
ID Length Diameter Mn TnMu+
Pu*LshaftTu
CheckMom. &Min Dia.
CheckTorsion
CheckMu+
Pu*LshaftTu
CheckMom. &Min Dia.
CheckTorsion
Check
30 0.25 11 23 29 10 10 107 0.25 12 27 34 11 11 125 1 DS/20/5 20 5 1800 589 393.7 Okay Okay Okay 0.0 0 0 040 0.25 13 32 40 20 20 145 0.25 14 37 47 22 22 166 2 DS/18/5 18 5 1312 477 375.0 Okay Okay Okay 0.0 0 0 050 0.3125 14 46 58 36 33 215 0.3125 15 53 67 40 37 244 3 DS/16/5 16 5 922 377 356.2 Okay Okay Okay 0.0 0 0 060 0.375 15 63 79 56 48 300 0.375 16 72 91 62 53 340 4 DS/16/4.5 16 4.5 829 305 356.2 Okay Okay Okay 0.0 0 0 070 0.375 17 81 103 85 71 380 0.375 18 91 115 100 77 422 5 DS/14/5 14 5 617 289 337.5 Okay Okay Okay 0.0 0 0 078 0.375 18 91 115 110 90 422 0.375 20 113 143 130 106 512 6 DS/14/4.5 14 4.5 556 234 337.5 Okay Okay Okay 0.0 0 0 0
7 DS/12/4.5 12 4.5 350 172 318.8 Okay Okay Okay 0.0 0 0 08 DS/12/4 12 4 311 136 318.8 NoGood NoGood NoGood 0.0 0 0 0
Signal/Sign 10
Signal/Sign 9
Signal/Sign 8
Signal/Sign 7
Signal/Sign 6
Signal/Sign 5
Signal/Sign 4
Signal/Sign 3
Signal/Sign 2
Signal/Sign 1 Total
1 Arm DSIndex #
2 Arm DSIndex #
Arm 1Shear
Arm 1Moment
Arm 2Shear
Arm 2Moment
Sign/SigMwl
(kip*ft)0.0 0.0 0.0 3.2 21.1 7.4 15.0 37.8 24.8 17.6 127.0 4.5 7 0 dl att N/A 9.9 N/A 0.0
Sign/Sig1.1*Mdl(kip*ft)
0.0 0.0 0.0 0.2 1.4 0.5 1.0 3.3 2.1 1.5 9.9 7 0 dl arm N/A 39.6 N/A 0.0
Arm 1Mwl
(kip*ft)43.9 49.3
Reg Arm /HD Arm
7 0 wl pole 2.6 52.9 0.0 0.0
Arm 11.1*Mdl(kip*ft)
39.6 44.0Reg Arm /HD Arm
wl att 4.1 91.0 0.0 0.0
177.9 184.8 wl arm 2.6 56.6 0.0 0.0One Arm Two Arms Tor wl att N/A 127.0 N/A 0.049.5 Tor wl arm N/A 43.9 N/A 0.0
Signal/Sign 10
Signal/Sign 9
Signal/Sign 8
Signal/Sign 7
Signal/Sign 6
Signal/Sign 5
Signal/Sign 4
Signal/Sign 3
Signal/Sign 2
Signal/Sign 1 Total 200.5
Sign/SigMwl
(kip*ft)0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 206.6 0.0
Sign/Sig1.1*Mdl(kip*ft)
0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 170.9 0.0Arm 1Length
50Arm 2Length
0
Arm 2Mwl
(kip*ft)0.0 0.0 9.4 0.0 Pole ID P3
Arm 21.1*Mdl(kip*ft)
0.0 0.0Shaft2 ArmFactor
1.1used forOT &Torsion
0.0 0.0
A50 /S P3 /S DSP3/S DS/12/4.5
DS
Note: Poles are designed to have a smaller CFI than Arms
Drilled Shaft
Pole ID
A50/S P3/S DS/12/4.5Arm 1 Arm 2
Design Arm Designation Pole Designation Drilled ShaftUse Regular Arm
Torsion
Forces at Top of DS
ArmWithout Attachments: Dead Load Moment, Wind Load Moment and Moment Capacity at Base Connection
Total ArmLength (ft)
Regular
50 00.98
0.000.000.77
0.84Max Design CFI %
Est. Regular Arm CFIEst. HD Arm CFI
Arm Length(s)
Assembly ID
Required Drilled Shaft Index Number Required (see Table for size)
Load Case
Drilled Shaft Index req'd for Overturning including Min.Diamter
Arm 2 Attachments: Extreme Event Dead Load Moment, Wind Load Moment at Base Connection
Extreme Event Arm Moment (kip*ft)
2 Arm Assembly
Shear
Moment Total
Drilled Shaft Index req'd for Torsion
Drilled Shaft Controlling Load Case
Moment dl
Moment wl
A50/S
Heavy Duty
Min ShaftDiameter
Arm 1 Attachments: Extreme Event Dead Load Moment, Wind Load Moment at Base Connection
0.0170.9
Index 17743 Drilled Shaft Capacities 1 Arm Assembly Loads And Capacity Check 2 Arm Assembly Loads and Capacity Check
assume a 37.5' polewl with lum
Pole Base Shears & Moments
A50/S P3/S DS/12/4.5
Use Regular Arm1 Arm AssemblyDesign Arm Designation Pole Designation Drilled Shaft
Ensuresanchorbolts fitinsiderebarcage
N/A
125
166
244
340
422
512
107145
215
300
380
422
185178
0
100
200
300
400
500
600
25 35 45 55 65 75
Arm
Mom
ent
Arm Lengths (ft)
Arm Loads And ResistancesHD Arm 1 Resistance Reg Arm 1 Resistance HD Arm 1 Load Reg. Arm 1 Load
GEOTECHNICAL PARAMETERS for DRILLED SHAFT SIZING
Definitions:
= phi = soil friction angle [degrees]
= gamma = soil unit weight [pounds per cubic foot]
N = number of blows it takes to drive a standard sampler (1.42” ID & 2” OD) with 140 pound hammer dropped from 30-inches
C = soil cohesion shear strength [pounds per square foot]
0’ to 2’ ……….. = 29º = 43 PSF N =0 C = 0 PSF
2’ to 16’……….. = 0º = 63. PSF N =15 C= 1900 PSF
Pro-rate geotechnical parameters as follow:
average = (2/14) x 29º + (14-2)/14 x 0º = 4.14º
average = (2/14) 43 PSF + (14-2)/14 x 63 PSF = 60.14 PSF
N average = (2/14) x 0 BPF + (14-2)/14 x 15 BPF = 12.86 blows per foot
C average = (2/9) 0 PSF + (9-2)/9 x 1900 PSF = 1478 PSF
Note that 14 is used in the denominator for the calculation of average phi, gamma and “N” because the resulting shaft length is 14’ in the last iteration of the computations for the sand model. Note that 9 is used in the denominator for “C” because the resulting shaft length is 9’ in the last iteration of the computation for the clay model.
STRUCTURE NO. 2 SAND MODEL
=
=
=
=
=
=
=
=
=
=
⋅=
:=
:=
= ⋅=
=
=
=
⋅=
=
⋅=
..:=
, , + ⋅, , ⋅, , :=
,
, ← ,
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⋅:= +:=
, ⋅ +⋅ ⋅+ ⋅ ⋅:= ⋅ ⋅+( )⋅ ⋅:=
⋅ +( )⋅ +
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, +⋅ ⋅+ +( )⋅ ⋅ +( )+
⋅ +⋅ ⋅+⋅+:=
⋅:= ⋅:=
, ⋅+ ⋅ ⋅ , ⋅
, := +:= ⋅=
⋅:= ⋅=
⋅ ⋅ ⋅:= ⋅+ ⋅+( )⋅:=
⋅ ⋅ ⋅:=
⋅ + +( ):= =
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+
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:=
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− +:= ⋅⋅=
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−:= ⋅⋅=
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+ +
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+
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:= ⋅=
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+ +
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⋅ ⋅ ⋅:= ⋅⋅=
⋅ ⋅ ⋅:= ⋅⋅=
⋅ ⋅ ⋅:= ⋅⋅=
⋅ ⋅ ⋅:= ⋅⋅=
= ⋅⋅= =
⋅ > ⋅ ⋅ −⋅ ⋅⋅ −
⋅ ( )⋅ ⋅
, ⋅ ⋅,
− ⋅⋅=:=
> ⋅ −( )⋅ ⋅−
⋅ ( )⋅ ⋅
, ⋅ ⋅,
− ⋅⋅=:=
> ⋅ −( )⋅ ⋅−
⋅ ( )⋅ ⋅
, ⋅ ⋅,
− − ⋅⋅=:=
⋅ ⋅− > ⋅⋅ ⋅ − ⋅−⋅ ⋅
, ⋅ ⋅,
− ⋅⋅=:=
⋅− > ⋅⋅ − ⋅−( )⋅ ⋅
, ⋅ ⋅,
− − ⋅⋅=:=
⋅− > ⋅⋅ − ⋅−( )⋅ ⋅
, ⋅ ⋅,
− − ⋅⋅=:=
, , ( ):= ⋅⋅=
, , ( ):= ⋅⋅=
, , ( ):= − ⋅⋅=
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⋅
⋅ ⋅ ⋅:= ⋅⋅=
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=
+ ≤ , , := =
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⋅ ⋅=
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⋅< , , ( ):= ⋅=
, , ( ) ⋅=
, , ( ) ≤ , , ( ):= =
( ) ( )+⋅:=⋅⋅=
⋅− ⋅> ⋅−, ⋅,
:= ⋅=
⋅⋅
⋅ ⋅
⋅ ⋅ ⋅
+ ⋅+
:= ⋅=
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:= =
:= =
:=⋅( )⋅
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:= =
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+ ++
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:=
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:=
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−
⋅+ −
:= ⋅=
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:=
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≤ , , ( ):=
=
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= ⋅= ⋅=
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=
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:=
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, ←
− ←
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:=
, ( ):= , ( ):=
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, ( ):= , (:=
, ( ):= , ( ):=
, ( ):= , ( ):=
= ⋅=
= = =
= = =
= =
=
=
=
=
=
= ⋅=
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⋅= ( ) ⋅= ( ) =
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⋅= ( ) ⋅= ( ) =
= ⋅=
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= = = =
⋅= ⋅=⋅=
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=⋅= ⋅=
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( ) =
= ⋅= ⋅=
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⋅=⋅=
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= ⋅= ⋅=
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=
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= = =
= ⋅= =
⋅:= ⋅:=
⋅( ) ⋅, ⋅, −:= ⋅( ) ⋅, ⋅,
−:=
⋅ ( )+:= ⋅=
( )⋅:= ⋅=
⋅ ⋅ ⋅ ⋅+ ( )+:= ⋅=
( )⋅:= ⋅=
⋅= ⋅> ⋅ −, , :=
⋅= ⋅= ⋅= ⋅=
⋅= ⋅=
−( )
⋅−:= := ⋅= ⋅=
−( )
⋅−
⋅ ⋅+:=
−( )
⋅−
⋅ ⋅−:= − ⋅= ⋅=
−( ) −( )+:= ≤( ) >( ) , ⋅, , , := ⋅=
− − − −
−
−
−
−
⋅=
⋅=
⋅=
⋅=
⋅=
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−
−
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=
=
− − −−
−
−
⋅=
⋅=
⋅=
⋅=
⋅=
⋅=
STRUCTURE NO. 2 CLAY MODEL
=
=
=
=
=
=
=
=
=
=
⋅=
:=
:=
= ⋅=
=
=
=
⋅=
=
⋅=
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,
, ← ,
, ← ,
, , ←
−..∈
−..∈:=
−:=
+:= =
, , ( ):= := =
+:= =
, , ( ):= := =
+:= =
, , ( ):=
:= =
+:= =
, , ( ):= :=
=
⋅ ⋅, , ( ):=
+:= =
, , := := =
+:= =
( ) −..:= ( ) −..:=
, , , ≠( ) ,
≠( )⋅ , , ,
:=
, ( ):=:=
=
+:= =
( ) −..:= ( ) −..:=
, , , ≠( ) ,
≠( )⋅ , ,
, ,
:=
, ( ):=
:=
=
, , , , ( ), ( ) , ( ),
:=
..:=
, ⋅:=
, :=
( )
, , , ( ):=
= = = =
, , , , ( ), ( ) , ( ),
:=
:=
, , ( ):=
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, ⋅:=
, ⋅:=
⋅, , ( ):=
⋅, ,
:=
= = =
←
+
⋅←
←
, −( )←
, ⋅−←
+←
..∈
..∈
:=
≤ ⋅
:=
≤ ⋅, ,
:=
:= :=
←
←
, −( ) −←
,
−←
, −( ) +←
,
−←
, −( ) +←
, ←
, −( ) −←
, ←
, , ←
, , ←
←
≤ , , ( )..∈
:=
=
:=
:= :=
> ⋅, −, ( ):=
≥ , , ( ):=
≥ , , ( ):=
≥ , , ( ):=
≥ , , ( ):=
− − − − −
−
⋅:= := ⋅:=
:=
:= ⋅=
⋅−:= ⋅=
⋅ ⋅+ ⋅+:= ⋅=
,
⋅:= ⋅=
( ) ⋅( )+ ⋅, , :=
⋅=
⋅:=
⋅−( )⋅:= ⋅=
, ( ):= ⋅=
⋅> ⋅, ⋅, ( ):= ⋅=
> , , ( ) +:= ⋅=
⋅ ⋅, , ( ):= ⋅=
⋅− ⋅−:= ⋅=
−:= ⋅=
⋅ ⋅, ⋅− ⋅, ( ), ( ):= ⋅=
⋅−( )−−
:= ⋅=
⋅ ⋅, , ( ):= ⋅=
⋅ ⋅, −( )⋅−, :=
⋅=
−( )−:= ⋅=
⋅− ⋅, ( ):= ⋅=
+ −:= ⋅=
⋅ ⋅, , ( ):= ⋅=
−( )⋅−:= ⋅=
⋅ ⋅, ⋅−( )−
,
+:=
=
:= =
− +:= ⋅=
:= ⋅=
−( )⋅−:= ⋅=
⋅+ ⋅+:= ⋅=
⋅−:= ⋅=
⋅ ⋅, , ( ):= ⋅=
⋅ , , ( ):= ⋅=
⋅ ⋅, , ( ):= ⋅=
⋅ ⋅, , ( ):= ⋅=
⋅ , , ( ):= ⋅=
⋅ −( )⋅−, , :=
⋅=
, , ( ):= ⋅=
, , ( ):= ⋅=
, , ( ):= ⋅=
, , ( ):= =
, , ( ):= ⋅=
, , ( ):= ⋅=
, , ( ):= ⋅=
, , ( ):= ⋅=
⋅= ⋅=
≥ , , ( ):= =
=
=
⋅=
⋅=
⋅=
:=
⋅
⋅ ⋅ ⋅:= ⋅=
⋅
⋅ ⋅ ⋅:= ⋅=
⋅:=
⋅:= :=
, , ( ):= =
⋅:= ⋅:= ⋅:= :=
⋅:= ⋅:= ⋅:= :=
( ) ⋅, ( ), :=
( ) ⋅( ), ⋅( ),
:=
( ) ⋅, ( ), :=
( ) ⋅( ), ⋅( ),
:=
( ) ⋅( )⋅, ,
:=
( ) ⋅( )⋅, ,
:=
( ) ⋅, ( ), :=
( ) ⋅( ), ( ),
:=
⋅ ⋅+ ⋅( ) , +:=
⋅ ⋅+ +( )⋅ ⋅:=
⋅=
⋅=
⋅ ⋅+ +( )⋅ ⋅:=
⋅=
:= ..:=
⋅−:=
− ⋅<( ) ⋅, −, ⋅ :=
− ⋅<( ) ⋅, −, ⋅ :=
− ⋅<( ) , , ⋅ :=
− ⋅<( ) , , ⋅ :=
− ⋅<( ) ⋅, −, ⋅ :=
− ⋅<( ) , , ⋅ :=
⋅:= :=
( ) ⋅, ,
:= = = =
⋅:=
⋅=
⋅ ⋅ ⋅:=×
⋅=
⋅ ⋅ ⋅:=
⋅=
− ⋅<( ) ⋅, −, ⋅ :=
− ⋅<( ) ⋅, −, ⋅ :=
− ⋅<( ) , , ⋅ :=
− ⋅<( ) , , ⋅ :=
− ⋅<( ) ⋅, −, ⋅ :=
− ⋅<( ) , , ⋅ :=
:=
−⋅⋅−
⋅ ⋅≤ ⋅, ,
+
−⋅⋅−
⋅
:=
− ⋅<( ) , , :=
−:= −:=
⋅ ⋅:= ( )⋅ ⋅:= ⋅:=
⋅ ⋅≤
⋅ ⋅ < ⋅≤
⋅ ⋅ < ⋅≤
⋅ ⋅ < ⋅≤
⋅ ⋅ < ⋅≤
⋅ ⋅ < ⋅≤
⋅ ⋅ < ⋅≤
:=
( ):=
⋅=
( ):=
⋅=
− ⋅<( ) , , :=
− ⋅<( ) , , +
:=
:=
, , , , ( ):=
( ) ⋅= ( ) ⋅=
( )⋅ ⋅:=:=
( )⋅ ⋅:=
, ( ):=
, ( ):=
, ( ):=
, , ( ):= , , , ( ):=
− − − − −
−
−
−( )
⋅=
⋅>
, ,
:= =
⋅, ⋅ ⋅
⋅,
:=
⋅=
..:=
−+
⋅ ⋅
⋅:= ( ) ⋅=
+:= ( ) ⋅=
⋅=
−
⋅−
+
−+( )⋅
⋅
−:=
−( )⋅ =
:= =
:=
..:=−
+:= := :=
:=
, , , , ,
:=( ) =
, , , , ,
:=( ) =
⋅ ⋅ ⋅ ⋅:=
−( )⋅ =
:= =
:=
⋅ ⋅ ⋅ ⋅:=
−( )⋅ =
:= =
:=
= =
..:=
+ +( )⋅:= +(⋅:=
+ +:= + +:=
+ +:= + +:=
( ):= = ⋅⋅= =
⋅
⋅
⋅
⋅
( ) ( )+:=⋅⋅=
( ) ( )+:= ⋅=
= = = =
= =
⋅:= ⋅:=
, , , , , , , ( ):=
( ) ⋅⋅= ( ) ⋅=
= ⋅:= ( ) ⋅⋅= ( ) ⋅=
:= := := ⋅= :=
=
, , , ( ):=
, , , , , , ( ):= := , (:=
−:= , , ( ):=
, , , , , , , ( ):=
( ) = ( ) =
, , , , , ( ):=
, , , , , , ( ):=
( ) ⋅=
( ) ⋅=
⋅:= ( ) ⋅=
( ) ⋅==
=
⋅:= ( ) ⋅=
( ) ⋅=
:= ⋅= :=
= ⋅=
, ⋅, , , , ( ):=
⋅:= ( ) ⋅=
( ) ⋅=
, ⋅, , , , ( ):= ( ) ⋅= ⋅:=
( ) ⋅= ( ) ⋅⋅=
( ) ⋅⋅=
= ⋅:= ( ) ⋅= ( ) =
= ⋅:= ( ) ⋅⋅= ( ) =
( ) ⋅⋅= ( ) ⋅⋅=
( ) ⋅= ( ) ⋅=
( ) ⋅= ( ) ⋅=
( ) ⋅⋅= ( ) ⋅⋅=
:=
:=
( ) = ( ) −×=
, , , , ( ):=
( ):=
( ) = ( ) =
⋅:= := ⋅:=
:= , ,
:=
, −, , , := −× − −× − −× −×(=
⋅+ ⋅+ ⋅+:=
:=
− − − − −− −×
−×
−×
−×
−×
−
⋅+ ⋅+ ⋅+ ⋅ ⋅ ⋅ ⋅+ ⋅ ⋅+ ⋅+
⋅ ⋅ ⋅ ⋅+ ⋅ ⋅+ ⋅ ⋅+
:=
⋅:= ( ) ⋅=
− − − − −−
−
−
−( )
−
⋅⋅=
⋅=
⋅⋅=
⋅=
=
⋅=
⋅=
⋅=
− − − − −
−
⋅= =
⋅=
⋅=
=
⋅=
= = = =
( ) = ( ) ⋅= ⋅ −( )⋅ ⋅=
= ⋅=
=
=
=
⋅=
⋅=
⋅=
− − −
−
⋅= =
⋅=
⋅=
=
⋅=
= = = =
( ) = ( ) ⋅= ⋅ −( )⋅ − ⋅=
= ⋅=
=
⋅=
⋅=
⋅=
=
⋅=
⋅=
⋅=
= ⋅= ⋅= ⋅=
= ⋅= ⋅= ⋅=
⋅= ⋅=
= = = =
= ⋅=
=
=
⋅=
⋅=
⋅=
+:= =
:= =
+:= =
:= =
+:= =
, , ( ):= := =
+:= =
, , ( ):= := =
+:= =
, , ( ):= := =
+:= =
, , ( ):= := =
+:= =
, , := :=
=
⋅ ⋅, , ( ):=
+:= = := =
⋅= ⋅= :=
⋅−( )⋅−:= ⋅=
−( )⋅+:= ⋅=
⋅= ..:=
⋅:=
⋅= ⋅= := ..:=
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Signal\Sign#10
Signal\Sign#9
Signal\Sign#8
Signal\Sign#7
Signal\Sign#6
Signal\Sign#5
Signal\Sign#4
Signal\Sign#3
Signal\Sign#2
Signal\Sign#1
Dist from Pole (ft.) 0 37 48 22 14 54 42 30
1 1 1 5 5 5 5 3 2 2
Sign Width (in.) 24 24 12 24 30 24 96 12 120 120Sign Height (in.) 36 36 18 18 36 30 24 18 24 24Area (SF) 0.0 0.0 0.0 3.0 7.5 5.0 16.0 12.3 9.8 9.8Mwl. (kip*ft) 0 0 0 7 24 7 15 44 27 20
60 Regular Heavy DutyRegular Heavy Duty 62 68
15 16 64 710.3750 0.3750300 340
222 231
Assumptions:
Resistance (Mr= Mn) (kip*ft)Total Moment (Mextreme)
11145
1.1*Sign/Signal Mdl (kip*ft)Sign/Signal Mwl (kip*ft)
Wall Thickness (in)
Arm 1 Loads1.1*Arm Mdl (kip*ft) Two Arm Assembly
A60/D A60/D P5/D DS/16/4.5
Mast Arm Assembly Information
Arm Mwl (kip*ft)
Arm 1 Length (ft)Design Standard Index 17743
Dia. at Arm Base (in)
Arm 1 Length, Signal/Sign Location and Size
Mast Arm Assembly Designation
5Back Plates?
Signal Orientation
5
5
505101520253035404550556065707580
Arm Signal/Sign 10 Signal/Sign 9 Signal/Sign 8 Signal/Sign 7 Signal/Sign 6
Signal/Sign 5 Signal/Sign 4 Signal/Sign 3 Signal/Sign 2 Signal/Sign 1 Pole
Vertical
Horizontal
YesNo
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
1
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
33
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
Arm 1 Length
Wind Speed130 mph 150 mph
None
3 Head
4 Head
5 Head
Sign
Luminaire?
No
Yes
170 mph
Mast Arm Assembly Information Arm 1 Length, Signal/Sign Location and SizeSignal\Sign Signal\Sign Signal\Sign Signal\Sign Signal\Sign Signal\Sign Signal\Sign Signal\Sign Signal\Sign
#10 #9 #8 #7 #6 #5 #4 #3 #2 #1Dist from Pole (ft.) 0 37 48 22 14 54 42 30
Si l O i t tiSignal Orientationn
H
5 He
4 H
5 H
4 H
5 H
4 H
5 H
4 H
5 H
4 H
5 H
4 H
5 H
4 H
5 H
He
He
4 H
5 HB k Pl t ?Back Plates?
Sign Width (in.) 24 24 12 24 30 24 96 12 120 120Sign Height (in.) 36 36 18 18 36 30 24 18 24 24Area (SF) 0.0 0.0 0.0 3.0 7.5 5.0 16.0 12.3 9.8 9.8Mwl.. (kip*ft) 0 0 0 7 24 7 15 44 27 20
5
800 75 70 655 600 5555 500 454 4040 35 300 25 200 1515 10010 55 000 5555
5Arm Signal/Sign 10 Signal/Sign 9 Signal/Sign 8 Signal/
Arm 1 Length (ft) Arm 1 Loads Mast Arm Assembly Designation60 Regular Heavy DutyDesign Standard Index 17743 1.1*Arm Mdl (kip*ft)Regular Heavy Duty 62 68 Two Arm Assembly
Dia. at Arm Base (in) A Mwl (kip*ft)15 16 64 71 A60/D A60/D P5/D DS/16/4.5Wall Thickness (in) 0.3750 0.3750 1.1*Sign/Signal Mdl (kip*ft) 11
Resistance ((Mr== Mn)) (kip*ft) Sign/Signal Mwl (kip*ft)300 340 145Total Moment ((Mextreme) 222 231
Assumptions:
Structure No. 3 SR 492
Signal\Sign#10
Signal\Sign#9
Signal\Sign#8
Signal\Sign#7
Signal\Sign#6
Signal\Sign#5
Signal\Sign#4
Signal\Sign#3
Signal\Sign#2
Signal\Sign#1
Dist from Pole (ft.) 46 55 38 12 51 42 34
Wind Speed =150 mph
Luminaire = No1 1 1 5 5 5 5 2 2 3
Sign Width (in.) 24 24 24 12 24 30 96 12 120 120Sign Height (in.) 36 36 36 18 30 36 24 18 24 24Area (SF) 0.0 0.0 0.0 1.5 5.0 7.5 16.0 9.8 9.8 12.3Mwl. (kip*ft) 0 0 0 5 18 19 13 33 27 28
60 Regular Heavy DutyRegular Heavy Duty 62 68
15 16 64 710.3750 0.3750300 340
220 229
Assumptions:
Mast Arm Assembly Information
Resistance (Mr= Mn) (kip*ft) Sign/Signal Mwl (kip*ft) 144
Design Standard Index 17743 1.1*Arm Mdl (kip*ft)
Arm 2 Length, Signal/Sign Location and Size
Vertical SignalOrientation with
Backplates.
Arm 2 Length (ft) Arm 2 Loads Mast Arm Assembly DesignationTwo Arm Assembly
A60/D A60/D P5/D DS/16/4.5
Total Moment (Mextreme)
Dia. at Arm Base (in) Arm Mwl (kip*ft)Wall Thickness (in) 1.1*Sign/Signal Mdl (kip*ft) 12
5
5
5
505101520253035404550556065707580
Arm Signal/Sign 10 Signal/Sign 9 Signal/Sign 8 Signal/Sign 7 Signal/Sign 6
Signal/Sign 5 Signal/Sign 4 Signal/Sign 3 Signal/Sign 2 Signal/Sign 1 Pole
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
1
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
22
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
None
3 Head
4 Head
5 Head
Sign
Arm 2 LengthNone
3 Head
4 Head
5 Head
Sign
Mast Arm Assembly Information Arm 2 Length, Signal/Sign Location and SizeSignal\Sign Signal\Sign Signal\Sign Signal\Sign Signal\Sign Signal\Sign Signal\Sign Signal\Sign Signal\Sign
0 #9 #8 #7 #6 #5 #4 #3 #2 #1Dist from Pole (ft.) 46 55 38 12 51 42 34
Wind Speed =150 mph
He
He
4 He
5 H
4 H
5 H
4 H
5 H
4 H
5 H
H
5 He
4 H
5 H
4 H
5 H
He
H
H
5 HeLuminaire = No
Sign Width (in.) 24 24 24 12 24 30 96 12 120 120Vertical SignalSign Height (in.) 36 36 36 18 30 36 24 18 24 24SOrientationOrientation withwithArea (SF) 0.0 0.0 0.0 1.5 5.0 7.5 16.0 9.8 9.8 12.3Backplates.Mwl.. (kip*ft) 0 0 0 5 18 19 13 33 27 28
5
8080 755 700 655 600 55555 5050 4544 4040 3535 300
5
Arm 2 Length (ft) Mast Arm60 Arm 2 Loads Assembly DesignationRegular Heavy DutyDesign Standard Index 17743 Regular Heavy Duty 1.1*Arm Mdl (kip*ft) 62 68 Two Arm Assembly
Dia. at Arm Base (in) A Mwl (kip*ft)15 16 64 71 A60/D A60/D P5/D DS/16/4.5Wall Thickness (in) 0.3750 0.3750 1.1*Sign/Signal Mdl (kip*ft) 12
Resistance ((Mr== Mn)) (kip*ft) Sign/Signal Mwl (kip*ft)300 340 144Total Moment ((Mextreme) 220 229
Assumptions:
Tube WindPressure(psf)
44.1Fy(ksi)
50
Sign/Sig.Wind
Pressure(psf)
67.0
wall thk(in)
base dia(in)
S(in3)
Z(in3)
Mdl
(kip*ft)Mwl 130 mph
(kip*ft)Mr= Mn
(kip*ft)wall thk(in)
base dia(in)
S(in3)
Z(in3)
Mdl
(kip*ft)Mwl 130mph
(kip*ft)Mr= Mn(kip*ft)
DSIndex #
ID Length Diameter Mn TnMu+
Pu*LshaftTu
CheckMom. &Min Dia.
CheckTorsion
CheckMu+
Pu*LshaftTu
CheckMom. &Min Dia.
CheckTorsion
Check
30 0.25 11 23 29 10 10 107 0.25 12 27 34 11 11 125 1 DS/20/5 20 5 1800 589 430.4 Okay Okay Okay 602.5 Okay Okay Okay40 0.25 13 32 40 20 20 145 0.25 14 37 47 22 22 166 2 DS/18/5 18 5 1312 477 410.2 Okay Okay Okay 574.3 Okay Okay Okay50 0.3125 14 46 58 36 33 215 0.3125 15 53 67 40 37 244 3 DS/16/5 16 5 922 377 390.0 Okay Okay Okay 546.0 Okay Okay Okay60 0.375 15 63 79 56 48 300 0.375 16 72 91 62 53 340 4 DS/16/4.5 16 4.5 829 305 390.0 NoGood Okay NoGood 546.0 NoGood Okay NoGood70 0.375 17 81 103 85 71 380 0.375 18 91 115 100 77 422 5 DS/14/5 14 5 617 289 369.8 Okay Okay Okay 517.8 Okay Okay Okay78 0.375 18 91 115 110 90 422 0.375 20 113 143 130 106 512 6 DS/14/4.5 14 4.5 556 234 369.8 NoGood Okay NoGood 517.8 NoGood NoGood NoGood
7 DS/12/4.5 12 4.5 350 172 349.7 NoGood NoGood NoGood 489.5 NoGood NoGood NoGood8 DS/12/4 12 4 311 136 349.7 NoGood NoGood NoGood 489.5 NoGood NoGood NoGood
Signal/Sign 10
Signal/Sign 9
Signal/Sign 8
Signal/Sign 7
Signal/Sign 6
Signal/Sign 5
Signal/Sign 4
Signal/Sign 3
Signal/Sign 2
Signal/Sign 1 Total
1 Arm DSIndex #
2 Arm DSIndex #
Arm 1Shear
Arm 1Moment
Arm 2Shear
Arm 2Moment
Sign/SigMwl
(kip*ft)0.0 0.0 0.0 3.7 24.1 7.4 15.0 44.4 27.4 19.6 141.6 5 5 5 dl att N/A 11.1 N/A 11.0
Sign/Sig1.1*Mdl(kip*ft)
0.0 0.0 0.0 0.2 1.6 0.5 1.0 3.9 2.3 1.7 11.1 6 5 dl arm N/A 61.6 N/A 61.6
Arm 1Mwl
(kip*ft)63.9 70.6
Reg Arm /HD Arm
5 5 wl pole 2.6 52.9 2.6 52.9
Arm 11.1*Mdl(kip*ft)
61.6 68.2Reg Arm /HD Arm
wl att 4.1 91.0 4.0 88.8
218.0 227.0 wl arm 3.3 72.8 3.3 72.8One Arm Two Arms Tor wl att N/A 141.6 N/A 139.172.7 Tor wl arm N/A 63.9 N/A 63.9
Signal/Sign 10
Signal/Sign 9
Signal/Sign 8
Signal/Sign 7
Signal/Sign 6
Signal/Sign 5
Signal/Sign 4
Signal/Sign 3
Signal/Sign 2
Signal/Sign 1 Total 216.7
Sign/SigMwl
(kip*ft)0.0 0.0 0.0 0.0 18.4 19.1 12.9 33.3 27.4 28.0 139.1 228.6 320.0
Sign/Sig1.1*Mdl(kip*ft)
0.0 0.0 0.0 0.0 1.8 0.8 0.8 2.8 2.3 2.4 11.0 205.5 287.7Arm 1Length
60Arm 2Length
60
Arm 2Mwl
(kip*ft)63.9 70.6 10.1 14.1 Pole ID P5
Arm 21.1*Mdl(kip*ft)
61.6 68.2Shaft2 ArmFactor
1.4used forOT &Torsion
215.6 224.6
A60 /S P5 /S DSP5/S DS/14/5
A60 /D P5 /D DSP5/D DS/14/5
Note: Poles are designed to have a smaller CFI than Arms
Drilled Shaft
Pole ID
A60/D A60/D P5/D DS/14/5Arm 1 Arm 2
A60/D
Design Arm Designation Pole Designation Drilled ShaftUse Regular Arm
Torsion
Forces at Top of DS
ArmWithout Attachments: Dead Load Moment, Wind Load Moment and Moment Capacity at Base Connection
Total ArmLength (ft)
Regular
60 600.98
0.730.670.68
0.74Max Design CFI %
Est. Regular Arm CFIEst. HD Arm CFI
Arm Length(s)
Assembly ID
Required Drilled Shaft Index Number Required (see Table for size)
Load Case
Drilled Shaft Index req'd for Overturning including Min.Diamter
Arm 2 Attachments: Extreme Event Dead Load Moment, Wind Load Moment at Base Connection
Extreme Event Arm Moment (kip*ft)
2 Arm Assembly
A60/D A60/D P5/D DS/14/5
Shear
Moment Total
Drilled Shaft Index req'd for Torsion
Drilled Shaft Controlling Load Case
Moment dl
Moment wl
A60/S
Heavy Duty
Min ShaftDiameter
Arm 1 Attachments: Extreme Event Dead Load Moment, Wind Load Moment at Base Connection
287.7205.5
Index 17743 Drilled Shaft Capacities 1 Arm Assembly Loads And Capacity Check 2 Arm Assembly Loads and Capacity Check
assume a 37.5' polewl with lum
Pole Base Shears & Moments
A60/S P5/S DS/14/5
Use Regular Arm1 Arm AssemblyDesign Arm Designation Pole Designation Drilled Shaft
Ensuresanchorbolts fitinsiderebarcage
N/A
125
166
244
340
422
512
107145
215
300
380
422
227218
0
100
200
300
400
500
600
25 35 45 55 65 75
Arm
Mom
ent
Arm Lengths (ft)
Arm Loads And ResistancesHD Arm 1 Resistance Reg Arm 1 Resistance HD Arm 1 Load Reg. Arm 1 Load
GEOTECHNICAL PARAMETERS for DRILLED SHAFT SIZING
Definitions:
= phi = soil friction angle [degrees]
= gamma = soil unit weight [pounds per cubic foot]
N = number of blows it takes to drive a standard sampler (1.42” ID & 2” OD) one foot with 140 pound hammer dropped from 30-inches
C = soil cohesion shear strength [pounds per square foot]
0’ to 8’ ……….. = 26º = 38 PSF N =1.5 C = 0 PSF
8’ to 23’……….. = 0º = 58. PSF N =7 C= 1150 PSF
23’ to 27’……….. = 0º = 73. PSF N =37 C= 8000 PSF
Pro-rate geotechnical parameters as follow:
average = (8/24) 29º + (24-8)/24 x 0º = 9.67 º
average = (8/24) 38 PSF + (23-8)/24 x 58+ (24-23)/24 x 73 PSF = 51.95 PSF
N average = (8/24) x 1.5 BPF+(23-8)/24 x 7 +(24-23)/24 x 37BPF= 6.42 blows/ft.
C average = (8/23) 0 PSF + (23-8)/23 x 1150 PSF = 750 PSF
Note that 24 is used in the denominator for the calculation of average phi, gamma and “N” because the resulting shaft length is 24’ in the last iteration of the computations for the sand model. Note that 23 is used in the denominator for “C” because the resulting shaft length is 23’ in the last iteration of the computation for the clay model.
STRUCTURE NO. 3 SAND MODEL
The new custom file will be a copy of the last file called fromthe program. A ".dat" extension will be added to the file name.Custom File Name (optional)
Add file to file list
Select Data File (required) All data files are in the same directory as the MastArm.xmcd fi
ReferenceThis program works in conjunction with Mastarm Design Standards 17743 and 17745.
References: AASHTO LRFD Specifications for Signs, Luminaires and Traffic Signals, 1st Edition (LRFDLTS).FDOT Structures Manual Vol. 3 (SM V3).
For more information see Reference.xmcd and Changes.xmcd.
Use Control+F9 torecalculate the worksheet,once to write out data, twiceto read in data
mph SM V3 3.8.2
use X to zero out datause 0 to keep current values " Yes" or " No"
use X to zero out datause 0 to keep current values
feet, 40 ft. max. for 1 piece arms
inches, measured flat to flat (FG)
feet, splice distance, for 2 piece arms,length of piece closest to pole,use X to zero out (FE)
set = for NO SPLICE
inches, this value is used for one piece arms (FD)
inches, for 2 piece arms, wall thickness of piece closest to the pole,
use X to zero out (FH)
*Note: for two piece arms (2nd length value greater than 0*ft), the first ArmLength value is entered as the actual length minus a 2 fosplice length. The 2 foot length is added to ArmLength0 at the end of the file. See drawing in reference file for more details.
Note: To model a damping device the weight is approximately the same as a 3 section signal (58 pounds) and the effective areafor wind loading is 2.1 square feet or less than half that of a 3 section signal at around 4.8 square feet
0 = user defined1 = custom design
Custom Design splice length
initial estimate of the tip diameter of the arm extension
base diameter of the arm rounded to the nearest inch
minimum and AASHTO splice length
tip diameter of arm extension
length of arm extension
User Defined splice length
Splice Length Check LTS 5.14.9
(min TipDiameter = 4.7 in. for 7 gage and 7 in. for 3 gage, see reference file)
gust factor LTS 3.8
SM V3 3.8
(min. 16 ft.)
constants that vary with exposure condition(values shown are for Exposure C):
height factor
segments n=1..50 segment 1 segment 2 segment 3 segment 4 segment5 .. segment 50
sections n=0..50 0 1 2 3 4 5 .. 49 50
(coeff drag)
Internally illuminated sign weightsvary from 5-9psf.
(coeff drag)
1. Section Properties (assume a 12 sided section) LTS Appendix Table B.1-1
inside bend radius of arm tube wall plate:
inside bend radius of arm tube wall plate:
effective width determination for use in classification of steel sectionsfor local buckling [LTS-1, Eq. C5.7.2-1]:
shape factor, Kp =Z/S:
[LTS-1, Table B.1-1] Elastic section modulus:
plastic section modulus:
ratio - inside-corner radius to wall thickness:
[see LTS-1 Eq. B.2-1]
stress concentration factor for multi-sided shapes: torsional constant:
[LTS-1, Eq. B.2-1]
2. Bare Arm DL Moment and Shear (divide arm into twenty segments, twenty one sections)
3. Bare Arm WL Moment and Shear (assume a min. ratio of break radius to tube radius of 0.25)
(Divide arm into 20 segments and use the average diameter to calculate the wind loading)
(velocity conversion factor) LTS Table 3.8.3-3
LTS Table 3.8.7-1
[LTS-1, 5.5.3.2]
flexure (bending): shear: torsion: axial compression:
tension, netsection fracture:
tension, grosssection yielding:
[LTS-1, 5.8]
no. of sides providedfor multi-sided pole:
steel modulus ofelasticity:
nominal bending strength for multi-sided tubes shall not exceed nominal bending strength for round tubes of equivalent diam
[LTS-1, 5.8.2]
flexure (bending): factored flexural resistance:
[LTS-1, 5.8]
[LTS-1, 5.10]
Note: HMLTs generally only experience pure axial comp., not pure axial tension; therefore, LTS-1, 5.9 is intentionally omitte
pole (column) totalunbraced length:
radius of gyration(per section):
steel modulus ofelasticity:effective length factor: gross section area:
[LTS-1, C5.10.2.1]
Euler stress:
critical buckling stress, used in determination ofnominal compressive strength:
buckling stress, used in determinationof for with : element effective wid
[LTS-1, Eq. 5.10.2.3-
effective pole tube wallmid-thickness radius: effective area:
local buckling adjustment factor:
section classification: [LTS-1, Tables 5.7.2-1 & Table 5.8.2-1]
torsional buckling: [LTS-1, 5.10.2.5]
Because torsional column buckling is not a common problem with sign andluminaire and signal support members, strength equations are not includedhere. If torsional buckling is of concern, design equations of AISC 14thEdition should be applied.
recalculate based on the refined value for :
critical buckling stress:
nominal compressive strength:
axial compression:
factored compressive resistance:
[LTS-1, Eq. 5.10.1-1]
[LTS-1, 5.11]
distance from max.to zero shear force:
outside distance fromflat side to flat side:
shear area:
:tip
:base
nominal shear stress capacity:
[LTS-1, 5.11.2.1.1 & 5.11.2.1.2]
nominal direct shear strength [LTS-1, 5.11.2]:
nominal torsion stress capacity: torsional constant: nominal torsional strength [LTS-1, 5.11.3]:
[LTS-1, 5.11.3.1.1 & 5.11.3.1.2]
shear: factored direct shear resistance:
[LTS-1, Eq. 5.11.1-1]
torsion: factored torsional shear resistance:
[LTS-1, Eq. 5.11.1-2]
factored flexural resistance:
factored compressive resistance:
factored direct shear resistance:
factored torsional shear resistance:
[LTS-1, 5.12.1]
moment capacity ratio: shear capacity ratio: torsion capacity ratio:
combined force interaction equation:
degree of polynomial tofit
number of data points
polynomialcoefficients
polynomial function
note: origin is the base of the arm
now integrate the curvature function twice to get deflections. Note: assuming pole connection to the foundation is rigid, theconstants of integration are zero for both slope and deflection
evaluates to
use X to zero out datause 0 to keep current values "yes" or "no"
use X to zero outuse 0 to keep current values
feet, 40 ft. max. for 1 piece arms, use X to zero out set = for NO ARM2
inches, measured flat to flat, use X to zero out (SG)
feet, splice distance, for 2 piece arms,length of piece closest to pole,use X to zero out (SE)
set = for NO SPLICE
inches, use X to zero out (SD)
inches, for 2 piece arms, wall thickness of piece closest to the pole,
use X to zero out (SH)
See Design Standards 17743 and 17745 for input values.
set = for NO LUMINAIRE
feet, use X to zero out (Standard LA = 40 feet)
feet, use X to zero out (Standard LB = 10 feet)
inches, use X to zero out (Standard LC = 3 inches)
inches, use X to zero out (Standard LD = 0.125 inches)
rise/run, use X to zero out (Standard LE = 0.5)
feet, use X to zero out (Standard LF = 8 feet)
inches, use X to zero out (Standard LG = 0.5 inches)
inches, use X to zero out (Standard LH = 0.75 inches)
feet (UA) Common wall thicknesses:0.1793 in.0.2391 in.0.25 in.0.313 in.0.375 in.0.5 in.
feet (UB)
inches, measured flat to flat (UD)
inches (UE)
inches, clear distance between connection plate and upright
inches, use X to zero out
Design Criteria: CFI (Combined Force Interation) must be less than 1
(shape factor)
(measured from face of upright to Arm BasePlate, same value is used in the ConnectionFile, a suggested minimum value for two armuprights is 5 1/2 inches to allow forfabrication and erection)
Angle between arms, a 360 degrees (this variable is ignored for single arm structures)
(Mast Arm Loads + Luminaire Loads)For analysis purposes, place the arm with the greater DL Moment as Arm1 on the X axis, and then place Arm2 on an angle a up to360 degrees. When including a Luminaire, add forces to Arm1 (conservative).
arm 1 forces
(Mast Arm only)
(Mast Arm only)
(from Luminaire only) (from Luminaire only
arm 2 forces
Axial Loadon pole
Arm deadand windloads onpole
Total PoleMoments
Wind Load Case 1wind on arm 1 only, wind direction equals 90 or 270 degrees. Note b 0 for one arm uprights
Wind Load Case 2 - calculate the torsion and shear for two arm uprights. Set wind Direction from the X Direction, b androtate the wind in increments of 5 degrees up to 360 degrees.
Wind Direction for Maximum Torsion on Upright
Wind Direction for Maximum Shear on Upright
summary of load case 2 torsion and shears in the x and z directions
Divide pole from the centerline of both arms to base into 10 segments and check each section for capacity
section properties (assume a 12 sided section)
LTS Appendix Table B.1-1
inside bend radius of tube wall plate:
inside bend radius of tube wall plate:
effective width determination for use in classification of steel sectionsfor local buckling [LTS-1, Eq. C5.7.2-1]:
shape factor, Kp =Z/S:
[LTS-1, Table B.1-1] Elastic section modulus:
plastic section modulus:
ratio - inside-corner radius to wall thickness:
[see LTS-1 Eq. B.2-1]
stress concentration factor for multi-sided shapes: torsional constant:
[LTS-1, Eq. B.2-1]
weight per segment
Height Coefficient (Kz) LTS Eqn C 3.8.4-1
height factor
Wind Load and Moments and Shears (assume a min. ratio of break radius to tube radius of 0.25)
(Divide arm into ten segments and use the average diameter to calculate the wind loading)
LTS Table 3.8.3-3
LTS Table 3.8.6-1
for one arm poles, the controlling load case is wind acting perpendicular to the arm, thereforeuse 20% of the Basic Load as the transverse loading component for this loading case. LTS 3.9.3
wind direction for maximum torsion wind direction for maximum overturning
[LTS-1, 5.5.3.2]
flexure (bending): shear: torsion: axial compression:
tension, netsection fracture:
tension, grosssection yielding:
[LTS-1, 5.8]
no. of sides providedfor multi-sided pole:
steel modulus ofelasticity:
nominal bending strength for multi-sided tubes shall not exceed nominal bending strength for round tubes of equivalent diam
[LTS-1, 5.8.2]
flexure (bending): factored flexural resistance:
[LTS-1, 5.8]
[LTS-1, 5.10]
Note: HMLTs generally only experience pure axial comp., not pure axial tension; therefore, LTS-1, 5.9 is intentionally omitte
radius of gyration(per section):
steel modulus ofelasticity:effective length factor: gross section area:
[LTS-1, C5.10.2.1]
Euler stress:
critical buckling stress, used in determination ofnominal compressive strength:
buckling stress, used in determinationof for with : element effective wid
[LTS-1, Eq. 5.10.2.3-
effective pole tube wallmid-thickness radius: effective area:
local buckling adjustment factor:
section classification: [LTS-1, Tables 5.7.2-1 & Table 5.8.2-1]
torsional buckling: [LTS-1, 5.10.2.5]
Because torsional column buckling is not a common problem with sign andluminaire and signal support members, strength equations are not includedhere. If torsional buckling is of concern, design equations of AISC 14thEdition should be applied.
recalculate based on the refined value for :
critical buckling stress:
nominal compressive strength:
axial compression:
factored compressive resistance:
[LTS-1, Eq. 5.10.1-1]
[LTS-1, 5.11]
distance from max.to zero shear force:
shear area:
nominal shear stress capacity:
[LTS-1, 5.11.2.1.1 & 5.11.2.1.2]
nominal direct shear strength [LTS-1, 5.11.2]:
nominal torsion stress capacity: torsional constant: nominal torsional strength [LTS-1, 5.11.3]:
[LTS-1, 5.11.3.1.1 & 5.11.3.1.2]
shear: factored direct shear resistance:
[LTS-1, Eq. 5.11.1-1]
torsion: factored torsional shear resistance:
[LTS-1, Eq. 5.11.1-2]
factored flexural resistance:
factored compressive resistance:
factored direct shear resistance:
factored torsional shear resistance:
[LTS-1, 4.8.1]
pole (column)unbraced length:
pole moment of inertiaat base:
pole moment of inertiaat tip:slenderness factor:
[LTS-1, C4.8.1]
check validity for use of LTS-1 Eq. 4.8.1-1:
[LTS-1, 4.8.1]
factored vertical concentratedload at pole tip:
factored weight of pole:load factors Extreme I:
equivalent axial load for a non-prismaticcantilever with a concentrated load at the tip:
Euler buckling load based upon moment ofinertia at pole bottom:
moment magnification factor for second-order effects:
[LTS-1, Eq. 4.8.1-1]
[LTS-1, 5.12.1]
moment magnification factor, calculatedaccording to AASHTO Section 4.8.1:
axial capacity ratio: moment capacity ratio: shear capacity ratio: torsion capacity ratio:
combined force interaction equation:
to clarify the stresses distributions and load cases for two arm uprights, graph CSR if minimum values for one arm shearand one arm torsion are not used
(for 16 sided pole, conservative)
From the curvature results (M/EI) at each section, curve fit a fourth degree polynomial, then integrate twice to get deflections.To get a function for curvature (M/EI), set the y-axis as curvature and the x-axis as distance along the pole starting atthe base. So the constants of integration are zero, and are calculated with section zero being at the base.
degree of polynomialto fit:
number of data points: polynomial coefficients:
polynomial function:
now integrate the curvature function twice to get deflections. Note: assuming pole connection to the foundation is rigid, the constantsof integration are zero for both slope and deflection
evaluates to:
lateral deflection atpole tip:
deflection as a percent of total pole height: lateral deflectionat pole tip:
[LTS-1, 10.4.2.1]
graph the calculated deflected shape:
inches, for two arm Mast Arms both connection plateheights must be equal (HT)
inches (FL)
inches, use X to zero out (SL)
inches (FP)
inches, use X to zero out (SP)
inches (FK)
inches, use X to zero out (SK)
inches (FJ)
inches, use X to zero out (SJ)
Trial Plate Thicknesses and Bolt Diameter
Design Criteria:performance ratio of bolt), (performance ratio of arm base plate),
& CS (combined stress ratio of vertical plate).
(for the base plate)
From Mast Arm Design
Note: Gap is the distance between the uprightand the Arm Base Plate. (5.5 inches is asuggested minimum for two arm poles)
From Upright Design(at arm connection)
(FO)
(SO)
Total Factored Moment and Shear
AISC LRFD, Vol 1, 6-A4 Specs, 2nd Ed.
Control dimensions
rounded up to the next 1/4 inch dimension
Minimum Mast Arm base plate height
Mast Arm base plate height, rounded up to next 1 inch dimension if necessary
Mast Arm base plate width
Mast Arm base plate width round up to next 1 inch dimension
(FJ)
(SJ)
Bolt spacing
(FS)
(SS)
Calculate Capacities of Connection Elements Based on the AISC LRFD Code, 2nd Edition
(Research Report 1126-4F by the Bureau of Engineering Research at the Univ. of Texas at Austin)(Design of bolts and plates based on "Design Guide for Steel to Concrete Connections by Cook, Doerr &Klingner)
Calculate Capacities of Connection Elements Based on the AISC LRFD Code, 13th Edition
Compute Shear Capacity of Back Truss Bolts (A325) [AISC J3]
Gross Bolt Area used forshear
Bending plane under full dead and wind load
Calculate the bolt moment arm
See Reference file for variable definitions
Shear perBolt
Bolt Shear Stress
Bolt Tensile Stress
AASHTO LTS minimum base plate thickness:
[LTS-1, Table 5.6.3-1] [SM 5.6.3-1]
See Reference file for formula derivations
(if PR <= 1.0 ok)
See Reference file for formula derivations
Round up to next quarter inch dimension.
(FR)
(SR)
round up to next1/8 inch dim.
NOTE: Old fillet welds, not used.
(Design welds of the socket joint to carry 100% of the design load using an E70 electrode.).
Weld Properties
Total Stress on Weld
Max. Bottom WeldSize
(FM)
(SM)
Bottom Weld Stress
AISC Table J2.5
Top Weld Stress
Top Weld Size
Round up tonext 1/16 inch
(FQ)
(SQ)
(Design welds to resist dead load moment , wind load moment, and dead load shear using an E70 electrode)
Weld Properties
Plate/Upright Weld size
AISC Table J2.5
min weld size
AISC Table J2.4
(FN)
(SN)
min weld size
AISC Table J2.4
min weld size
AISC p. 8-119
(FT)
(ST)
Trial Plate Thickness
Controlling Slenderness Parameter
Plastic Moment
Limiting Buckling Moment
Flexural Slenderness Parameters
AISC Table A-F1.1
For < <= Nominal Flex. Strength
AISC Eqn A-F1-3
For <Nominal Flex. Strength
AISC Eqn F1-14
Required Flexural Strength
Column Slenderness Parameter
AISC Eqn E2-4
Nominal Critical Stress
AISC Eqns E2-2 & E2-3
Nominal Compressive Strength
AISC Eqn E2-1
Required Compressive Strength
Combined Stress RatioFlexure and Tension members
AISC Eqns H1-1a & H1-1b (if CSR<1, then ok)
(if PR<1, then ok)
set variables equal to zero if there is no second arm
use 6 bolts minimum
inches (BC)
maximum torsion (Mx & Mz not used)maximum overturning (My not used) maximum CSR
load cases for maximum torsion (T), overturning (OT), and Combined Force Interation (CFI)
Design per AISC J3
Design plate thickness based on yield line theory
minimum base plate thickness
LTS 5.14.3SM V3 5.14.3
Round up to next1/8 inch dim.
final Diameter.tip.poleadjusted for t.baseplate.pole.
NOTE: Old fillet welds, not used.
(Design welds of the socket joint to carry 100% of the design load using an E70 electrode.).
AISC LRFD, Vol 1, 6-A4 Specs, 2nd Ed.
AISC Table J2.5
(BD)
(BE)
0 - clay 1 - sand
degrees, soil friction angle (sand)
psf, soil shear strength (clay)
pcf, soil density (typical design value = 45-50 pcf)
vertical distance between top offoundation and groundline
Number of blows per foot.If N< 5, contact the district geotech Engineer SM V3 13.6
(not used)
LRFD = AASHTO LRFD Bridge Design Specifications
SM V3 = FDOT Structures Manual Volume 3
SDG = FDOT Structures Design Guidelines
Spec = FDOT Standard Specifications
ACI = ACI 318 Structural Concrete Building Code
UF Report = FDOT/University of Florida Report BD545 RPWO #54
(From Arm1 Design)
(from Base Plate Design)
(from Upright Design)
round shaft diameter up to the nearest half foot dimension to accommodate available coring equipment
SM V3 13.6 vertical distance between top offoundation and groundline
short free-head pile in cohesionless soil using Broms method
Guess value
(round up to next foot)
short free-head pile in cohesive soil using Modified Broms method for L < 3b (see reference file forderivation)
Guess value
(round up to next foot)
short free-head pile in cohesive soil using Regular Broms method for L > 3b
(round up to next foot)
(If , use Modified Broms method)
NOTE: and are based upon CONCRETE and soilinteraction. This torsion methodology is not to be used withpermanent casing.
SM V3 13.6
Number of blows per foot. If N< 5, contact the district geotech Engineer
load transfer ratio
coefficient of friction between concrete shaft and soil
short free-head pile in cohesionless soil
Guess value
(round up to next foot)
short free-head pile in cohesive soil
Guess value
(round up to next foot)
short free-head pile in cohesionless soil using Broms method
short free-head pile in cohesive soil using Modified Broms method for L < 3b (see reference file forderivation)
Guess value
short free-head pile in cohesive soil using Regular Broms method for L > 3b
(If , use Modified Broms method)
(this is a Service moment)
Sand model controls
reinforcing yield strength
concrete strength Spec 346-3
cover SDG Table 1.4.2-1
longitudinal bar area
longitudinal bar diameter
stirrup area SM V3 13.6.2
stirrup diameter
stirrup spacing, depth = 0 ft-2 ft SM V3 13.6.2
stirrup spacing, depth = 2 ft-depth.stir
stirrup spacing, depth > depth.stir
stirrup spacing, depth > depth.stirA
stirrup depth, see s.v2 and s.v3 above
irrup depth, see s.v3 and s.v4 above
shaft diameter
LRFD 5.7.4.2
number of longitudinal bars
SDG 3.6.10
Shear Load Factor
Torsion Load Factor
Shear Resistance Factor LRFD 5.5.4.2.1
Torsion Resistance Factor LRFD 5.5.4.2.1
Area and perimeter of concrete cross-section
Diameter, perimeter and area enclosed by the centerline of the outermost closed transverse torsion reinforcement
LRFD C5.8.2.1
Effective shear depth
LRFD C5.8.2.1
Check Shear Strength
LRFD Eqn 5.8.3.3-3LRFD 5.8.3.4.1
ACI 11.3.3
LRFD Eqn 5.8.3.3-4
Check Torsion Strength
LRFD Eqn 5.8.3.6.2-1
LRFD 5.8.3.4.1
LRFD Eqn 5.8.2.1-4
LRFD Eqn 5.8.2.1-3
Check Maximum Spacing Transverse Reinforcement
LRFD Eqn 5.8.2.9-1
LRFD Eqn 5.8.2.7-1
LRFD Eqn 5.8.2.7-2
Check Longitudinal Reinforcement for Combined Shear and Torsion LRFD Eqn 5.8.3.6.3-1
LRFD 5.8.3.4.1
Use a maximum of three rebarper anchor bolt (conservative)
2015 AASHTO Development Length of Deformed Bars in Tension 5.11.2.1
= the smaller of the distance from center of bar or wire being developed to the nearest concretesurface and one half the center-to-center spacing of the bars or wires being developed
. assume no transverse bars:
LRFD Eqn 5.11.2.1.3-1
tension development length LRFD Eqn 5.11.2.1.1-2
Note: minimum embedment was in old AASHTO LTS, 2nd Ed. 1985 and 3rd Ed. 1994 in Section 3 - 1.3.4. It was removedin the 4th Ed., but is still a good rule of thumb.
References:ACI 318-05 Appendix D.FDOT/University of Florida Report BD545 RPWO #54,Anchor Embedment Requirements for Signal/Sign Structures, July 2007.
number of anchor bolts
anchor bolt diameter
anchor bolt circle diameter
anchor bolt embedment
shaft diameter
adjusted cover
UF Report Eqn 3-2
load bearing length of anchor for shear
ACI D.6.2.2
shear break-out strength (single anchor)
UF Report Eqn 2-11
UF Report Fig 3-7
UF Report Fig 3-7
projected concrete failure area (single anchor)
ACI Eqn D-23
projected concrete failure area (group)
ACI D.6.2.1
eccentric load modifier ACI D.6.2.5
edge effect modifier ACI D.6.2.6
cracked section modifier ACI D.6.2.7 (stirrup spacing <= 4")
member thickness modifier ACI D.6.2.8
strength reduction factor ACI D.4.4.c.i ( shear breakout, condition A)
concrete breakout strength - shear
ACI Eqn D-22 Shear force | to edge
ACI D.6.2.1.c Shear force || to edge
concrete breakout strength - torsion
maximum torsion (Mx & Mz not used)maximum overturning (My not used) maximum CSR
0 - clay1 - sand
Use the member cross section adjacent to the weld toe to compute the nominal stress range. LTS 11.9
SM V3 11.6
Arm and Pole Welds
A325 Connection Bolts
Anchor Bolts
zero out initial header row for signal/sign information
(use MC10x33.6 channel for connection)
Compare Mast Arm deflection of each arm to a proposed camber
(for Two Arm Structures only)
(if Clearance equals 0, then Connection Plates intersect and redesign is required.
STRUCTURE NO. 3 CLAY MODEL
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⋅ , ( ):= ⋅=
⋅ ⋅ ⋅
⋅:=
⋅=
⋅⋅=:=
⋅( )
⋅=:=
≤ , , ( ):=
=
⋅
⋅:= ⋅=
⋅:= ⋅=
⋅ ⋅:= ⋅=
> , , ( ):= ⋅=
:=
:=
:=
:=
:=
⋅ ⋅ ⋅ ⋅( )⋅ ⋅:= ⋅=
⋅:= ⋅=
⋅:= ⋅⋅=
⋅ ⋅⋅=
⋅⋅=
⋅ ≥ , , ( ):= =
≤ , , ( ):=
=
⋅⋅=
⋅⋅=
⋅⋅=
= ⋅= ⋅= ⋅= =
= = ⋅=
= ⋅= ⋅=
= = =
= =
= =
=
= ⋅=
:=
⋅= ⋅= =
⋅= ⋅= =
⋅= ⋅= =
⋅= =
⋅= =
⋅= =
⋅= ⋅=
=
⋅=
=
⋅= ⋅= =
⋅= =
, ←
− ←
..∈
:=
, ( ):= , ( ):=
, ( ):= , (:=
, ( ):= , (:=
, ( ):= , ( ):=
, ( ):= , ( ):=
=⋅=
= = =
= = =
= =
=
=
=
=
=
= ⋅=
⋅=
⋅=
⋅=
⋅= ( ) ⋅= ( ) =
= =
=
=
=
=
=
= ⋅= ⋅=
⋅=
⋅=
⋅=
⋅= ( ) ⋅= ( ) =
= ⋅=
= = ⋅=
⋅= = =
⋅= ⋅=
⋅= ⋅=
= = = =
⋅= ⋅=⋅=
⋅= ⋅= ⋅=
=⋅= ⋅=
− ⋅= ⋅= =
( ) =
= ⋅= ⋅=
⋅= ⋅=
⋅= ⋅=
⋅= ⋅=
=⋅= ⋅=
= ⋅= ⋅=
⋅= ⋅=
⋅= ⋅=
⋅= ⋅=
⋅= ⋅=
=
=
= ⋅=
= ⋅= ⋅=
⋅= ⋅=
⋅=
= = =
⋅= ⋅= ⋅= =
= = =
= ⋅= =
⋅:= ⋅:=
⋅( ) ⋅, ⋅, −:= ⋅( ) ⋅, ⋅,
−:=
⋅ ( )+:= ⋅=
( )⋅:= ⋅=
⋅ ⋅ ⋅ ⋅+ ( )+:= ⋅=
( )⋅:= ⋅=
⋅= ⋅> ⋅ −, , :=
⋅= ⋅= ⋅= ⋅=
⋅= ⋅=
−( )
⋅−:= := ⋅= ⋅=
−( )
⋅−
⋅ ⋅+:=
−( )
⋅−
⋅ ⋅−:= ⋅= ⋅=
−( ) −( )+:= ≤( ) >( ) , ⋅, , , := ⋅=
− − − −
−
−
−
−
⋅=
⋅=
⋅=
⋅=
⋅=
⋅=
⋅=
⋅=
⋅=
⋅=
⋅=
⋅=
−
−
⋅=
⋅=
⋅=
⋅=
⋅=
=
=
− − −−
−
−
⋅=
⋅=
⋅=
⋅=
⋅=
⋅=
––
Soil Parameters
Shaft Embedment/Length
––
the “ East, Florida”
Based on a review of the “Potentiometric Surface of the Upper Floridan Aquifer, Florida” maps published by the USGS; the