===============================================================================
MASTLOD 1.2 (USA)-loads on latticed towers (c)1997,2004 Guymast Inc.
Tel:(416)736-7453 Fax:(416)736-4372 Web:www.guymast.com
Processed under license at:
Weisman Consultants Inc. on: 24 sep 2004 at: 17:04:26
===============================================================================
[DEMOGU] - 300 FT GUYED TOWER ANALYSIS - OCTOBER 2004
MAST GEOMETRY ( ft )
====================
PANEL NO.OF SUB ..ELEVATION OF.. ..FACE WIDTH AT.. TYPICAL
TYPE LEGS DIVIDE BOTTOM TOP BOTTOM TOP PANEL
HEIGHT
x 3 0 260.000 300.000 2.500 2.500 1.67
d 3 0 160.000 260.000 2.500 2.500 1.25
x 3 0 120.000 160.000 2.500 2.500 1.67
d 3 0 0.000 120.000 2.500 2.500 1.25
PANEL PROPERTIES
================
BOTTOM TOP .................TYPE OF MATERIALS USED IN..........
ELEV ELEV LEGS DIAGS HORIZ INTRNL SUB SUB GUSSET
ft ft BRACING DIAGS HORIZ
260.000 300.000 2 4 4 0 0 0 0
160.000 260.000 2 3 0 0 0 0 0
120.000 160.000 1 4 4 0 0 0 0
0.000 120.000 1 3 0 0 0 0 0
MATERIAL TYPES
==============
TYPE OF TYPE NO OF ORIENT- PROJECTION.ALONG THICK- DENSITY
SHAPE NO ELEMENTS ATION VERT HORIZ NESS
& deg in in # in * pcf
sr 1 1 0.0 2.25 0.00 0.000 500.0
sr 2 1 0.0 2.00 0.00 0.000 500.0
sr 3 1 0.0 0.75 0.00 0.000 500.0
sr 4 1 0.0 1.00 0.00 0.000 500.0
sr 5 1 0.0 0.50 0.00 0.000 500.0
sch40 6 1 0.0 2.50 0.00 0.000 165.0
c 7 1 0.0 2.00 5.00 0.125 0.125
sch40 8 1 0.0 12.00 0.00 0.000 100.0
l 9 1 0.0 4.00 4.00 0.250 500.0
sch40 10 1 0.0 4.00 0.00 0.000 500.0
sch40 11 2 0.0 6.00 0.00 0.000 100.0
l 12 2 0.0 3.50 3.00 0.250 500.0
RHSS 13 1 0.0 2.88 0.00 0.188 500.0
sch40 14 1 0.0 2.50 0.00 0.000 165.0
sch40 15 1 0.0 1.50 0.00 0.000 165.0
& - With respect to vertical # - Web in WF,C & T sections
* - Flange thickness in WF,C & T sections
LADDER GEOMETRY
===============
..ELEVATION OF.. .....SIZE.... ......POSITION...... ...MATERIALS....
BOTTOM TOP WIDTH STEP DIST AZI ORIENT RAIL RUNG SAFE
ft ft in in * ft deg & deg T-RAIL
0.000 300.000 26.00 45.00 0.72 180.00 90.00 0 7 0
0.000 300.000 10.00 15.00 0.63 180.00 90.00 0 5 6
* if negative a constant distance from face based on bottom elevation
& if negative orientation is disregarded in calculation of loads
TRANSMISSION LINES
==================
TYPE OF ..ELEVATION OF.. NO.OF ........POSITION....... C/C WT
LINE BOTTOM TOP LINES DISTANCE AZI ORIENT SPACING MULT
ft ft * ft # deg & deg in
ewp63 0.000 287.000 1 0.50 230.0 230.0 0.00 1
ewp63 0.000 272.000 2 0.30 180.0 90.0 2.32 1
ewp63 0.000 236.000 1 0.30 180.0 180.0 0.00 1
fh1.625 0.000 151.000 1 0.50 130.0 130.0 0.00 1
fh0.875 0.000 131.000 1 0.70 120.0 120.0 0.00 1
* if negative a constant distance from face based on bottom elevation
# if negative the line considered same on all faces and integral with tower
& if negative orientation is disregarded in calculation of loads
OTHER MOUNTINGS
===============
ELEV TYPE.OF NO.OF LENGTH ....LOCATION.... ORIENTATION
MATERIAL ELMNTS DISTANCE AZI HORIZ VERT
ft ft ft & deg deg deg
300.000 8 1 1.00 0.00 0.00 0.00 90.00
287.000 10 1 8.00 2.00 350.00 0.00 90.00
287.000 9 2 3.00 0.83 300.00 30.00 0.00
280.000 12 2 14.00 1.80 240.00 150.00 0.00
280.000 12 2 14.00 1.80 0.00 90.00 0.00
280.000 12 2 14.00 1.80 120.00 30.00 0.00
272.000 10 1 8.00 2.00 350.00 0.00 90.00
272.000 9 2 3.00 0.83 60.00 150.00 0.00
272.000 10 1 6.00 2.00 110.00 0.00 90.00
272.000 9 2 3.00 0.83 300.00 30.00 0.00
236.000 10 1 6.00 2.00 110.00 0.00 90.00
236.000 9 2 3.00 0.83 60.00 150.00 0.00
151.000 10 1 6.00 2.00 230.00 0.00 90.00
151.000 9 2 3.00 0.83 180.00 90.00 0.00
140.000 12 2 14.00 1.80 240.00 150.00 0.00
140.000 12 2 14.00 1.80 0.00 90.00 0.00
140.000 12 2 14.00 1.80 120.00 30.00 0.00
131.000 10 1 4.00 2.00 230.00 0.00 90.00
& if negative orientation is disregarded in calculation of loads
MICROWAVE PARABOLIC ANTENNAS
============================
.....ANTENNA..... ....POSITION.... SHIELDING
TYPE ELEV AZIMUTH SIZE RADIUS AZIMUTH PERMITTED
ft deg ft ft deg percent
std+r 287.000 296.00 10.00 2.45 0.00 50.
hp 272.000 105.00 10.00 2.45 120.00 50.
hp 272.000 296.00 8.00 2.45 0.00 50.
hp 236.000 105.00 10.00 2.45 120.00 50.
std 151.000 241.00 10.00 2.45 240.00 50.
GUY GEOMETRY
============
ELEV GUY GUY DIAMETER HEIGHT RADIUS MAST ATTACH INITIAL
AZI TYPE ATTACH AZI TENSION
* RADIUS
ft deg in ft ft ft deg kip
280.0 120. BS 0.750 280.0 230.0 8.080 60. 6.800
280.0 240. BS 0.750 280.0 230.0 8.080 180. 6.800
280.0 0. BS 0.750 280.0 230.0 8.080 300. 6.800
280.0 0. BS 0.750 280.0 230.0 8.080 60. 6.800
280.0 120. BS 0.750 280.0 230.0 8.080 180. 6.800
280.0 240. BS 0.750 280.0 230.0 8.080 300. 6.800
230.0 0. GS 0.625 230.0 230.0 1.440 0. 4.030
230.0 120. GS 0.625 230.0 230.0 1.440 120. 4.030
230.0 240. GS 0.625 230.0 230.0 1.440 240. 4.030
185.0 0. GS 0.500 185.0 230.0 1.440 0. 2.550
185.0 120. GS 0.500 185.0 230.0 1.440 120. 2.550
185.0 240. GS 0.500 185.0 230.0 1.440 240. 2.550
140.0 120. GS 0.500 140.0 230.0 8.080 60. 2.550
140.0 240. GS 0.500 140.0 230.0 8.080 180. 2.550
140.0 0. GS 0.500 140.0 230.0 8.080 300. 2.550
140.0 0. GS 0.500 140.0 230.0 8.080 60. 2.550
140.0 120. GS 0.500 140.0 230.0 8.080 180. 2.550
140.0 240. GS 0.500 140.0 230.0 8.080 300. 2.550
90.0 0. GS 0.438 90.0 230.0 1.440 0. 1.950
90.0 120. GS 0.438 90.0 230.0 1.440 120. 1.950
90.0 240. GS 0.438 90.0 230.0 1.440 240. 1.950
45.0 0. GS 0.438 45.0 230.0 1.440 0. 1.950
45.0 120. GS 0.438 45.0 230.0 1.440 120. 1.950
45.0 240. GS 0.438 45.0 230.0 1.440 240. 1.950
* GS - guy strand
BS - bridge strand
================================================================================
LOADING CONDITION A ========================================================
Bare tower 100 mph wind at azimuth 0 deg
WIND LOADING
============
.....WIND LOADING..... ...ICE LOADING.. .....TYPE OF..... ....FACTORS.....
AZI SPEED REF.VEL. RADIUS DENSITY EXP STD ANT WIND DEAD ICE
PRESS. LOAD LOAD LOAD LOAD
deg mph psf in pcf * & #
0.0 100.00 0.00 0.00 56.20 1 1 1 1.00 1.00 1.00
* Type of Exposure : 1 - Wind profile (Kz) based on EIA 222 F (June 1996)
2 - Wind profile Kz = 1 ; Gh = 1
3 - Wind profile (Kz) based on EIA 222 C (Mar.1976)
4 - Wind factors supplied by user ( Gh=1, step function)
5 - Wind profile UBC (May.1988) Exposure C
6 - Wind profile UBC (May.1988) Exposure B
7 - Wind profile Site Specific Wind Formula
& Type of Standard : 1 - EIA - 222 F ( June 1996 )
2 - EIA - 222 C ( March 1976 )
3 - UBC - 88 ( May 1 1988 )
# Type of Antenna load :
1 - Antenna forces for this wind direction
2 - Maximum possible forces regardless of
wind direction
SUPPRESS PRINTING
=================
....LOAD SUMMARY FOR.... ................LOAD COMPONENTS....................
MAST GUYMAST PANEL PANELS LADDERS TX-LINES DISCRETE INDIVIDUAL
POINTS APPURTENANCES ELEMENTS
no no no no no no no no
MAST LOADING
============
LOAD ELEV APPLY..LOAD..AT LOAD ......FORCES...... ......MOMENTS.....
TYPE RADIUS AZI AZI HORIZ DOWN VERTICAL TORSNAL
ft ft kip kip ft-kip ft-kip
D 300.000 0.00 0.0 0.0 0.0812 0.0810 0.0036 0.0000
D 288.338 0.00 0.0 0.0 0.0804 0.0810 0.0036 0.0000
D 288.338 0.00 0.0 0.0 0.0820 0.0811 0.0036 0.0006
D 286.672 0.00 0.0 0.0 0.0820 0.0811 0.0036 0.0006
D 286.672 0.00 0.0 0.0 0.0886 0.0815 0.0038 0.0032
D 273.344 0.00 0.0 0.0 0.0876 0.0815 0.0038 0.0032
D 273.344 0.00 0.0 0.0 0.0896 0.0817 0.0038 0.0032
D 271.678 0.00 0.0 0.0 0.0896 0.0817 0.0038 0.0032
D 271.678 0.00 0.0 0.0 0.0989 0.0826 0.0041 0.0032
D 261.682 0.00 0.0 0.0 0.0980 0.0826 0.0041 0.0032
D 261.682 0.00 0.0 0.0 0.0976 0.0822 0.0041 0.0031
D 260.000 0.00 0.0 0.0 0.0976 0.0822 0.0041 0.0031
D 260.000 0.00 0.0 0.0 0.0821 0.0501 0.0041 0.0032
D 236.250 0.00 0.0 0.0 0.0800 0.0501 0.0041 0.0031
D 236.250 0.00 0.0 0.0 0.0852 0.0505 0.0042 0.0031
D 160.000 0.00 0.0 0.0 0.0774 0.0506 0.0042 0.0028
D 160.000 0.00 0.0 0.0 0.0919 0.0918 0.0042 0.0027
D 151.670 0.00 0.0 0.0 0.0908 0.0918 0.0042 0.0027
D 151.670 0.00 0.0 0.0 0.0955 0.0923 0.0044 0.0008
D 150.004 0.00 0.0 0.0 0.0955 0.0923 0.0044 0.0008
D 150.004 0.00 0.0 0.0 0.0986 0.0926 0.0045 -0.0005
D 131.678 0.00 0.0 0.0 0.0953 0.0926 0.0045 -0.0005
D 131.678 0.00 0.0 0.0 0.0976 0.0928 0.0046 -0.0021
D 130.012 0.00 0.0 0.0 0.0976 0.0928 0.0046 -0.0021
D 130.012 0.00 0.0 0.0 0.0990 0.0929 0.0046 -0.0032
D 121.682 0.00 0.0 0.0 0.0975 0.0929 0.0046 -0.0031
D 121.682 0.00 0.0 0.0 0.0970 0.0926 0.0046 -0.0031
D 120.000 0.00 0.0 0.0 0.0970 0.0926 0.0046 -0.0031
D 120.000 0.00 0.0 0.0 0.0823 0.0604 0.0046 -0.0030
D 0.000 0.00 0.0 0.0 0.0570 0.0604 0.0046 -0.0021
C 300.000 0.00 0.0 0.0 0.0467 0.0109 0.0000 0.0000
C 287.000 1.55 342.6 0.0 0.2125 0.1285 0.0000 0.0107
C 280.000 0.00 300.6 0.0 1.2568 0.9115 0.0000 0.0000
C 272.000 0.80 30.0 0.0 0.3633 0.2350 0.0000 0.0149
C 236.000 1.46 100.5 0.0 0.1479 0.1065 0.0000 0.0235
C 151.000 1.46 220.5 0.0 0.2248 0.1065 0.0000 0.0627
C 140.000 0.00 300.6 0.0 1.0310 0.9115 0.0000 0.0000
C 131.000 2.00 230.0 0.0 0.0566 0.0441 0.0000 0.0000
GUYMAST LOADING
===============
LOAD ELEV .....FORCES (kip)...... ...MOMENTS (ft.kips)... ANTENNA
TYPE ft NORTH EAST DOWN NORTH EAST TORSION AZIMUTH
D 300.000 -0.0812 0.0000 0.0810 -0.0036 0.0000 0.0000
D 288.338 -0.0804 0.0000 0.0810 -0.0036 0.0000 0.0000
D 288.338 -0.0820 0.0000 0.0811 -0.0036 0.0000 0.0006
D 286.672 -0.0820 0.0000 0.0811 -0.0036 0.0000 0.0006
D 286.672 -0.0886 0.0000 0.0815 -0.0038 -0.0002 0.0032
D 273.344 -0.0876 0.0000 0.0815 -0.0038 -0.0002 0.0032
D 273.344 -0.0896 0.0000 0.0817 -0.0038 -0.0002 0.0032
D 271.678 -0.0896 0.0000 0.0817 -0.0038 -0.0002 0.0032
D 271.678 -0.0989 0.0000 0.0826 -0.0041 -0.0002 0.0032
D 261.682 -0.0980 0.0000 0.0826 -0.0041 -0.0002 0.0032
D 261.682 -0.0976 0.0000 0.0822 -0.0041 -0.0002 0.0031
D 260.000 -0.0976 0.0000 0.0822 -0.0041 -0.0002 0.0031
D 260.000 -0.0821 0.0000 0.0501 -0.0041 -0.0002 0.0032
D 236.250 -0.0800 0.0000 0.0501 -0.0041 -0.0002 0.0031
D 236.250 -0.0852 0.0000 0.0505 -0.0042 -0.0002 0.0031
D 160.000 -0.0774 0.0000 0.0506 -0.0042 -0.0002 0.0028
D 160.000 -0.0919 0.0000 0.0918 -0.0042 -0.0002 0.0027
D 151.670 -0.0908 0.0000 0.0918 -0.0042 -0.0002 0.0027
D 151.670 -0.0955 0.0000 0.0923 -0.0044 0.0000 0.0008
D 150.004 -0.0955 0.0000 0.0923 -0.0044 0.0000 0.0008
D 150.004 -0.0986 0.0000 0.0926 -0.0045 0.0001 -0.0005
D 131.678 -0.0953 0.0000 0.0926 -0.0045 0.0001 -0.0005
D 131.678 -0.0976 0.0000 0.0928 -0.0045 0.0002 -0.0021
D 130.012 -0.0976 0.0000 0.0928 -0.0045 0.0002 -0.0021
D 130.012 -0.0990 0.0000 0.0929 -0.0046 0.0003 -0.0032
D 121.682 -0.0975 0.0000 0.0929 -0.0046 0.0003 -0.0031
D 121.682 -0.0970 0.0000 0.0926 -0.0046 0.0003 -0.0031
D 120.000 -0.0970 0.0000 0.0926 -0.0046 0.0003 -0.0031
D 120.000 -0.0823 0.0000 0.0604 -0.0046 0.0003 -0.0030
D 0.000 -0.0570 0.0000 0.0604 -0.0046 0.0003 -0.0021
C 300.000 -0.0467 0.0000 0.0109 0.0000 0.0000 0.0000
C 287.000 -0.2125 0.0000 0.1285 0.1904 -0.0596 0.1093
C 280.000 -1.2568 0.0000 0.9115 0.0000 0.0000 0.0000
C 272.000 -0.3633 0.0000 0.2350 0.1619 0.0937 -0.1299
C 236.000 -0.1479 0.0000 0.1065 -0.0285 0.1533 -0.1895
C 151.000 -0.2248 0.0000 0.1065 -0.1185 -0.1013 0.2766
C 140.000 -1.0310 0.0000 0.9115 0.0000 0.0000 0.0000
C 131.000 -0.0566 0.0000 0.0441 -0.0567 -0.0675 0.0867
C 287.000 -2.4348 0.5088 0.4420 1.0829 0.0000 -0.4415 296.
C 272.000 -2.6380 1.1160 0.5410 -0.6627 1.1479 -8.7489 105.
C 272.000 -1.8816 1.4606 0.4470 1.0951 0.0000 -3.4986 296.
C 236.000 -2.5374 1.0734 0.5410 -0.6627 1.1479 -8.4153 105.
C 151.000 -2.0862 -0.6099 0.3420 -0.4189 -0.7256 8.4773 241.
LOADS AT PANEL POINTS
=====================
LOAD ELEV .....FORCES (kip)...... ...MOMENTS (ft.kips)...
TYPE ft NORTH EAST DOWN NORTH EAST TORSION
C 300.000 -0.1143 0.0000 0.0784 -0.0030 0.0000 0.0000
C 298.334 -0.1352 0.0000 0.1350 -0.0060 0.0000 0.0000
C 296.668 -0.1350 0.0000 0.1350 -0.0060 0.0000 0.0000
C 295.002 -0.1348 0.0000 0.1350 -0.0060 0.0000 0.0000
C 293.336 -0.1345 0.0000 0.1350 -0.0060 0.0000 0.0000
C 291.670 -0.1343 0.0000 0.1350 -0.0060 0.0000 0.0000
C 290.004 -0.1341 0.0000 0.1350 -0.0060 0.0000 0.0000
C 288.338 -0.6563 0.1001 0.2474 0.2446 -0.0118 -0.0649
C 286.672 -2.2683 0.4087 0.5938 1.0166 -0.0481 -0.2636
C 285.006 -0.1475 0.0000 0.1358 -0.0063 -0.0003 0.0054
C 283.340 -0.1472 0.0000 0.1358 -0.0063 -0.0003 0.0054
C 281.674 -0.1470 0.0000 0.1358 -0.0063 -0.0003 0.0054
C 280.008 -1.3973 0.0000 1.0428 -0.0063 -0.0003 0.0054
C 278.342 -0.1527 0.0000 0.1403 -0.0063 -0.0003 0.0053
C 276.676 -0.1462 0.0000 0.1358 -0.0063 -0.0003 0.0053
C 275.010 -0.1460 0.0000 0.1358 -0.0063 -0.0003 0.0053
C 273.344 -1.0906 0.4976 0.3722 0.1085 0.2394 -2.3851
C 271.678 -4.0969 2.0790 1.1237 0.4730 1.0014 -9.9817
C 270.012 -0.1646 0.0000 0.1375 -0.0068 -0.0003 0.0053
C 268.346 -0.1643 0.0000 0.1375 -0.0068 -0.0003 0.0053
C 266.680 -0.1640 0.0000 0.1375 -0.0068 -0.0003 0.0053
C 265.014 -0.1637 0.0000 0.1375 -0.0068 -0.0003 0.0053
C 263.348 -0.1634 0.0000 0.1375 -0.0068 -0.0003 0.0053
C 261.682 -0.1638 0.0000 0.1379 -0.0068 -0.0003 0.0053
C 260.000 -0.1335 0.0000 0.1005 -0.0060 -0.0003 0.0046
C 258.750 -0.1026 0.0000 0.0626 -0.0051 -0.0002 0.0040
C 257.500 -0.1024 0.0000 0.0626 -0.0051 -0.0002 0.0040
C 256.250 -0.1023 0.0000 0.0626 -0.0051 -0.0002 0.0040
C 255.000 -0.1021 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 253.750 -0.1020 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 252.500 -0.1019 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 251.250 -0.1017 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 250.000 -0.1016 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 248.750 -0.1014 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 247.500 -0.1013 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 246.250 -0.1011 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 245.000 -0.1010 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 243.750 -0.1008 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 242.500 -0.1007 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 241.250 -0.1005 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 240.000 -0.1004 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 238.750 -0.1002 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 237.500 -0.1001 0.0000 0.0626 -0.0051 -0.0002 0.0039
C 236.250 -2.2511 0.8587 0.5808 -0.5581 1.0407 -6.8799
C 235.000 -0.6432 0.2147 0.1927 -0.1435 0.2600 -1.7171
C 233.750 -0.1067 0.0000 0.0632 -0.0053 -0.0002 0.0039
C 232.500 -0.1065 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 231.250 -0.1063 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 230.000 -0.1062 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 228.750 -0.1060 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 227.500 -0.1058 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 226.250 -0.1057 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 225.000 -0.1055 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 223.750 -0.1053 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 222.500 -0.1052 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 221.250 -0.1050 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 220.000 -0.1048 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 218.750 -0.1047 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 217.500 -0.1045 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 216.250 -0.1043 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 215.000 -0.1042 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 213.750 -0.1040 0.0000 0.0632 -0.0053 -0.0002 0.0038
C 212.500 -0.1038 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 211.250 -0.1036 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 210.000 -0.1035 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 208.750 -0.1033 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 207.500 -0.1031 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 206.250 -0.1029 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 205.000 -0.1027 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 203.750 -0.1026 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 202.500 -0.1024 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 201.250 -0.1022 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 200.000 -0.1020 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 198.750 -0.1018 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 197.500 -0.1017 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 196.250 -0.1015 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 195.000 -0.1013 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 193.750 -0.1011 0.0000 0.0632 -0.0053 -0.0002 0.0037
C 192.500 -0.1009 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 191.250 -0.1007 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 190.000 -0.1005 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 188.750 -0.1003 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 187.500 -0.1002 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 186.250 -0.1000 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 185.000 -0.0998 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 183.750 -0.0996 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 182.500 -0.0994 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 181.250 -0.0992 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 180.000 -0.0990 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 178.750 -0.0988 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 177.500 -0.0986 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 176.250 -0.0984 0.0000 0.0632 -0.0053 -0.0002 0.0036
C 175.000 -0.0982 0.0000 0.0632 -0.0053 -0.0002 0.0035
C 173.750 -0.0980 0.0000 0.0632 -0.0053 -0.0002 0.0035
C 172.500 -0.0978 0.0000 0.0632 -0.0053 -0.0002 0.0035
C 171.250 -0.0976 0.0000 0.0632 -0.0053 -0.0002 0.0035
C 170.000 -0.0974 0.0000 0.0632 -0.0053 -0.0002 0.0035
C 168.750 -0.0972 0.0000 0.0632 -0.0053 -0.0002 0.0035
C 167.500 -0.0970 0.0000 0.0632 -0.0053 -0.0002 0.0035
C 166.250 -0.0968 0.0000 0.0632 -0.0053 -0.0002 0.0035
C 165.000 -0.0966 0.0000 0.0632 -0.0053 -0.0002 0.0035
C 163.750 -0.0964 0.0000 0.0632 -0.0053 -0.0002 0.0035
C 162.500 -0.0961 0.0000 0.0632 -0.0053 -0.0002 0.0035
C 161.250 -0.0959 0.0000 0.0632 -0.0053 -0.0002 0.0035
C 160.000 -0.1245 0.0000 0.1081 -0.0061 -0.0003 0.0040
C 158.334 -0.1529 0.0000 0.1529 -0.0070 -0.0003 0.0045
C 156.668 -0.1524 0.0000 0.1529 -0.0070 -0.0003 0.0045
C 155.002 -0.1520 0.0000 0.1529 -0.0070 -0.0003 0.0045
C 153.336 -0.1515 0.0000 0.1529 -0.0070 -0.0003 0.0045
C 151.670 -1.5368 -0.3646 0.4214 -0.3285 -0.4946 5.2363
C 150.004 -1.0911 -0.2453 0.3343 -0.2235 -0.3325 3.5207
C 148.338 -0.1640 0.0000 0.1542 -0.0075 0.0002 -0.0009
C 146.672 -0.1634 0.0000 0.1542 -0.0075 0.0002 -0.0009
C 145.006 -0.1629 0.0000 0.1542 -0.0075 0.0002 -0.0009
C 143.340 -0.1624 0.0000 0.1542 -0.0075 0.0002 -0.0009
C 141.674 -0.1618 0.0000 0.1542 -0.0075 0.0002 -0.0009
C 140.008 -1.1873 0.0000 1.0613 -0.0075 0.0002 -0.0009
C 138.342 -0.1657 0.0000 0.1586 -0.0075 0.0002 -0.0008
C 136.676 -0.1602 0.0000 0.1542 -0.0075 0.0002 -0.0008
C 135.010 -0.1596 0.0000 0.1542 -0.0075 0.0002 -0.0008
C 133.344 -0.1591 0.0000 0.1542 -0.0075 0.0002 -0.0008
C 131.678 -0.1942 0.0000 0.1805 -0.0411 -0.0398 0.0492
C 130.012 -0.1868 0.0000 0.1726 -0.0307 -0.0270 0.0309
C 128.346 -0.1647 0.0000 0.1548 -0.0076 0.0005 -0.0053
C 126.680 -0.1641 0.0000 0.1548 -0.0076 0.0005 -0.0053
C 125.014 -0.1634 0.0000 0.1548 -0.0076 0.0005 -0.0052
C 123.348 -0.1628 0.0000 0.1548 -0.0076 0.0005 -0.0052
C 121.682 -0.1629 0.0000 0.1553 -0.0077 0.0005 -0.0052
C 120.000 -0.1346 0.0000 0.1156 -0.0067 0.0005 -0.0046
C 118.750 -0.1059 0.0000 0.0755 -0.0057 0.0004 -0.0039
C 117.500 -0.1056 0.0000 0.0755 -0.0057 0.0004 -0.0039
C 116.250 -0.1053 0.0000 0.0755 -0.0057 0.0004 -0.0039
C 115.000 -0.1049 0.0000 0.0755 -0.0057 0.0004 -0.0039
C 113.750 -0.1046 0.0000 0.0755 -0.0057 0.0004 -0.0039
C 112.500 -0.1043 0.0000 0.0755 -0.0057 0.0004 -0.0039
C 111.250 -0.1039 0.0000 0.0755 -0.0057 0.0004 -0.0038
C 110.000 -0.1036 0.0000 0.0755 -0.0057 0.0004 -0.0038
C 108.750 -0.1033 0.0000 0.0755 -0.0057 0.0004 -0.0038
C 107.500 -0.1029 0.0000 0.0755 -0.0057 0.0004 -0.0038
C 106.250 -0.1026 0.0000 0.0755 -0.0057 0.0004 -0.0038
C 105.000 -0.1022 0.0000 0.0755 -0.0057 0.0004 -0.0038
C 103.750 -0.1019 0.0000 0.0755 -0.0057 0.0004 -0.0038
C 102.500 -0.1015 0.0000 0.0755 -0.0057 0.0004 -0.0038
C 101.250 -0.1012 0.0000 0.0755 -0.0057 0.0004 -0.0037
C 100.000 -0.1008 0.0000 0.0755 -0.0057 0.0004 -0.0037
C 98.750 -0.1005 0.0000 0.0755 -0.0057 0.0004 -0.0037
C 97.500 -0.1001 0.0000 0.0755 -0.0057 0.0004 -0.0037
C 96.250 -0.0997 0.0000 0.0755 -0.0057 0.0004 -0.0037
C 95.000 -0.0994 0.0000 0.0755 -0.0057 0.0004 -0.0037
C 93.750 -0.0990 0.0000 0.0755 -0.0057 0.0004 -0.0037
C 92.500 -0.0986 0.0000 0.0755 -0.0057 0.0004 -0.0036
C 91.250 -0.0982 0.0000 0.0755 -0.0057 0.0004 -0.0036
C 90.000 -0.0978 0.0000 0.0755 -0.0057 0.0004 -0.0036
C 88.750 -0.0974 0.0000 0.0755 -0.0057 0.0004 -0.0036
C 87.500 -0.0970 0.0000 0.0755 -0.0057 0.0004 -0.0036
C 86.250 -0.0966 0.0000 0.0755 -0.0057 0.0004 -0.0036
C 85.000 -0.0962 0.0000 0.0755 -0.0057 0.0004 -0.0036
C 83.750 -0.0958 0.0000 0.0755 -0.0057 0.0004 -0.0035
C 82.500 -0.0954 0.0000 0.0755 -0.0057 0.0004 -0.0035
C 81.250 -0.0950 0.0000 0.0755 -0.0057 0.0004 -0.0035
C 80.000 -0.0946 0.0000 0.0755 -0.0057 0.0004 -0.0035
C 78.750 -0.0942 0.0000 0.0755 -0.0057 0.0004 -0.0035
C 77.500 -0.0937 0.0000 0.0755 -0.0057 0.0004 -0.0035
C 76.250 -0.0933 0.0000 0.0755 -0.0057 0.0004 -0.0034
C 75.000 -0.0929 0.0000 0.0755 -0.0057 0.0004 -0.0034
C 73.750 -0.0924 0.0000 0.0755 -0.0057 0.0004 -0.0034
C 72.500 -0.0920 0.0000 0.0755 -0.0057 0.0004 -0.0034
C 71.250 -0.0915 0.0000 0.0755 -0.0057 0.0004 -0.0034
C 70.000 -0.0911 0.0000 0.0755 -0.0057 0.0004 -0.0034
C 68.750 -0.0906 0.0000 0.0755 -0.0057 0.0004 -0.0033
C 67.500 -0.0901 0.0000 0.0755 -0.0057 0.0004 -0.0033
C 66.250 -0.0896 0.0000 0.0755 -0.0057 0.0004 -0.0033
C 65.000 -0.0891 0.0000 0.0755 -0.0057 0.0004 -0.0033
C 63.750 -0.0887 0.0000 0.0755 -0.0057 0.0004 -0.0033
C 62.500 -0.0882 0.0000 0.0755 -0.0057 0.0004 -0.0033
C 61.250 -0.0876 0.0000 0.0755 -0.0057 0.0004 -0.0032
C 60.000 -0.0871 0.0000 0.0755 -0.0057 0.0004 -0.0032
C 58.750 -0.0866 0.0000 0.0755 -0.0057 0.0004 -0.0032
C 57.500 -0.0861 0.0000 0.0755 -0.0057 0.0004 -0.0032
C 56.250 -0.0855 0.0000 0.0755 -0.0057 0.0004 -0.0032
C 55.000 -0.0850 0.0000 0.0755 -0.0057 0.0004 -0.0031
C 53.750 -0.0844 0.0000 0.0755 -0.0057 0.0004 -0.0031
C 52.500 -0.0839 0.0000 0.0755 -0.0057 0.0004 -0.0031
C 51.250 -0.0833 0.0000 0.0755 -0.0057 0.0004 -0.0031
C 50.000 -0.0827 0.0000 0.0755 -0.0057 0.0004 -0.0031
C 48.750 -0.0821 0.0000 0.0755 -0.0057 0.0004 -0.0030
C 47.500 -0.0815 0.0000 0.0755 -0.0057 0.0004 -0.0030
C 46.250 -0.0809 0.0000 0.0755 -0.0057 0.0004 -0.0030
C 45.000 -0.0803 0.0000 0.0755 -0.0057 0.0004 -0.0030
C 43.750 -0.0796 0.0000 0.0755 -0.0057 0.0004 -0.0029
C 42.500 -0.0790 0.0000 0.0755 -0.0057 0.0004 -0.0029
C 41.250 -0.0783 0.0000 0.0755 -0.0057 0.0004 -0.0029
C 40.000 -0.0776 0.0000 0.0755 -0.0057 0.0004 -0.0029
C 38.750 -0.0769 0.0000 0.0755 -0.0057 0.0004 -0.0028
C 37.500 -0.0762 0.0000 0.0755 -0.0057 0.0004 -0.0028
C 36.250 -0.0754 0.0000 0.0755 -0.0057 0.0004 -0.0028
C 35.000 -0.0747 0.0000 0.0755 -0.0057 0.0004 -0.0028
C 33.750 -0.0739 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 32.500 -0.0735 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 31.250 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 30.000 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 28.750 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 27.500 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 26.250 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 25.000 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 23.750 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 22.500 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 21.250 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 20.000 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 18.750 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 17.500 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 16.250 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 15.000 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 13.750 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 12.500 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 11.250 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 10.000 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 8.750 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 7.500 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 6.250 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 5.000 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 3.750 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 2.500 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 1.250 -0.0734 0.0000 0.0755 -0.0057 0.0004 -0.0027
C 0.000 -0.0367 0.0000 0.0378 -0.0029 0.0002 -0.0014
PANEL LOADING
=============
LOAD ELEV APPLY..LOAD..AT LOAD ......FORCES...... ......MOMENTS.....
TYPE RADIUS AZI AZI HORIZ DOWN VERTICAL TORSNAL
ft ft kip kip ft-kip ft-kip
C 299.167 0.00 0.0 0.0 0.1353 0.1350 0.0060 0.0000
C 297.501 0.00 0.0 0.0 0.1351 0.1350 0.0060 0.0000
C 295.835 0.00 0.0 0.0 0.1349 0.1350 0.0060 0.0000
C 294.169 0.00 0.0 0.0 0.1346 0.1350 0.0060 0.0000
C 292.503 0.00 0.0 0.0 0.1344 0.1350 0.0060 0.0000
C 290.837 0.00 0.0 0.0 0.1342 0.1350 0.0060 0.0000
C 289.171 0.00 0.0 0.0 0.1340 0.1350 0.0060 0.0000
C 287.505 0.00 0.0 0.0 0.1365 0.1352 0.0060 0.0011
C 285.839 0.00 0.0 0.0 0.1476 0.1358 0.0063 0.0054
C 284.173 0.00 0.0 0.0 0.1474 0.1358 0.0063 0.0054
C 282.507 0.00 0.0 0.0 0.1471 0.1358 0.0063 0.0054
C 280.841 0.00 0.0 0.0 0.1469 0.1358 0.0063 0.0054
C 279.175 0.00 0.0 0.0 0.1466 0.1358 0.0063 0.0053
C 277.509 0.00 0.0 0.0 0.1464 0.1358 0.0063 0.0053
C 275.843 0.00 0.0 0.0 0.1461 0.1358 0.0063 0.0053
C 274.177 0.00 0.0 0.0 0.1459 0.1358 0.0063 0.0053
C 272.511 0.00 0.0 0.0 0.1493 0.1362 0.0064 0.0053
C 270.845 0.00 0.0 0.0 0.1647 0.1375 0.0068 0.0053
C 269.179 0.00 0.0 0.0 0.1644 0.1375 0.0068 0.0053
C 267.513 0.00 0.0 0.0 0.1641 0.1375 0.0068 0.0053
C 265.847 0.00 0.0 0.0 0.1638 0.1375 0.0068 0.0053
C 264.181 0.00 0.0 0.0 0.1635 0.1375 0.0068 0.0053
C 262.515 0.00 0.0 0.0 0.1632 0.1375 0.0068 0.0053
C 260.841 0.00 0.0 0.0 0.1643 0.1383 0.0068 0.0053
C 259.375 0.00 0.0 0.0 0.1026 0.0626 0.0051 0.0040
C 258.125 0.00 0.0 0.0 0.1025 0.0626 0.0051 0.0040
C 256.875 0.00 0.0 0.0 0.1024 0.0626 0.0051 0.0040
C 255.625 0.00 0.0 0.0 0.1022 0.0626 0.0051 0.0040
C 254.375 0.00 0.0 0.0 0.1021 0.0626 0.0051 0.0039
C 253.125 0.00 0.0 0.0 0.1019 0.0626 0.0051 0.0039
C 251.875 0.00 0.0 0.0 0.1018 0.0626 0.0051 0.0039
C 250.625 0.00 0.0 0.0 0.1016 0.0626 0.0051 0.0039
C 249.375 0.00 0.0 0.0 0.1015 0.0626 0.0051 0.0039
C 248.125 0.00 0.0 0.0 0.1014 0.0626 0.0051 0.0039
C 246.875 0.00 0.0 0.0 0.1012 0.0626 0.0051 0.0039
C 245.625 0.00 0.0 0.0 0.1011 0.0626 0.0051 0.0039
C 244.375 0.00 0.0 0.0 0.1009 0.0626 0.0051 0.0039
C 243.125 0.00 0.0 0.0 0.1008 0.0626 0.0051 0.0039
C 241.875 0.00 0.0 0.0 0.1006 0.0626 0.0051 0.0039
C 240.625 0.00 0.0 0.0 0.1005 0.0626 0.0051 0.0039
C 239.375 0.00 0.0 0.0 0.1003 0.0626 0.0051 0.0039
C 238.125 0.00 0.0 0.0 0.1002 0.0626 0.0051 0.0039
C 236.875 0.00 0.0 0.0 0.1000 0.0626 0.0051 0.0039
C 235.625 0.00 0.0 0.0 0.1055 0.0631 0.0052 0.0039
C 234.375 0.00 0.0 0.0 0.1068 0.0632 0.0053 0.0039
C 233.125 0.00 0.0 0.0 0.1066 0.0632 0.0053 0.0038
C 231.875 0.00 0.0 0.0 0.1064 0.0632 0.0053 0.0038
C 230.625 0.00 0.0 0.0 0.1063 0.0632 0.0053 0.0038
C 229.375 0.00 0.0 0.0 0.1061 0.0632 0.0053 0.0038
C 228.125 0.00 0.0 0.0 0.1059 0.0632 0.0053 0.0038
C 226.875 0.00 0.0 0.0 0.1058 0.0632 0.0053 0.0038
C 225.625 0.00 0.0 0.0 0.1056 0.0632 0.0053 0.0038
C 224.375 0.00 0.0 0.0 0.1054 0.0632 0.0053 0.0038
C 223.125 0.00 0.0 0.0 0.1053 0.0632 0.0053 0.0038
C 221.875 0.00 0.0 0.0 0.1051 0.0632 0.0053 0.0038
C 220.625 0.00 0.0 0.0 0.1049 0.0632 0.0053 0.0038
C 219.375 0.00 0.0 0.0 0.1048 0.0632 0.0053 0.0038
C 218.125 0.00 0.0 0.0 0.1046 0.0632 0.0053 0.0038
C 216.875 0.00 0.0 0.0 0.1044 0.0632 0.0053 0.0038
C 215.625 0.00 0.0 0.0 0.1042 0.0632 0.0053 0.0038
C 214.375 0.00 0.0 0.0 0.1041 0.0632 0.0053 0.0038
C 213.125 0.00 0.0 0.0 0.1039 0.0632 0.0053 0.0038
C 211.875 0.00 0.0 0.0 0.1037 0.0632 0.0053 0.0037
C 210.625 0.00 0.0 0.0 0.1035 0.0632 0.0053 0.0037
C 209.375 0.00 0.0 0.0 0.1034 0.0632 0.0053 0.0037
C 208.125 0.00 0.0 0.0 0.1032 0.0632 0.0053 0.0037
C 206.875 0.00 0.0 0.0 0.1030 0.0632 0.0053 0.0037
C 205.625 0.00 0.0 0.0 0.1028 0.0632 0.0053 0.0037
C 204.375 0.00 0.0 0.0 0.1027 0.0632 0.0053 0.0037
C 203.125 0.00 0.0 0.0 0.1025 0.0632 0.0053 0.0037
C 201.875 0.00 0.0 0.0 0.1023 0.0632 0.0053 0.0037
C 200.625 0.00 0.0 0.0 0.1021 0.0632 0.0053 0.0037
C 199.375 0.00 0.0 0.0 0.1019 0.0632 0.0053 0.0037
C 198.125 0.00 0.0 0.0 0.1017 0.0632 0.0053 0.0037
C 196.875 0.00 0.0 0.0 0.1016 0.0632 0.0053 0.0037
C 195.625 0.00 0.0 0.0 0.1014 0.0632 0.0053 0.0037
C 194.375 0.00 0.0 0.0 0.1012 0.0632 0.0053 0.0037
C 193.125 0.00 0.0 0.0 0.1010 0.0632 0.0053 0.0036
C 191.875 0.00 0.0 0.0 0.1008 0.0632 0.0053 0.0036
C 190.625 0.00 0.0 0.0 0.1006 0.0632 0.0053 0.0036
C 189.375 0.00 0.0 0.0 0.1004 0.0632 0.0053 0.0036
C 188.125 0.00 0.0 0.0 0.1003 0.0632 0.0053 0.0036
C 186.875 0.00 0.0 0.0 0.1001 0.0632 0.0053 0.0036
C 185.625 0.00 0.0 0.0 0.0999 0.0632 0.0053 0.0036
C 184.375 0.00 0.0 0.0 0.0997 0.0632 0.0053 0.0036
C 183.125 0.00 0.0 0.0 0.0995 0.0632 0.0053 0.0036
C 181.875 0.00 0.0 0.0 0.0993 0.0632 0.0053 0.0036
C 180.625 0.00 0.0 0.0 0.0991 0.0632 0.0053 0.0036
C 179.375 0.00 0.0 0.0 0.0989 0.0632 0.0053 0.0036
C 178.125 0.00 0.0 0.0 0.0987 0.0632 0.0053 0.0036
C 176.875 0.00 0.0 0.0 0.0985 0.0632 0.0053 0.0036
C 175.625 0.00 0.0 0.0 0.0983 0.0632 0.0053 0.0035
C 174.375 0.00 0.0 0.0 0.0981 0.0632 0.0053 0.0035
C 173.125 0.00 0.0 0.0 0.0979 0.0632 0.0053 0.0035
C 171.875 0.00 0.0 0.0 0.0977 0.0632 0.0053 0.0035
C 170.625 0.00 0.0 0.0 0.0975 0.0632 0.0053 0.0035
C 169.375 0.00 0.0 0.0 0.0973 0.0632 0.0053 0.0035
C 168.125 0.00 0.0 0.0 0.0971 0.0632 0.0053 0.0035
C 166.875 0.00 0.0 0.0 0.0969 0.0632 0.0053 0.0035
C 165.625 0.00 0.0 0.0 0.0967 0.0632 0.0053 0.0035
C 164.375 0.00 0.0 0.0 0.0965 0.0632 0.0053 0.0035
C 163.125 0.00 0.0 0.0 0.0962 0.0632 0.0053 0.0035
C 161.875 0.00 0.0 0.0 0.0960 0.0632 0.0053 0.0035
C 160.625 0.00 0.0 0.0 0.0958 0.0632 0.0053 0.0035
C 159.167 0.00 0.0 0.0 0.1531 0.1529 0.0070 0.0046
C 157.501 0.00 0.0 0.0 0.1527 0.1529 0.0070 0.0045
C 155.835 0.00 0.0 0.0 0.1522 0.1529 0.0070 0.0045
C 154.169 0.00 0.0 0.0 0.1517 0.1529 0.0070 0.0045
C 152.503 0.00 0.0 0.0 0.1513 0.1529 0.0070 0.0045
C 150.837 0.00 0.0 0.0 0.1591 0.1537 0.0073 0.0013
C 149.171 0.00 0.0 0.0 0.1642 0.1542 0.0075 -0.0009
C 147.505 0.00 0.0 0.0 0.1637 0.1542 0.0075 -0.0009
C 145.839 0.00 0.0 0.0 0.1632 0.1542 0.0075 -0.0009
C 144.173 0.00 0.0 0.0 0.1626 0.1542 0.0075 -0.0009
C 142.507 0.00 0.0 0.0 0.1621 0.1542 0.0075 -0.0009
C 140.841 0.00 0.0 0.0 0.1616 0.1542 0.0075 -0.0009
C 139.175 0.00 0.0 0.0 0.1610 0.1542 0.0075 -0.0008
C 137.509 0.00 0.0 0.0 0.1605 0.1542 0.0075 -0.0008
C 135.843 0.00 0.0 0.0 0.1599 0.1542 0.0075 -0.0008
C 134.177 0.00 0.0 0.0 0.1593 0.1542 0.0075 -0.0008
C 132.511 0.00 0.0 0.0 0.1588 0.1542 0.0075 -0.0008
C 130.845 0.00 0.0 0.0 0.1626 0.1546 0.0076 -0.0035
C 129.179 0.00 0.0 0.0 0.1650 0.1548 0.0077 -0.0053
C 127.513 0.00 0.0 0.0 0.1644 0.1548 0.0077 -0.0053
C 125.847 0.00 0.0 0.0 0.1638 0.1548 0.0077 -0.0053
C 124.181 0.00 0.0 0.0 0.1631 0.1548 0.0077 -0.0052
C 122.515 0.00 0.0 0.0 0.1625 0.1548 0.0077 -0.0052
C 120.841 0.00 0.0 0.0 0.1632 0.1557 0.0077 -0.0052
C 119.375 0.00 0.0 0.0 0.1061 0.0755 0.0058 -0.0039
C 118.125 0.00 0.0 0.0 0.1057 0.0755 0.0058 -0.0039
C 116.875 0.00 0.0 0.0 0.1054 0.0755 0.0058 -0.0039
C 115.625 0.00 0.0 0.0 0.1051 0.0755 0.0058 -0.0039
C 114.375 0.00 0.0 0.0 0.1048 0.0755 0.0058 -0.0039
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C 79.375 0.00 0.0 0.0 0.0944 0.0755 0.0058 -0.0035
C 78.125 0.00 0.0 0.0 0.0940 0.0755 0.0058 -0.0035
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C 74.375 0.00 0.0 0.0 0.0926 0.0755 0.0058 -0.0034
C 73.125 0.00 0.0 0.0 0.0922 0.0755 0.0058 -0.0034
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C 61.875 0.00 0.0 0.0 0.0879 0.0755 0.0058 -0.0032
C 60.625 0.00 0.0 0.0 0.0874 0.0755 0.0058 -0.0032
C 59.375 0.00 0.0 0.0 0.0869 0.0755 0.0058 -0.0032
C 58.125 0.00 0.0 0.0 0.0863 0.0755 0.0058 -0.0032
C 56.875 0.00 0.0 0.0 0.0858 0.0755 0.0058 -0.0032
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C 54.375 0.00 0.0 0.0 0.0847 0.0755 0.0058 -0.0031
C 53.125 0.00 0.0 0.0 0.0842 0.0755 0.0058 -0.0031
C 51.875 0.00 0.0 0.0 0.0836 0.0755 0.0058 -0.0031
C 50.625 0.00 0.0 0.0 0.0830 0.0755 0.0058 -0.0031
C 49.375 0.00 0.0 0.0 0.0824 0.0755 0.0058 -0.0030
C 48.125 0.00 0.0 0.0 0.0818 0.0755 0.0058 -0.0030
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C 43.125 0.00 0.0 0.0 0.0793 0.0755 0.0058 -0.0029
C 41.875 0.00 0.0 0.0 0.0786 0.0755 0.0058 -0.0029
C 40.625 0.00 0.0 0.0 0.0779 0.0755 0.0058 -0.0029
C 39.375 0.00 0.0 0.0 0.0773 0.0755 0.0058 -0.0029
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C 33.125 0.00 0.0 0.0 0.0735 0.0755 0.0058 -0.0027
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C 30.625 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 29.375 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 28.125 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 26.875 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 25.625 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
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C 21.875 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 20.625 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 19.375 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 18.125 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 16.875 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 15.625 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 14.375 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 13.125 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 11.875 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 10.625 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 9.375 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 8.125 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 6.875 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 5.625 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 4.375 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 3.125 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 1.875 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
C 0.625 0.00 0.0 0.0 0.0734 0.0755 0.0058 -0.0027
LOADS DUE TO LADDER
===================
LOAD ELEV APPLY..LOAD..AT LOAD ......FORCES...... ......MOMENTS.....
TYPE RADIUS AZI AZI HORIZ DOWN VERTICAL TORSNAL
ft ft kip kip ft-kip ft-kip
D 300.000 0.00 0.0 0.0 0.0265 0.0053 0.0036 0.0000
D 261.682 0.00 0.0 0.0 0.0255 0.0053 0.0036 0.0000
D 261.682 0.00 0.0 0.0 0.0257 0.0053 0.0036 0.0000
D 160.000 0.00 0.0 0.0 0.0226 0.0053 0.0036 0.0000
D 160.000 0.00 0.0 0.0 0.0221 0.0053 0.0036 0.0000
D 120.000 0.00 0.0 0.0 0.0204 0.0053 0.0036 0.0000
D 120.000 0.00 0.0 0.0 0.0199 0.0053 0.0036 0.0000
D 0.000 0.00 0.0 0.0 0.0138 0.0053 0.0036 0.0000
LOADS DUE TO TRANSMISSION LINES
===============================
LOAD ELEV APPLY..LOAD..AT LOAD ......FORCES...... ......MOMENTS.....
TYPE RADIUS AZI AZI HORIZ DOWN VERTICAL TORSNAL
ft ft kip kip ft-kip ft-kip
D 300.000 0.00 0.0 180.0 0.0000 0.0000 0.0000 0.0000
D 288.338 0.00 0.0 180.0 0.0000 0.0000 0.0000 0.0000
D 288.338 0.00 0.0 0.0 0.0017 0.0001 0.0001 0.0006
D 286.672 0.00 0.0 0.0 0.0017 0.0001 0.0001 0.0006
D 286.672 0.00 0.0 0.0 0.0084 0.0005 0.0003 0.0032
D 273.344 0.00 0.0 0.0 0.0083 0.0005 0.0003 0.0032
D 273.344 0.00 0.0 0.0 0.0106 0.0007 0.0003 0.0032
D 271.678 0.00 0.0 0.0 0.0106 0.0007 0.0003 0.0032
D 271.678 0.00 0.0 0.0 0.0199 0.0015 0.0005 0.0032
D 261.682 0.00 0.0 0.0 0.0198 0.0015 0.0005 0.0032
D 261.682 0.00 0.0 0.0 0.0198 0.0015 0.0005 0.0032
D 236.250 0.00 0.0 0.0 0.0195 0.0015 0.0005 0.0031
D 236.250 0.00 0.0 0.0 0.0238 0.0019 0.0006 0.0031
D 235.000 0.00 0.0 0.0 0.0238 0.0019 0.0006 0.0031
D 235.000 0.00 0.0 0.0 0.0250 0.0020 0.0007 0.0031
D 160.000 0.00 0.0 0.0 0.0224 0.0020 0.0007 0.0028
D 160.000 0.00 0.0 0.0 0.0221 0.0020 0.0007 0.0027
D 151.670 0.00 0.0 0.0 0.0218 0.0020 0.0007 0.0027
D 151.670 0.00 0.0 0.0 0.0268 0.0025 0.0008 0.0008
D 150.004 0.00 0.0 0.0 0.0268 0.0025 0.0008 0.0008
D 150.004 0.00 0.0 0.0 0.0301 0.0029 0.0009 -0.0005
D 131.678 0.00 0.0 0.0 0.0291 0.0029 0.0009 -0.0005
D 131.678 0.00 0.0 0.0 0.0316 0.0031 0.0010 -0.0021
D 130.012 0.00 0.0 0.0 0.0316 0.0031 0.0010 -0.0021
D 130.012 0.00 0.0 0.0 0.0333 0.0032 0.0011 -0.0032
D 121.682 0.00 0.0 0.0 0.0328 0.0032 0.0011 -0.0031
D 121.682 0.00 0.0 0.0 0.0319 0.0032 0.0011 -0.0030
D 0.000 0.00 0.0 0.0 0.0222 0.0032 0.0011 -0.0021
LOADS DUE TO OTHER MOUNTINGS
============================
LOAD ELEV APPLY..LOAD..AT LOAD ......FORCES...... ......MOMENTS.....
TYPE RADIUS AZI AZI HORIZ DOWN VERTICAL TORSNAL
ft ft kip kip ft-kip ft-kip
C 300.000 0.00 0.0 0.0 0.0467 0.0109 0.0000 0.0000
C 287.000 1.55 342.6 0.0 0.2125 0.1285 0.0000 0.0107
C 280.000 0.00 300.6 0.0 1.2568 0.9115 0.0000 0.0000
C 272.000 0.80 30.0 0.0 0.3633 0.2350 0.0000 0.0149
C 236.000 1.46 100.5 0.0 0.1479 0.1065 0.0000 0.0235
C 151.000 1.46 220.5 0.0 0.2248 0.1065 0.0000 0.0627
C 140.000 0.00 300.6 0.0 1.0310 0.9115 0.0000 0.0000
C 131.000 2.00 230.0 0.0 0.0566 0.0441 0.0000 0.0000
LOADS DUE TO MICROWAVE PARABOLIC ANTENNAS
=========================================
.........ANTENNA......... .ATTACHMENT. ........ANTENNA FORCES..........
TYPE SIZE ELEV AZIM RADIUS AZIM AXIAL SHEAR GRAVITY TORSION
ft ft deg ft deg kip kip kip ft-kip
STD+R 10.0 287.000 296. 2.45 0. 1.52 1.97 0.44 0.81
HP 10.0 272.000 105. 2.45 120. -1.76 -2.26 0.54 -4.52
HP 8.0 272.000 296. 2.45 0. 2.14 1.05 0.45 0.08
HP 10.0 236.000 105. 2.45 120. -1.69 -2.17 0.54 -4.35
STD 10.0 151.000 241. 2.45 240. -1.54 1.53 0.34 4.80
INDIVIDUAL ELEMENT LOADS
========================
TYPE MATERIAL ......BARE LOADS..... ...CURRENT LOADING...
NO TYPE GRAVITY WIND AREA GRAVITY WIND AREA
plf ft.sq/ft plf ft.sq/ft
1 sr 13.806 0.188 13.806 0.225
2 sr 10.908 0.167 10.908 0.200
3 sr 1.534 0.063 1.534 0.075
4 sr 2.727 0.083 2.727 0.100
5 sr 0.682 0.042 0.682 0.050
6 sch40 1.953 0.240 1.953 0.287
7 c 4.998 0.167 4.998 0.333
8 sch40 10.934 1.063 10.934 1.275
9 l 6.727 0.333 6.727 0.667
10 sch40 11.021 0.375 11.021 0.450
11 sch40 7.752 0.552 7.752 0.663
12 l 10.851 0.292 10.851 0.583
13 RHSS 5.510 0.240 5.510 0.287
14 sch40 1.953 0.240 1.953 0.287
15 sch40 0.916 0.158 0.916 0.190
ewp63 0.510 0.168 0.510 0.166
ewp63 1.020 0.193 1.020 0.232
ewp63 0.510 0.168 0.510 0.116
fh1.625 0.820 0.165 0.820 0.198
fh0.875 0.330 0.091 0.330 0.109
================================================================================
LOADING CONDITION B ========================================================
Bare tower 100 mph wind at azimuth 90 deg
WIND LOADING
============
.....WIND LOADING..... ...ICE LOADING.. .....TYPE OF..... ....FACTORS.....
AZI SPEED REF.VEL. RADIUS DENSITY EXP STD ANT WIND DEAD ICE
PRESS. LOAD LOAD LOAD LOAD
deg mph psf in pcf * & #
90.0 100.00 0.00 0.00 56.20 1 1 1 1.00 1.00 1.00
* Type of Exposure : 1 - Wind profile (Kz) based on EIA 222 F (June 1996)
2 - Wind profile Kz = 1 ; Gh = 1
3 - Wind profile (Kz) based on EIA 222 C (Mar.1976)
4 - Wind factors supplied by user ( Gh=1, step function)
5 - Wind profile UBC (May.1988) Exposure C
6 - Wind profile UBC (May.1988) Exposure B
7 - Wind profile Site Specific Wind Formula
& Type of Standard : 1 - EIA - 222 F ( June 1996 )
2 - EIA - 222 C ( March 1976 )
3 - UBC - 88 ( May 1 1988 )
# Type of Antenna load :
1 - Antenna forces for this wind direction
2 - Maximum possible forces regardless of
wind direction
SUPPRESS PRINTING
=================
....LOAD SUMMARY FOR.... ................LOAD COMPONENTS....................
MAST GUYMAST PANEL PANELS LADDERS TX-LINES DISCRETE INDIVIDUAL
POINTS APPURTENANCES ELEMENTS
yes no yes yes no no no no
GUYMAST LOADING
===============
LOAD ELEV .....FORCES (kip)...... ...MOMENTS (ft.kips)... ANTENNA
TYPE ft NORTH EAST DOWN NORTH EAST TORSION AZIMUTH
D 300.000 0.0000 -0.0696 0.0810 -0.0036 0.0000 -0.0093
D 288.338 0.0000 -0.0689 0.0810 -0.0036 0.0000 -0.0092
D 288.338 0.0000 -0.0703 0.0811 -0.0036 0.0000 -0.0096
D 286.672 0.0000 -0.0703 0.0811 -0.0036 0.0000 -0.0096
D 286.672 0.0000 -0.0764 0.0815 -0.0038 -0.0002 -0.0116
D 273.344 0.0000 -0.0755 0.0815 -0.0038 -0.0002 -0.0115
D 273.344 0.0000 -0.0773 0.0817 -0.0038 -0.0002 -0.0120
D 271.678 0.0000 -0.0773 0.0817 -0.0038 -0.0002 -0.0120
D 271.678 0.0000 -0.0853 0.0826 -0.0041 -0.0002 -0.0145
D 261.682 0.0000 -0.0845 0.0826 -0.0041 -0.0002 -0.0143
D 261.682 0.0000 -0.0842 0.0822 -0.0041 -0.0002 -0.0143
D 260.000 0.0000 -0.0842 0.0822 -0.0041 -0.0002 -0.0143
D 260.000 0.0000 -0.0686 0.0501 -0.0041 -0.0002 -0.0144
D 236.250 0.0000 -0.0668 0.0501 -0.0041 -0.0002 -0.0140
D 236.250 0.0000 -0.0745 0.0505 -0.0042 -0.0002 -0.0164
D 235.000 0.0000 -0.0745 0.0505 -0.0042 -0.0002 -0.0164
D 235.000 0.0000 -0.0765 0.0506 -0.0042 -0.0002 -0.0170
D 160.000 0.0000 -0.0687 0.0506 -0.0042 -0.0002 -0.0152
D 160.000 0.0000 -0.0839 0.0918 -0.0042 -0.0002 -0.0150
D 151.670 0.0000 -0.0829 0.0918 -0.0042 -0.0002 -0.0148
D 151.670 0.0000 -0.0876 0.0923 -0.0044 0.0000 -0.0164
D 150.004 0.0000 -0.0876 0.0923 -0.0044 0.0000 -0.0164
D 150.004 0.0000 -0.0907 0.0926 -0.0045 0.0001 -0.0174
D 131.678 0.0000 -0.0877 0.0926 -0.0045 0.0001 -0.0168
D 131.678 0.0000 -0.0900 0.0928 -0.0045 0.0002 -0.0177
D 130.012 0.0000 -0.0900 0.0928 -0.0045 0.0002 -0.0177
D 130.012 0.0000 -0.0915 0.0929 -0.0046 0.0003 -0.0183
D 121.682 0.0000 -0.0901 0.0929 -0.0046 0.0003 -0.0180
D 121.682 0.0000 -0.0896 0.0926 -0.0046 0.0003 -0.0179
D 120.000 0.0000 -0.0896 0.0926 -0.0046 0.0003 -0.0179
D 120.000 0.0000 -0.0751 0.0604 -0.0046 0.0003 -0.0175
D 0.000 0.0000 -0.0520 0.0604 -0.0046 0.0003 -0.0121
C 300.000 0.0000 -0.0467 0.0109 0.0000 0.0000 0.0000
C 287.000 0.0000 -0.2883 0.1285 0.1904 -0.0596 0.4630
C 280.000 0.0000 -1.2568 0.9115 0.0000 0.0000 1.1311
C 272.000 0.0000 -0.5126 0.2350 0.1619 0.0937 0.3546
C 236.000 0.0000 -0.2196 0.1065 -0.0285 0.1533 -0.0854
C 151.000 0.0000 -0.0987 0.1065 -0.1185 -0.1013 -0.0928
C 140.000 0.0000 -1.0310 0.9115 0.0000 0.0000 0.9279
C 131.000 0.0000 -0.0566 0.0441 -0.0567 -0.0675 -0.0727
C 287.000 0.0536 -2.4672 0.4420 1.0829 0.0000 7.6994 296.
C 272.000 0.7711 -4.9883 0.5410 -0.6627 1.1479 -3.0075 105.
C 272.000 0.3505 -1.1994 0.4470 1.0951 0.0000 3.4963 296.
C 236.000 0.7404 -4.7900 0.5410 -0.6627 1.1479 -2.8880 105.
C 151.000 -0.1567 -2.9358 0.3420 -0.4189 -0.7256 -6.8468 241.
LOADS DUE TO LADDER
===================
LOAD ELEV APPLY..LOAD..AT LOAD ......FORCES...... ......MOMENTS.....
TYPE RADIUS AZI AZI HORIZ DOWN VERTICAL TORSNAL
ft ft kip kip ft-kip ft-kip
D 300.000 0.00 0.0 90.0 0.0148 0.0053 0.0036 -0.0093
D 261.682 0.00 0.0 90.0 0.0143 0.0053 0.0036 -0.0089
D 261.682 0.00 0.0 90.0 0.0144 0.0053 0.0036 -0.0090
D 160.000 0.00 0.0 90.0 0.0126 0.0053 0.0036 -0.0079
D 160.000 0.00 0.0 90.0 0.0124 0.0053 0.0036 -0.0077
D 120.000 0.00 0.0 90.0 0.0115 0.0053 0.0036 -0.0072
D 120.000 0.00 0.0 90.0 0.0112 0.0053 0.0036 -0.0070
D 0.000 0.00 0.0 90.0 0.0077 0.0053 0.0036 -0.0048
LOADS DUE TO TRANSMISSION LINES
===============================
LOAD ELEV APPLY..LOAD..AT LOAD ......FORCES...... ......MOMENTS.....
TYPE RADIUS AZI AZI HORIZ DOWN VERTICAL TORSNAL
ft ft kip kip ft-kip ft-kip
D 300.000 0.00 0.0 180.0 0.0000 0.0000 0.0000 0.0000
D 288.338 0.00 0.0 180.0 0.0000 0.0000 0.0000 0.0000
D 288.338 0.00 0.0 90.0 0.0015 0.0001 0.0001 -0.0005
D 286.672 0.00 0.0 90.0 0.0015 0.0001 0.0001 -0.0005
D 286.672 0.00 0.0 90.0 0.0077 0.0005 0.0003 -0.0025
D 273.344 0.00 0.0 90.0 0.0076 0.0005 0.0003 -0.0024
D 273.344 0.00 0.0 90.0 0.0095 0.0007 0.0003 -0.0030
D 271.678 0.00 0.0 90.0 0.0095 0.0007 0.0003 -0.0030
D 271.678 0.00 0.0 90.0 0.0176 0.0015 0.0005 -0.0055
D 261.682 0.00 0.0 90.0 0.0175 0.0015 0.0005 -0.0054
D 261.682 0.00 0.0 90.0 0.0175 0.0015 0.0005 -0.0054
D 236.250 0.00 0.0 90.0 0.0172 0.0015 0.0005 -0.0053
D 236.250 0.00 0.0 90.0 0.0249 0.0019 0.0006 -0.0076
D 235.000 0.00 0.0 90.0 0.0249 0.0019 0.0006 -0.0076
D 235.000 0.00 0.0 90.0 0.0269 0.0020 0.0007 -0.0082
D 160.000 0.00 0.0 90.0 0.0242 0.0020 0.0007 -0.0074
D 160.000 0.00 0.0 90.0 0.0238 0.0020 0.0007 -0.0073
D 151.670 0.00 0.0 90.0 0.0235 0.0020 0.0007 -0.0072
D 151.670 0.00 0.0 90.0 0.0285 0.0025 0.0008 -0.0088
D 150.004 0.00 0.0 90.0 0.0285 0.0025 0.0008 -0.0088
D 150.004 0.00 0.0 90.0 0.0317 0.0029 0.0009 -0.0098
D 131.678 0.00 0.0 90.0 0.0307 0.0029 0.0009 -0.0095
D 131.678 0.00 0.0 90.0 0.0332 0.0031 0.0010 -0.0104
D 130.012 0.00 0.0 90.0 0.0332 0.0031 0.0010 -0.0104
D 130.012 0.00 0.0 90.0 0.0349 0.0032 0.0011 -0.0110
D 121.682 0.00 0.0 90.0 0.0343 0.0032 0.0011 -0.0108
D 121.682 0.00 0.0 90.0 0.0334 0.0032 0.0011 -0.0105
D 0.000 0.00 0.0 90.0 0.0233 0.0032 0.0011 -0.0073
LOADS DUE TO OTHER MOUNTINGS
============================
LOAD ELEV APPLY..LOAD..AT LOAD ......FORCES...... ......MOMENTS.....
TYPE RADIUS AZI AZI HORIZ DOWN VERTICAL TORSNAL
ft ft kip kip ft-kip ft-kip
C 300.000 0.00 0.0 90.0 0.0467 0.0109 0.0000 0.0000
C 287.000 1.55 342.6 90.0 0.2883 0.1285 0.0000 0.0360
C 280.000 0.00 300.6 90.0 1.2568 0.9115 0.0000 1.1311
C 272.000 0.80 30.0 90.0 0.5126 0.2350 0.0000 0.0014
C 236.000 1.46 100.5 90.0 0.2196 0.1065 0.0000 -0.0266
C 151.000 1.46 220.5 90.0 0.0987 0.1065 0.0000 0.0170
C 140.000 0.00 300.6 90.0 1.0310 0.9115 0.0000 0.9279
C 131.000 2.00 230.0 90.0 0.0566 0.0441 0.0000 0.0000
LOADS DUE TO MICROWAVE PARABOLIC ANTENNAS
=========================================
.........ANTENNA......... .ATTACHMENT. ........ANTENNA FORCES..........
TYPE SIZE ELEV AZIM RADIUS AZIM AXIAL SHEAR GRAVITY TORSION
ft ft deg ft deg kip kip kip ft-kip
STD+R 10.0 287.000 296. 2.45 0. -2.24 1.03 0.44 1.65
HP 10.0 272.000 105. 2.45 120. 5.02 -0.55 0.54 1.47
HP 8.0 272.000 296. 2.45 0. -1.23 0.21 0.45 0.56
HP 10.0 236.000 105. 2.45 120. 4.82 -0.52 0.54 1.41
STD 10.0 151.000 241. 2.45 240. -2.64 -1.29 0.34 -3.58
INDIVIDUAL ELEMENT LOADS
========================
TYPE MATERIAL ......BARE LOADS..... ...CURRENT LOADING...
NO TYPE GRAVITY WIND AREA GRAVITY WIND AREA
plf ft.sq/ft plf ft.sq/ft
1 sr 13.806 0.188 13.806 0.225
2 sr 10.908 0.167 10.908 0.200
3 sr 1.534 0.063 1.534 0.075
4 sr 2.727 0.083 2.727 0.100
5 sr 0.682 0.042 0.682 0.050
6 sch40 1.953 0.240 1.953 0.287
7 c 4.998 0.167 4.998 0.333
8 sch40 10.934 1.063 10.934 1.275
9 l 6.727 0.333 6.727 0.667
10 sch40 11.021 0.375 11.021 0.450
11 sch40 7.752 0.552 7.752 0.663
12 l 10.851 0.292 10.851 0.583
13 RHSS 5.510 0.240 5.510 0.287
14 sch40 1.953 0.240 1.953 0.287
15 sch40 0.916 0.158 0.916 0.190
ewp63 0.510 0.168 0.510 0.151
ewp63 1.020 0.193 1.020 0.201
ewp63 0.510 0.168 0.510 0.201
fh1.625 0.820 0.165 0.820 0.198
fh0.875 0.330 0.091 0.330 0.109
================================================================================
LOADING CONDITION C ========================================================
Bare tower 100 mph wind at azimuth 180 deg
WIND LOADING
============
.....WIND LOADING..... ...ICE LOADING.. .....TYPE OF..... ....FACTORS.....
AZI SPEED REF.VEL. RADIUS DENSITY EXP STD ANT WIND DEAD ICE
PRESS. LOAD LOAD LOAD LOAD
deg mph psf in pcf * & #
180.0 100.00 0.00 0.00 56.20 1 1 1 1.00 1.00 1.00
* Type of Exposure : 1 - Wind profile (Kz) based on EIA 222 F (June 1996)
2 - Wind profile Kz = 1 ; Gh = 1
3 - Wind profile (Kz) based on EIA 222 C (Mar.1976)
4 - Wind factors supplied by user ( Gh=1, step function)
5 - Wind profile UBC (May.1988) Exposure C
6 - Wind profile UBC (May.1988) Exposure B
7 - Wind profile Site Specific Wind Formula
& Type of Standard : 1 - EIA - 222 F ( June 1996 )
2 - EIA - 222 C ( March 1976 )
3 - UBC - 88 ( May 1 1988 )
# Type of Antenna load :
1 - Antenna forces for this wind direction
2 - Maximum possible forces regardless of
wind direction
SUPPRESS PRINTING
=================
....LOAD SUMMARY FOR.... ................LOAD COMPONENTS....................
MAST GUYMAST PANEL PANELS LADDERS TX-LINES DISCRETE INDIVIDUAL
POINTS APPURTENANCES ELEMENTS
no no yes yes no no no no
MAST LOADING
============
LOAD ELEV APPLY..LOAD..AT LOAD ......FORCES...... ......MOMENTS.....
TYPE RADIUS AZI AZI HORIZ DOWN VERTICAL TORSNAL
ft ft kip kip ft-kip ft-kip
D 300.000 0.00 0.0 180.0 0.0812 0.0810 0.0036 0.0000
D 288.338 0.00 0.0 180.0 0.0804 0.0810 0.0036 0.0000
D 288.338 0.00 0.0 180.0 0.0820 0.0811 0.0036 -0.0006
D 286.672 0.00 0.0 180.0 0.0820 0.0811 0.0036 -0.0006
D 286.672 0.00 0.0 180.0 0.0886 0.0815 0.0038 -0.0032
D 273.344 0.00 0.0 180.0 0.0876 0.0815 0.0038 -0.0032
D 273.344 0.00 0.0 180.0 0.0896 0.0817 0.0038 -0.0032
D 271.678 0.00 0.0 180.0 0.0896 0.0817 0.0038 -0.0032
D 271.678 0.00 0.0 180.0 0.0989 0.0826 0.0041 -0.0032
D 261.682 0.00 0.0 180.0 0.0980 0.0826 0.0041 -0.0032
D 261.682 0.00 0.0 180.0 0.0976 0.0822 0.0041 -0.0031
D 260.000 0.00 0.0 180.0 0.0976 0.0822 0.0041 -0.0031
D 260.000 0.00 0.0 180.0 0.0821 0.0501 0.0041 -0.0032
D 236.250 0.00 0.0 180.0 0.0800 0.0501 0.0041 -0.0031
D 236.250 0.00 0.0 180.0 0.0852 0.0505 0.0042 -0.0031
D 160.000 0.00 0.0 180.0 0.0774 0.0506 0.0042 -0.0028
D 160.000 0.00 0.0 180.0 0.0919 0.0918 0.0042 -0.0027
D 151.670 0.00 0.0 180.0 0.0908 0.0918 0.0042 -0.0027
D 151.670 0.00 0.0 180.0 0.0955 0.0923 0.0044 -0.0008
D 150.004 0.00 0.0 180.0 0.0955 0.0923 0.0044 -0.0008
D 150.004 0.00 0.0 180.0 0.0986 0.0926 0.0045 0.0005
D 131.678 0.00 0.0 180.0 0.0953 0.0926 0.0045 0.0005
D 131.678 0.00 0.0 180.0 0.0976 0.0928 0.0046 0.0021
D 130.012 0.00 0.0 180.0 0.0976 0.0928 0.0046 0.0021
D 130.012 0.00 0.0 180.0 0.0990 0.0929 0.0046 0.0032
D 121.682 0.00 0.0 180.0 0.0975 0.0929 0.0046 0.0031
D 121.682 0.00 0.0 180.0 0.0970 0.0926 0.0046 0.0031
D 120.000 0.00 0.0 180.0 0.0970 0.0926 0.0046 0.0031
D 120.000 0.00 0.0 180.0 0.0823 0.0604 0.0046 0.0030
D 0.000 0.00 0.0 180.0 0.0570 0.0604 0.0046 0.0021
C 300.000 0.00 0.0 180.0 0.0467 0.0109 0.0000 0.0000
C 287.000 1.55 342.6 180.0 0.2125 0.1285 0.0000 -0.0107
C 280.000 0.00 300.6 180.0 1.2568 0.9115 0.0000 0.0000
C 272.000 0.80 30.0 180.0 0.3633 0.2350 0.0000 -0.0149
C 236.000 1.46 100.5 180.0 0.1479 0.1065 0.0000 -0.0235
C 151.000 1.46 220.5 180.0 0.2248 0.1065 0.0000 -0.0627
C 140.000 0.00 300.6 180.0 1.0310 0.9115 0.0000 0.0000
C 131.000 2.00 230.0 180.0 0.0566 0.0441 0.0000 0.0000
GUYMAST LOADING
===============
LOAD ELEV .....FORCES (kip)...... ...MOMENTS (ft.kips)... ANTENNA
TYPE ft NORTH EAST DOWN NORTH EAST TORSION AZIMUTH
D 300.000 0.0812 0.0000 0.0810 -0.0036 0.0000 0.0000
D 288.338 0.0804 0.0000 0.0810 -0.0036 0.0000 0.0000
D 288.338 0.0820 0.0000 0.0811 -0.0036 0.0000 -0.0006
D 286.672 0.0820 0.0000 0.0811 -0.0036 0.0000 -0.0006
D 286.672 0.0886 0.0000 0.0815 -0.0038 -0.0002 -0.0032
D 273.344 0.0876 0.0000 0.0815 -0.0038 -0.0002 -0.0032
D 273.344 0.0896 0.0000 0.0817 -0.0038 -0.0002 -0.0032
D 271.678 0.0896 0.0000 0.0817 -0.0038 -0.0002 -0.0032
D 271.678 0.0989 0.0000 0.0826 -0.0041 -0.0002 -0.0032
D 261.682 0.0980 0.0000 0.0826 -0.0041 -0.0002 -0.0032
D 261.682 0.0976 0.0000 0.0822 -0.0041 -0.0002 -0.0031
D 260.000 0.0976 0.0000 0.0822 -0.0041 -0.0002 -0.0031
D 260.000 0.0821 0.0000 0.0501 -0.0041 -0.0002 -0.0032
D 236.250 0.0800 0.0000 0.0501 -0.0041 -0.0002 -0.0031
D 236.250 0.0852 0.0000 0.0505 -0.0042 -0.0002 -0.0031
D 160.000 0.0774 0.0000 0.0506 -0.0042 -0.0002 -0.0028
D 160.000 0.0919 0.0000 0.0918 -0.0042 -0.0002 -0.0027
D 151.670 0.0908 0.0000 0.0918 -0.0042 -0.0002 -0.0027
D 151.670 0.0955 0.0000 0.0923 -0.0044 0.0000 -0.0008
D 150.004 0.0955 0.0000 0.0923 -0.0044 0.0000 -0.0008
D 150.004 0.0986 0.0000 0.0926 -0.0045 0.0001 0.0005
D 131.678 0.0953 0.0000 0.0926 -0.0045 0.0001 0.0005
D 131.678 0.0976 0.0000 0.0928 -0.0045 0.0002 0.0021
D 130.012 0.0976 0.0000 0.0928 -0.0045 0.0002 0.0021
D 130.012 0.0990 0.0000 0.0929 -0.0046 0.0003 0.0032
D 121.682 0.0975 0.0000 0.0929 -0.0046 0.0003 0.0031
D 121.682 0.0970 0.0000 0.0926 -0.0046 0.0003 0.0031
D 120.000 0.0970 0.0000 0.0926 -0.0046 0.0003 0.0031
D 120.000 0.0823 0.0000 0.0604 -0.0046 0.0003 0.0030
D 0.000 0.0570 0.0000 0.0604 -0.0046 0.0003 0.0021
C 300.000 0.0467 0.0000 0.0109 0.0000 0.0000 0.0000
C 287.000 0.2125 0.0000 0.1285 0.1904 -0.0596 -0.1093
C 280.000 1.2568 0.0000 0.9115 0.0000 0.0000 0.0000
C 272.000 0.3633 0.0000 0.2350 0.1619 0.0937 0.1299
C 236.000 0.1479 0.0000 0.1065 -0.0285 0.1533 0.1894
C 151.000 0.2248 0.0000 0.1065 -0.1185 -0.1013 -0.2766
C 140.000 1.0310 0.0000 0.9115 0.0000 0.0000 0.0000
C 131.000 0.0566 0.0000 0.0441 -0.0567 -0.0675 -0.0867
C 287.000 1.5243 0.1792 0.4420 1.0829 0.0000 -6.9561 296.
C 272.000 2.5316 -1.2768 0.5410 -0.6627 1.1479 5.6490 105.
C 272.000 1.8080 -0.9416 0.4470 1.0951 0.0000 0.1026 296.
C 236.000 2.4310 -1.2261 0.5410 -0.6627 1.1479 5.4245 105.
C 151.000 3.4317 4.3543 0.3420 -0.4189 -0.7256 0.7267 241.
LOADS DUE TO LADDER
===================
LOAD ELEV APPLY..LOAD..AT LOAD ......FORCES...... ......MOMENTS.....
TYPE RADIUS AZI AZI HORIZ DOWN VERTICAL TORSNAL
ft ft kip kip ft-kip ft-kip
D 300.000 0.00 0.0 180.0 0.0265 0.0053 0.0036 0.0000
D 261.682 0.00 0.0 180.0 0.0255 0.0053 0.0036 0.0000
D 261.682 0.00 0.0 180.0 0.0257 0.0053 0.0036 0.0000
D 160.000 0.00 0.0 180.0 0.0226 0.0053 0.0036 0.0000
D 160.000 0.00 0.0 180.0 0.0221 0.0053 0.0036 0.0000
D 120.000 0.00 0.0 180.0 0.0204 0.0053 0.0036 0.0000
D 120.000 0.00 0.0 180.0 0.0199 0.0053 0.0036 0.0000
D 0.000 0.00 0.0 180.0 0.0138 0.0053 0.0036 0.0000
LOADS DUE TO TRANSMISSION LINES
===============================
LOAD ELEV APPLY..LOAD..AT LOAD ......FORCES...... ......MOMENTS.....
TYPE RADIUS AZI AZI HORIZ DOWN VERTICAL TORSNAL
ft ft kip kip ft-kip ft-kip
D 300.000 0.00 0.0 180.0 0.0000 0.0000 0.0000 0.0000
D 288.338 0.00 0.0 180.0 0.0000 0.0000 0.0000 0.0000
D 288.338 0.00 0.0 180.0 0.0017 0.0001 0.0001 -0.0006
D 286.672 0.00 0.0 180.0 0.0017 0.0001 0.0001 -0.0006
D 286.672 0.00 0.0 180.0 0.0084 0.0005 0.0003 -0.0032
D 273.344 0.00 0.0 180.0 0.0083 0.0005 0.0003 -0.0032
D 273.344 0.00 0.0 180.0 0.0106 0.0007 0.0003 -0.0032
D 271.678 0.00 0.0 180.0 0.0106 0.0007 0.0003 -0.0032
D 271.678 0.00 0.0 180.0 0.0199 0.0015 0.0005 -0.0032
D 261.682 0.00 0.0 180.0 0.0198 0.0015 0.0005 -0.0032
D 261.682 0.00 0.0 180.0 0.0198 0.0015 0.0005 -0.0032
D 236.250 0.00 0.0 180.0 0.0195 0.0015 0.0005 -0.0031
D 236.250 0.00 0.0 180.0 0.0238 0.0019 0.0006 -0.0031
D 235.000 0.00 0.0 180.0 0.0238 0.0019 0.0006 -0.0031
D 235.000 0.00 0.0 180.0 0.0250 0.0020 0.0007 -0.0031
D 160.000 0.00 0.0 180.0 0.0224 0.0020 0.0007 -0.0028
D 160.000 0.00 0.0 180.0 0.0221 0.0020 0.0007 -0.0027
D 151.670 0.00 0.0 180.0 0.0218 0.0020 0.0007 -0.0027
D 151.670 0.00 0.0 180.0 0.0268 0.0025 0.0008 -0.0008
D 150.004 0.00 0.0 180.0 0.0268 0.0025 0.0008 -0.0008
D 150.004 0.00 0.0 180.0 0.0301 0.0029 0.0009 0.0005
D 131.678 0.00 0.0 180.0 0.0291 0.0029 0.0009 0.0005
D 131.678 0.00 0.0 180.0 0.0316 0.0031 0.0010 0.0021
D 130.012 0.00 0.0 180.0 0.0316 0.0031 0.0010 0.0021
D 130.012 0.00 0.0 180.0 0.0333 0.0032 0.0011 0.0032
D 121.682 0.00 0.0 180.0 0.0328 0.0032 0.0011 0.0031
D 121.682 0.00 0.0 180.0 0.0319 0.0032 0.0011 0.0030
D 0.000 0.00 0.0 180.0 0.0222 0.0032 0.0011 0.0021
LOADS DUE TO OTHER MOUNTINGS
============================
LOAD ELEV APPLY..LOAD..AT LOAD ......FORCES...... ......MOMENTS.....
TYPE RADIUS AZI AZI HORIZ DOWN VERTICAL TORSNAL
ft ft kip kip ft-kip ft-kip
C 300.000 0.00 0.0 180.0 0.0467 0.0109 0.0000 0.0000
C 287.000 1.55 342.6 180.0 0.2125 0.1285 0.0000 -0.0107
C 280.000 0.00 300.6 180.0 1.2568 0.9115 0.0000 0.0000
C 272.000 0.80 30.0 180.0 0.3633 0.2350 0.0000 -0.0149
C 236.000 1.46 100.5 180.0 0.1479 0.1065 0.0000 -0.0235
C 151.000 1.46 220.5 180.0 0.2248 0.1065 0.0000 -0.0627
C 140.000 0.00 300.6 180.0 1.0310 0.9115 0.0000 0.0000
C 131.000 2.00 230.0 180.0 0.0566 0.0441 0.0000 0.0000
LOADS DUE TO MICROWAVE PARABOLIC ANTENNAS
=========================================
.........ANTENNA......... .ATTACHMENT. ........ANTENNA FORCES..........
TYPE SIZE ELEV AZIM RADIUS AZIM AXIAL SHEAR GRAVITY TORSION
ft ft deg ft deg kip kip kip ft-kip
STD+R 10.0 287.000 296. 2.45 0. -0.51 -1.45 0.44 -6.52
HP 10.0 272.000 105. 2.45 120. 1.89 2.11 0.54 1.84
HP 8.0 272.000 296. 2.45 0. -1.64 -1.21 0.45 -2.20
HP 10.0 236.000 105. 2.45 120. 1.81 2.03 0.54 1.77
STD 10.0 151.000 241. 2.45 240. 5.47 -0.89 0.34 2.67
INDIVIDUAL ELEMENT LOADS
========================
TYPE MATERIAL ......BARE LOADS..... ...CURRENT LOADING...
NO TYPE GRAVITY WIND AREA GRAVITY WIND AREA
plf ft.sq/ft plf ft.sq/ft
1 sr 13.806 0.188 13.806 0.225
2 sr 10.908 0.167 10.908 0.200
3 sr 1.534 0.063 1.534 0.075
4 sr 2.727 0.083 2.727 0.100
5 sr 0.682 0.042 0.682 0.050
6 sch40 1.953 0.240 1.953 0.287
7 c 4.998 0.167 4.998 0.333
8 sch40 10.934 1.063 10.934 1.275
9 l 6.727 0.333 6.727 0.667
10 sch40 11.021 0.375 11.021 0.450
11 sch40 7.752 0.552 7.752 0.663
12 l 10.851 0.292 10.851 0.583
13 RHSS 5.510 0.240 5.510 0.287
14 sch40 1.953 0.240 1.953 0.287
15 sch40 0.916 0.158 0.916 0.190
ewp63 0.510 0.168 0.510 0.166
ewp63 1.020 0.193 1.020 0.232
ewp63 0.510 0.168 0.510 0.116
fh1.625 0.820 0.165 0.820 0.198
fh0.875 0.330 0.091 0.330 0.109
===============================================================================
ORIGINAL DATA FILE :
c:\Documents and Settings\sean\My Documents\Projects\Website\samples\working\de
===============================================================================
line contents
no
1 [DEMOGU] - 300 FT GUYED TOWER ANALYSIS - OCTOBER 2004
2 mast geometry
3 d,3,0,0,120,2.5,2.5,1.25
4 x,3,0,120,160,,,1.666
5 d,3,0,160,260,,,1.25
6 x,3,0,260,300,,,1.666
7 panel properties
8 0,120,1,3,0,0,0,0,0
9 120,160,1,4,4
10 160,260,2,3,0
11 260,300,2,4,4
12 material types
13 sr,1,1,0,2.25,0,0,500 /legs
14 ,2,,,2
15 ,3,,,.75 /diags
16 ,4,,,1
17 ,5,,,.5 /ladder rungs
18 sch40,6,,,2.5,0,0,165 /safety rail
19 c,7,1,0,2,5,.125,.125 /tx support
20 sch40,8,1,0,12,0,0,100 /beacon
21 l,9,1,0,4,4,.25,500 /mw mount angle
22 sch40,10,,,4,0,0 /mw mount pipe
23 sch40,11,2,0,6,0,0,100 /dol
24 l,12,2,0,3.5,3.0,.25,500 /tr member @ EL. 280'
25 RHSS,13,1,0,2.875,0,.188 /pinwheel mount
26 sch40,14,1,0,2.5,0,0,165 /srl480
27 ,15,1,0,1.5 /srl420
28 ladder geometry
29 0,300,10,15,.625,180,90,0,5,6
30 0,300,26,45,.722,180,90,0,7,0 /tx support
31 transmission lines
32 ewp63,0,287,1,0.5,230,230
33 ewp63,0,272,2,0.3,180,90
34 ewp63,0,236,1,0.3,180,180
35 fh1.625,0,151,1,0.5,130,130
36 fh0.875,0,131,1,0.7,120,120
37 other mountings
38 272,9,2,3.0,0.83,300,30,0 /mw mount angle
39 287
40 272,10,1,8,2,350,0,90 /mw pipe
41 287
42 272,9,2,3,.83,60,150,0 /mw mount angle
43 236
44 272,10,1,6,2,110,0,90 /mw pipe
45 236
46 151,9,2,3,.83,180,90,0 /mw angle
47 ,10,1,6,2,230,0,90 /mw pipe
48 131,10,1,4,2,230,0,90 /mw pipe
49 300,8,1,1,0,0,0,90 /beacon
50 140,12,2,14,1.8,120,30,0 /torsion resistors
51 5*,240,150
52 5*,0,90
53 280,4*,120,30
54 5*,240,150
55 5*,0,90
56 MICROWAVE PARABOLIC ANTENNAS
57 std,151,241,10.0,2.45,240,50
58 hp,236,105,10.0,2.45,120,50
59 ,272,296,8.00,2.45,0,50
60 ,272,105,10.0,2.45,120,50
61 std+r,287,296,10.0,2.45,0,50
62 GUY GEOMETRY
63 45,0,GS,0.4375,45,230,1.44,0,1.95,2,120,120
64 90,,,,90
65 140,0,GS,0.5,140,,8.08,60,2.55,2,120,120
66 ,120
67 185,0,GS,0.5,185,,1.44,0,2.55
68 230,,,0.625,230,,,,4.03
69 280,0,BS,0.75,280,,8.08,60,6.80,2,120,120
70 ,120
71 Bare tower 100 mph wind at azimuth 0 deg
72 wind loading
73 0,100,0,0,56.2,1,1,1,1,1,1
74 suppress printing
75 8*0
76 Bare tower 100 mph wind at azimuth 90 deg
77 wind loading
78 90,100,0,0,56.2,1,1,1,1,1,1
79 suppress printing
80 1,0,1,1,4*0
81 Bare tower 100 mph wind at azimuth 180 deg
82 wind loading
83 180,100,0,0,56.2,1,1,1,1,1,1
===============================================================================
END OF FILE
ELAPSED CPU TIME 0.11 SECONDS.
===============================================================================