Download - Method of Design Cantilever Erection
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DESIGN OF LINK ARRANGEMENT AND BUFFER
FOR
CANTILEVER ERECTION
92M SPAN STEEL BRIDGE
EAST COAST RAILWAY
RAIL VIKAS NIGAM LIMITEDPMC : WILBUR SMITH ASSOCIATES LTD
CONTRACTOR : HCIL ADHI KARYA ARSS (JV)Construction of Doubling railway line between Barang-Rajathgarh, Barang-Cuttack,and
3rd Line Between Barang-Khurda Road
PROJPROJPROJPROJ
PROJPROJPROJPROJ
PROJPROJPROJPROJ
PROJPROJPROJPROJ
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ARRANGEMENT OF LINK AND BUFFER
Ref. drg. No. 9114/E/DD-22-101 (ALT-1) (R5)
c/c of pier : 93231 mm
c/c of bearing : 92000 mm
c/c of bearing at pier = 93231 92000 = 1231 mm
Distance between U15 and U1 = 2 x 5750 + 1231 = 12731 mm
EXTENSION PIECE
Max erection force = 1255.2 t ~ 1256 t
Try 2PL 680x20 + 1PL 680x16 (Yst=36 kg/mm2) with each gusset
Gross area = 4x68x2 + 2x68x1.6 = 761.6 cm2
Holes =10x(2+2+1.6)x2.35 = 131.6 cm2
= 630.0 cm2
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Tension allowed = 630x2130x1.25 = 1677 t > 1256 t ok
EXTENSION PIECE ACROSS PIN HOLE
Net area req :
=
cm2Try 2 additional plate 660x12 and 660x10 with each gusset
with 250 pin
Gross area of main section = 761.6 cm2
Add. PL 2x66x(1.2+1) = 290.4 cm2
= 1052.0 cm2
Deduction for holes
2x25x7.8 =-390.00 cm2
8x7.8x2.15 =-134.16 cm2
= 527.84 cm2 > 475cm2 ok
Longitudinal net sectional are to be provided to additional
plate beyond pin holes
= 2xbx7.8 = 475 cm2 b=30.5 cm
Hence b1 (min) req
= 30.5+2x2.15+25/2 = 47.3 cm provide b1 = 500mm
LINK
Pmax = 1255.2 t ~ 1256 t
Try 2PL 680x20 + 1PL 680x16 (Yst=36 kg/mm2) with each gusset
Gross area = 4x68x2 + 2x68x1.6 = 761.6 cm2
Holes =10x(2+2+1.6)x2.35 = 131.6 cm2
= 630.0 cm2
Tension allowed = 630x2130x1.25 = 1677 t > 1256 t ok
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LINK ACROSS PIN HOLE
Gross area of main section = 761.6 cm2
Add. PL 2x66x(1.2+1) = 290.4 cm2
= 1052.0 cm2
Deduction for holes
2x25x7.8 =-390.00 cm2
8x7.8x2.35 =-146.64 cm2
= 515.36 cm2
> 475cm2 ok
Longitudinal net sectional are to be provided to additional plate
beyond pin holes
= 2xbx7.8 = 475 cm2
b=30.5 cm
Hence b1 (min) req
= 30.5+2x2.15+25/2 = 47.3 cm provide b1 = 500mm
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LINK PIN
Material : carbon steel class 4 to IS-1875 or equivalent
LINK ARRANGEMENT (IN PLAN)
e =
+ 4 = 90 mm
w1 = ( x 1256)/ 9.4 =66.81 t/cm
w2 = ( x 1256)/ 7.8 = 80.51t/cm
Try 250 mm dia pin
B.M = (66.81 x 9.4) x 9.0 80.51 x
= 5655 612 = 5043 t.cm
Bending Stress =
= (5043 x 1000)/( x 253/32) =3287 kg/cm2 < 2990 (table 1 ) x 1.25 (ok)
Shear stress on pin = 1256000/(2 x /4 x 252) = 1279 kg/cm2 < 1420 x 1.25 (ok) (table 1)
Min. bearing area provided on each side of pin = 7.8 cm x 25.0 cm = 195 cm
2
Bearing Stress on H.T.S Steel plate = 1256000/(2x195) = 3220 kg/cm2 < 2600 (table 1) x 1.25=3250
kg/cm2
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BUFFER SLAB
Material : Grade 58HTC to I.S 961 or equivalent with st = 35 kg/mm2
Try 1000 mm wide x 900 mm high slab
Let t = thickness in mm.
Length of line contract from buffer = 650 mm
Total buffer force = 1192 t (phase 2)
w = 1192/100 = 11.92 t/cmMA = (11.92 x 17.5
2
) / 2 = 1825.25 t.cm
RA = 1192/2 = 596.1 t
MC = 596.1 x 32.5 11.92 x (502/2) = 19373 14900 = 4470 t.cm
Allowable bending stress
= 2280 x 1.25 = 2850 kg/cm2
=2.88 t/cm
2
t =
=
= 10.22 cm, Provide t= 100 mm
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BUFFER
Let L= contact length of buffer = 650 mm (Ref. cl. 3.12.3 of steel Bridge code)
Allowable working load per unit length of roller = 0.8 D kg/mm length
Where D = diameter of roller in mm
= 0.8D
Or D = (1192 x 1000) / (0.8 x 650) = 2292 mm
Provide D = 2300 mm ( i.e radius = 1150 mm)
Check bottom chord area in bearing
Gross area of bottom chord (L0 L1) = 420 cm2 ( increased section area )
Bearing stress ( on H.T.S material of main bridge )
= 1192000/420 = 2838 kg / cm2
< 2600 * 1.25 = 3250 kg / cm2
( Table II for H.T.S steel ) ok
Check Link member for crane load
Span 6.5 m
A . Crane wheel load = 7.0 t per wheel
B . UDL
Self weight of link : 4 x 0.68 x 157.0 + 2 x 0.68 x 125.6 = 598 kg / m
Self weight of track : 0.46 / 5.75 = 80 kg / m
= 678 kg / m ~ 0.7 t/m
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Section used for link :
4PL 680 x 20 + 2PL 680 x 16 (HTS)
I xx = (4 x 2.0 + 2.0 x 1.6) x 683
/ 12 = 293470 cm4
Zxx = 293470 / 34.0 = 8631 cm3
B.M = 7.0 x + 0.7 x
=11.38 + 3.7 = 15.08 tm
Bending Stress = (15.08 x 105) / 8631 = 175 kg/cm
2< (2250 kg/cm
2(for HTS) x 1.25 (erection) ok.
LINK PROP
Loads :
Crane wheel = 7.0 ton
Crack Track 0.7 t/m x 6.5 m = 4.6 ton
Self wt.say 2/ mc-300 = 2 x 12.25 m @ 35.8 kg/m = 0.9 ton
= 12.5 ton
Area = 2 x 45.64 = 91.28 cm2
r xx = 11.81 cm
l/r = (1.0 x 1225)/11.81 = 104 < 140 (cl.6.2.3)
Ref. Table IV,, Yst = 26 kg/mm2
(P=17.8)
Allowable compression during erection = 91.28 x 0.794 x 1.25 = 90.5 ton > 12.5 ton o.k
Use 2/MC-300
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LINK SHORTENING
As per computer output , enclosed.
Deflection at free end of cantilever span = 106.71 cm
Shortening of link to neutralize this deflection
= * h/L where, = 106.71 cm
h = 12.250 m
L = 92.0 m
= 106.71 x = 14.21 cm .. (1)
Shortening of link to neutralize camber effect of Top chord
= 4 x (5756 5750 ) + 10 x (5758 5750) = 104 mm = 10.4 cm .. (2)
Shortening of link to keep free end at least 150 mm above top of bearing
= 15 cm x m = 1.99 cm 2.0 cm . (3)
Total Shortening
= (1) + (2) + (3)
= 14.21 + 10.4 + 2.0 = 26.61 cm 270 mm
Nominal length of link between pin centers (ref. page 1)
= 12731 2 x 1000 = 10731 mm
Actual length to be fabricated
= 10731 270 = 10461 mm 10470 mm
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PAGE NO. 1
****************************************************
* *
* STAAD.Pro *
* Version 2003 Bld 1001.US *
* Proprietary Program of *
* Research Engineers, Intl. *
* Date= FEB 1, 2008 *
* Time= 17:31:20 *
* *
* USER ID: *
****************************************************
1. STAAD SPACE DXF IMPORT OF ACAD-89 SPAN.DXF
2. START JOB INFORMATION
3. JOB NAME CANTILEVER ERECTION SPAN 92M
4. JOB CLIENT RVNL
5. JOB NO AA
6. JOB PART 0
7. JOB REF 0
8. ENGINEER NAME ADHI T
9. ENGINEER DATE 31-JAN-08
10. END JOB INFORMATION
11. INPUT WIDTH 79
12. OUTPUT WIDTH 118
13. OUTPUT WIDTH 72
14. UNIT METER KG
15. JOINT COORDINATES
16. 1 0 0 0; 2 5.75 0 0; 3 11.5 0 0; 4 17.25 0 0; 6 23 0 0; 7 28.75 0 0
17. 8 34.5 0 0; 9 40.25 0 0; 10 46 0 0; 11 51.75 0 0; 12 57.5 0 0; 13 63.25 0 0
18. 14 69 0 0; 15 74.75 0 0; 16 80.5 0 0; 17 86.25 0 0; 18 92 0 0; 19 97.75 0 0
19. 20 103.5 0 0; 21 109.25 0 0; 22 115 0 0; 23 120.75 0 0; 24 126.5 0 0
20. 25 132.25 0 0; 26 138 0 0; 27 143.75 0 0; 28 149.5 0 0; 29 155.25 0 0
21. 30 161 0 0; 31 166.75 0 0; 32 172.5 0 0; 33 178.25 0 0; 34 184 0 0
22. 35 0 6.25 0; 36 5.75 6.25 0; 37 11.5 6.25 0; 38 23 6.25 0; 39 34.5 6.25 0
23. 40 46 6.25 0; 41 57.5 6.25 0; 42 69 6.25 0; 43 80.5 6.25 0; 44 86.25 6.25 0
24. 45 92 6.25 0; 46 97.75 6.25 0; 47 103.5 6.25 0; 48 115 6.25 0; 49 126.5 6.25 0
25. 50 138 6.25 0; 51 149.5 6.25 0; 52 161 6.25 0; 53 172.5 6.25 0
26. 54 178.25 6.25 0; 55 184 6.25 0; 56 5.75 12.5 0; 57 11.5 12.5 0
27. 58 17.25 12.5 0; 59 23 12.5 0; 60 28.75 12.5 0; 61 34.5 12.5 0
28. 62 40.25 12.5 0; 63 46 12.5 0; 64 51.75 12.5 0; 65 57.5 12.5 0
29. 66 63.25 12.5 0; 67 69 12.5 0; 68 74.75 12.5 0; 69 80.5 12.5 0
30. 70 86.25 12.5 0; 71 92 12.5 0; 72 97.75 12.5 0; 73 103.5 12.5 0
31. 74 109.25 12.5 0; 75 115 12.5 0; 76 120.75 12.5 0; 77 126.5 12.5 0
32. 78 132.25 12.5 0; 79 138 12.5 0; 80 143.75 12.5 0; 81 149.5 12.5 0
33. 82 155.25 12.5 0; 83 161 12.5 0; 84 166.75 12.5 0; 85 172.5 12.5 0
34. 86 178.25 12.5 0
35. MEMBER INCIDENCES
36. 1 1 2; 2 2 3; 3 3 4; 5 6 7; 6 7 8; 7 8 9; 8 9 10; 9 10 11; 10 11 12; 11 12 13
37. 12 13 14; 13 14 15; 14 15 16; 15 16 17; 16 17 18; 17 18 19; 18 19 20; 19 20 21
38. 20 21 22; 21 22 23; 22 23 24; 23 24 25; 24 25 26; 25 26 27; 26 27 28; 27 28 29
39. 28 29 30; 29 30 31; 30 31 32; 31 32 33; 32 33 34; 33 1 35; 34 2 36; 35 3 37
40. 36 6 38; 37 8 39; 38 10 40; 39 12 41; 40 14 42; 41 16 43; 42 17 44; 43 18 45
41. 44 19 46; 45 20 47; 46 22 48; 47 24 49; 48 26 50; 49 28 51; 50 30 52; 51 32 53
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 2
42. 52 33 54; 53 34 55; 54 36 56; 55 35 56; 56 56 57; 57 57 58; 58 58 59; 59 59 60
43. 60 60 61; 61 61 62; 62 62 63; 63 63 64; 64 64 65; 65 65 66; 66 66 67; 67 67 68
44. 68 68 69; 69 69 70; 70 70 71; 71 71 72; 72 72 73; 73 73 74; 74 74 75; 75 75 76
45. 76 76 77; 77 77 78; 78 78 79; 79 79 80; 80 80 81; 81 81 82; 82 82 83; 83 83 84
46. 84 84 85; 85 85 86; 86 86 55; 87 35 2; 88 2 37; 89 37 4; 90 4 38; 91 38 7
47. 92 7 39; 93 39 9; 94 9 40; 95 40 11; 96 11 41; 97 41 13; 98 13 42; 99 42 15
48. 100 15 43; 101 43 17; 102 17 45; 103 45 19; 104 19 47; 105 47 21; 106 21 48
49. 107 48 23; 108 23 49; 109 49 25; 110 25 50; 111 50 27; 112 27 51; 113 51 29
50. 114 29 52; 115 52 31; 116 31 53; 117 53 33; 118 33 55; 119 37 57; 120 38 59
51. 121 39 61; 122 40 63; 123 41 65; 124 42 67; 125 43 69; 126 44 70; 127 45 71
52. 128 46 72; 129 47 73; 130 48 75; 131 49 77; 132 50 79; 133 51 81; 134 52 83
53. 135 53 85; 136 54 86; 137 35 36; 138 56 37; 139 37 58; 140 58 38; 141 38 60
54. 142 60 39; 143 39 62; 144 62 40; 145 40 64; 146 64 41; 147 41 66; 148 66 42
55. 149 42 68; 150 68 43; 151 43 70; 152 70 45; 153 45 72; 154 72 47; 155 47 74
56. 156 74 48; 157 48 76; 158 76 49; 159 49 78; 160 78 50; 161 50 80; 162 80 51
57. 163 51 82; 164 82 52; 165 52 84; 166 84 53; 167 53 86; 168 4 6; 169 55 54
58. 170 44 45; 171 45 46
59. UNIT MMS KG
60. DEFINE MATERIAL START
61. ISOTROPIC STEEL
62. E 20904.2
63. POISSON 0.3
64. DENSITY 7.83341E-006
65. ALPHA 6.5E-006
66. DAMP 0.03
67. END DEFINE MATERIAL
68. CONSTANTS
69. MATERIAL STEEL MEMB 1 TO 3 5 TO 171
70. START USER TABLE
71. TABLE 1
72. UNIT METER KG
73. PRISMATIC
74. L0-L1
75. 0.042 0.00300535 0.003635 5.227E-006 0 0 0.75 0.65
76. L3-L5
77. 0.0466 0.002876 0.004157 3.101E-006 0 0 0.75 0.65
78. L5-L7
79. 0.0544 0.00315055 0.00484085 4.362E-006 0 0 0.75 0.65
80. L7-L9
81. 0.0568 0.003456 0.004977 5.06161E-006 0 0 0.75 0.65
82. U1-U3
83. 0.03956 0.00273966 0.00291664 3.75952E-006 0 0 0.7 0.65
84. U3-U5
85. 0.030416 0.00212652 0.00224754 1.73941E-006 0 0 0.7 0.65
86. U5-U7
87. 0.037088 0.00255131 0.00283797 2.97484E-006 0 0 0.7 0.65
88. U7-U9
89. 0.03956 0.00273966 0.00291664 3.75952E-006 0 0 0.7 0.65
90. M0-L0
91. 0.0702 0.00390456 0.00557558 8.78136E-006 0 0 0.7 0.65
92. M0-U1
93. 0.027912 0.0019362 0.00216577 1.26135E-006 0 0 0.7 0.65
94. VERT
95. 0.0113 2.60942E-005 0.000720414 3.54516E-007 0 0 0.25 0.65
96. DIL0-L3
97. 0.0224 0.000524766 0.00183019 1.79125E-006 0 0 0.4 0.65
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 3
98. DIL3-L5
99. 0.0168 0.000399066 0.00139836 7.57914E-007 0 0 0.4 0.65
100. DIL5-L8
101. 0.014 0.000334867 0.00117612 4.38745E-007 0 0 0.4 0.65
102. LINK
103. 0.07616 0.0029347 0.0067379 8.56867E-006 0 0 0.68 0.65
104. END
105. UNIT MMS KG
106. MEMBER PROPERTY AMERICAN
107. 1 TO 3 14 TO 19 30 TO 32 UPTABLE 1 L0-L1
108. 5 12 13 20 21 28 29 168 UPTABLE 1 L3-L5
109. MEMBER PROPERTY AMERICAN
110. 6 7 10 11 22 23 26 27 UPTABLE 1 L5-L7
111. 8 9 24 25 UPTABLE 1 L7-L9
112. 56 57 68 69 72 73 84 85 UPTABLE 1 U1-U3
113. 58 59 66 67 74 75 82 83 UPTABLE 1 U3-U5
114. 60 61 64 65 76 77 80 81 UPTABLE 1 U5-U7
115. 62 63 78 79 UPTABLE 1 U7-U9
116. 33 43 53 UPTABLE 1 M0-L0
117. 55 86 152 153 UPTABLE 1 M0-U1
118. 34 TO 42 44 TO 52 54 119 TO 126 128 TO 137 169 TO 171 UPTABLE 1 VERT
119. 87 TO 89 100 TO 105 116 TO 118 138 139 150 151 154 155 166 -
120. 167 UPTABLE 1 DIL0-L3
121. 90 91 98 99 106 107 114 115 140 141 148 149 156 157 164 165 UPTABLE 1 DIL3-L5
122. 92 TO 97 108 TO 113 142 TO 147 158 TO 163 UPTABLE 1 DIL5-L8
123. 70 71 127 UPTABLE 1 LINK
124. SUPPORTS
125. 1 PINNED
126. 18 FIXED BUT FX MX MY MZ
127. UNIT METER KG
128. MEMBER TRUSS
129. 1 TO 3 5 TO 171
130. UNIT MMS KG
131. LOAD 1 LOAD 1 DEAD LOAD
132. SELFWEIGHT Y -1
133. LOAD 2 LOAD 2 ERECTION
134. JOINT LOAD
135. 1 18 FY -6320
136. 2 TO 4 6 TO 17 FY -12640
137. 19 TO 28 FY -12340
138. 29 FY -14570
139. 30 FY -21800
140. 31 FY -21110
141. 32 FY -11120
142. 33 FY -9620
143. 34 FY -4410
144. UNIT METER KG
145. LOAD COMB 3 LOAD COMBINATION
146. 1 1.0 2 1.0
147. UNIT MMS KG
148. PERFORM ANALYSIS
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 4
P R O B L E M S T A T I S T I C S
-----------------------------------
NUMBER OF JOINTS/MEMBER+ELEMENTS/SUPPORTS = 85/ 170/ 2
ORIGINAL/FINAL BAND-WIDTH= 34/ 4/ 30 DOF
TOTAL PRIMARY LOAD CASES = 2, TOTAL DEGREES OF FREEDOM = 505
SIZE OF STIFFNESS MATRIX = 16 DOUBLE KILO-WORDS
REQRD/AVAIL. DISK SPACE = 12.4/ 25300.5 MB, EXMEM = 520.2 MB
ZERO STIFFNESS IN DIRECTION 4 AT JOINT 1 EQN.NO. 1
LOADS APPLIED OR DISTRIBUTED HERE FROM ELEMENTS WILL BE IGNORED.
THIS MAY BE DUE TO ALL MEMBERS AT THIS JOINT BEING RELEASED OR
EFFECTIVELY RELEASED IN THIS DIRECTION.
ZERO STIFFNESS IN DIRECTION 5 AT JOINT 1 EQN.NO. 2
ZERO STIFFNESS IN DIRECTION 6 AT JOINT 1 EQN.NO. 3
ZERO STIFFNESS IN DIRECTION 3 AT JOINT 2 EQN.NO. 6
ZERO STIFFNESS IN DIRECTION 4 AT JOINT 2 EQN.NO. 7
ZERO STIFFNESS IN DIRECTION 5 AT JOINT 2 EQN.NO. 8
ZERO STIFFNESS IN DIRECTION 6 AT JOINT 2 EQN.NO. 9
ZERO STIFFNESS IN DIRECTION 3 AT JOINT 35 EQN.NO. 12
ZERO STIFFNESS IN DIRECTION 4 AT JOINT 35 EQN.NO. 13
ZERO STIFFNESS IN DIRECTION 5 AT JOINT 35 EQN.NO. 14
ZERO STIFFNESS IN DIRECTION 6 AT JOINT 35 EQN.NO. 15
ZERO STIFFNESS IN DIRECTION 3 AT JOINT 3 EQN.NO. 18
**WARNING - THERE WERE MORE THAN 12 DOF WITH ZERO STIFFNESS.
THE FIRST 12 ARE LISTED ABOVE.
TOTAL # TRANSLATIONAL= 83 TOTAL # ROTATIONAL= 255
149. PRINT ANALYSIS RESULTS
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 5
JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = SPACE
------------------
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
1 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
3 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
2 1 0.0000 0.2373 0.0000 0.0000 0.0000 0.0000
2 0.0000 0.4570 0.0000 0.0000 0.0000 0.0000
3 0.0000 0.6944 0.0000 0.0000 0.0000 0.0000
3 1 -0.0060 0.4833 0.0000 0.0000 0.0000 0.0000
2 -0.0142 0.9161 0.0000 0.0000 0.0000 0.0000
3 -0.0202 1.3994 0.0000 0.0000 0.0000 0.0000
4 1 -0.0120 0.7428 0.0000 0.0000 0.0000 0.0000
2 -0.0284 1.4176 0.0000 0.0000 0.0000 0.0000
3 -0.0403 2.1604 0.0000 0.0000 0.0000 0.0000
6 1 -0.0308 1.0129 0.0000 0.0000 0.0000 0.0000
2 -0.0663 1.9287 0.0000 0.0000 0.0000 0.0000
3 -0.0971 2.9416 0.0000 0.0000 0.0000 0.0000
7 1 -0.0496 1.2741 0.0000 0.0000 0.0000 0.0000
2 -0.1043 2.4347 0.0000 0.0000 0.0000 0.0000
3 -0.1539 3.7088 0.0000 0.0000 0.0000 0.0000
8 1 -0.0831 1.5422 0.0000 0.0000 0.0000 0.0000
2 -0.1697 2.9445 0.0000 0.0000 0.0000 0.0000
3 -0.2528 4.4867 0.0000 0.0000 0.0000 0.0000
9 1 -0.1165 1.7806 0.0000 0.0000 0.0000 0.0000
2 -0.2351 3.4034 0.0000 0.0000 0.0000 0.0000
3 -0.3516 5.1840 0.0000 0.0000 0.0000 0.0000
10 1 -0.1710 2.0061 0.0000 0.0000 0.0000 0.0000
2 -0.3409 3.8351 0.0000 0.0000 0.0000 0.0000
3 -0.5119 5.8412 0.0000 0.0000 0.0000 0.0000
11 1 -0.2255 2.1635 0.0000 0.0000 0.0000 0.0000
2 -0.4468 4.1363 0.0000 0.0000 0.0000 0.0000
3 -0.6723 6.2998 0.0000 0.0000 0.0000 0.0000
12 1 -0.3120 2.2988 0.0000 0.0000 0.0000 0.0000
2 -0.6137 4.3949 0.0000 0.0000 0.0000 0.0000
3 -0.9257 6.6936 0.0000 0.0000 0.0000 0.0000
13 1 -0.3985 2.3067 0.0000 0.0000 0.0000 0.0000
2 -0.7806 4.4158 0.0000 0.0000 0.0000 0.0000
3 -1.1791 6.7225 0.0000 0.0000 0.0000 0.0000
14 1 -0.5413 2.2341 0.0000 0.0000 0.0000 0.0000
2 -1.0555 4.2713 0.0000 0.0000 0.0000 0.0000
3 -1.5968 6.5055 0.0000 0.0000 0.0000 0.0000
15 1 -0.6840 1.9247 0.0000 0.0000 0.0000 0.0000
2 -1.3305 3.6857 0.0000 0.0000 0.0000 0.0000
3 -2.0145 5.6104 0.0000 0.0000 0.0000 0.0000
16 1 -0.8962 1.4772 0.0000 0.0000 0.0000 0.0000
2 -1.7391 2.8276 0.0000 0.0000 0.0000 0.0000
3 -2.6353 4.3049 0.0000 0.0000 0.0000 0.0000
17 1 -1.1085 0.6638 0.0000 0.0000 0.0000 0.0000
2 -2.1476 1.2863 0.0000 0.0000 0.0000 0.0000
3 -3.2561 1.9502 0.0000 0.0000 0.0000 0.0000
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JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = SPACE
------------------
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
18 1 -1.3765 0.0000 0.0000 0.0000 0.0000 0.0000
2 -2.6603 0.0000 0.0000 0.0000 0.0000 0.0000
3 -4.0368 0.0000 0.0000 0.0000 0.0000 0.0000
19 1 -1.6445 -1.6374 0.0000 0.0000 0.0000 0.0000
2 -3.1730 -3.1190 0.0000 0.0000 0.0000 0.0000
3 -4.8175 -4.7564 0.0000 0.0000 0.0000 0.0000
20 1 -1.8567 -3.1252 0.0000 0.0000 0.0000 0.0000
2 -3.5800 -5.9820 0.0000 0.0000 0.0000 0.0000
3 -5.4367 -9.1071 0.0000 0.0000 0.0000 0.0000
21 1 -2.0689 -4.9789 0.0000 0.0000 0.0000 0.0000
2 -3.9870 -9.5248 0.0000 0.0000 0.0000 0.0000
3 -6.0559 -14.5037 0.0000 0.0000 0.0000 0.0000
22 1 -2.2117 -6.9707 0.0000 0.0000 0.0000 0.0000
2 -4.2592 -13.3475 0.0000 0.0000 0.0000 0.0000
3 -6.4709 -20.3182 0.0000 0.0000 0.0000 0.0000
23 1 -2.3544 -9.1993 0.0000 0.0000 0.0000 0.0000
2 -4.5315 -17.6107 0.0000 0.0000 0.0000 0.0000
3 -6.8859 -26.8100 0.0000 0.0000 0.0000 0.0000
24 1 -2.4409 -11.5084 0.0000 0.0000 0.0000 0.0000
2 -4.6942 -22.0259 0.0000 0.0000 0.0000 0.0000
3 -7.1352 -33.5343 0.0000 0.0000 0.0000 0.0000
25 1 -2.5274 -13.9449 0.0000 0.0000 0.0000 0.0000
2 -4.8569 -26.6694 0.0000 0.0000 0.0000 0.0000
3 -7.3844 -40.6143 0.0000 0.0000 0.0000 0.0000
26 1 -2.5819 -16.4035 0.0000 0.0000 0.0000 0.0000
2 -4.9572 -31.3741 0.0000 0.0000 0.0000 0.0000
3 -7.5391 -47.7776 0.0000 0.0000 0.0000 0.0000
27 1 -2.6364 -18.9302 0.0000 0.0000 0.0000 0.0000
2 -5.0574 -36.2038 0.0000 0.0000 0.0000 0.0000
3 -7.6939 -55.1340 0.0000 0.0000 0.0000 0.0000
28 1 -2.6699 -21.4698 0.0000 0.0000 0.0000 0.0000
2 -5.1146 -41.0309 0.0000 0.0000 0.0000 0.0000
3 -7.7844 -62.5007 0.0000 0.0000 0.0000 0.0000
29 1 -2.7033 -24.0391 0.0000 0.0000 0.0000 0.0000
2 -5.1717 -45.8920 0.0000 0.0000 0.0000 0.0000
3 -7.8750 -69.9311 0.0000 0.0000 0.0000 0.0000
30 1 -2.7221 -26.6015 0.0000 0.0000 0.0000 0.0000
2 -5.1987 -50.7971 0.0000 0.0000 0.0000 0.0000
3 -7.9208 -77.3986 0.0000 0.0000 0.0000 0.0000
31 1 -2.7409 -29.1728 0.0000 0.0000 0.0000 0.0000
2 -5.2256 -55.6300 0.0000 0.0000 0.0000 0.0000
3 -7.9666 -84.8028 0.0000 0.0000 0.0000 0.0000
32 1 -2.7469 -31.7335 0.0000 0.0000 0.0000 0.0000
2 -5.2347 -60.3931 0.0000 0.0000 0.0000 0.0000
3 -7.9816 -92.1266 0.0000 0.0000 0.0000 0.0000
33 1 -2.7529 -34.2807 0.0000 0.0000 0.0000 0.0000
2 -5.2438 -65.1344 0.0000 0.0000 0.0000 0.0000
3 -7.9967 -99.4151 0.0000 0.0000 0.0000 0.0000
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 8
JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = SPACE
------------------
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
50 1 -0.0387 -16.3960 0.0000 0.0000 0.0000 0.0000
2 -0.1059 -31.3415 0.0000 0.0000 0.0000 0.0000
3 -0.1445 -47.7374 0.0000 0.0000 0.0000 0.0000
51 1 -0.0207 -21.4626 0.0000 0.0000 0.0000 0.0000
2 -0.1079 -40.9982 0.0000 0.0000 0.0000 0.0000
3 -0.1286 -62.4608 0.0000 0.0000 0.0000 0.0000
52 1 -0.0072 -26.5952 0.0000 0.0000 0.0000 0.0000
2 -0.0450 -50.7394 0.0000 0.0000 0.0000 0.0000
3 -0.0522 -77.3346 0.0000 0.0000 0.0000 0.0000
53 1 -0.0028 -31.7278 0.0000 0.0000 0.0000 0.0000
2 -0.1050 -60.3637 0.0000 0.0000 0.0000 0.0000
3 -0.1077 -92.0915 0.0000 0.0000 0.0000 0.0000
54 1 -0.0064 -34.2806 0.0000 0.0000 0.0000 0.0000
2 -0.0788 -65.1370 0.0000 0.0000 0.0000 0.0000
3 -0.0852 -99.4176 0.0000 0.0000 0.0000 0.0000
55 1 -0.0064 -36.8181 0.0000 0.0000 0.0000 0.0000
2 -0.0788 -69.8935 0.0000 0.0000 0.0000 0.0000
3 -0.0852 -106.7116 0.0000 0.0000 0.0000 0.0000
56 1 -0.4952 0.2396 0.0000 0.0000 0.0000 0.0000
2 -0.9530 0.4750 0.0000 0.0000 0.0000 0.0000
3 -1.4482 0.7146 0.0000 0.0000 0.0000 0.0000
57 1 -0.4888 0.4836 0.0000 0.0000 0.0000 0.0000
2 -0.9417 0.9495 0.0000 0.0000 0.0000 0.0000
3 -1.4305 1.4331 0.0000 0.0000 0.0000 0.0000
58 1 -0.4824 0.7397 0.0000 0.0000 0.0000 0.0000
2 -0.9303 1.4438 0.0000 0.0000 0.0000 0.0000
3 -1.4128 2.1835 0.0000 0.0000 0.0000 0.0000
59 1 -0.4540 1.0148 0.0000 0.0000 0.0000 0.0000
2 -0.8778 1.9622 0.0000 0.0000 0.0000 0.0000
3 -1.3318 2.9770 0.0000 0.0000 0.0000 0.0000
60 1 -0.4255 1.2635 0.0000 0.0000 0.0000 0.0000
2 -0.8253 2.4425 0.0000 0.0000 0.0000 0.0000
3 -1.2508 3.7060 0.0000 0.0000 0.0000 0.0000
61 1 -0.3767 1.5443 0.0000 0.0000 0.0000 0.0000
2 -0.7334 2.9779 0.0000 0.0000 0.0000 0.0000
3 -1.1100 4.5222 0.0000 0.0000 0.0000 0.0000
62 1 -0.3278 1.7662 0.0000 0.0000 0.0000 0.0000
2 -0.6414 3.4092 0.0000 0.0000 0.0000 0.0000
3 -0.9693 5.1754 0.0000 0.0000 0.0000 0.0000
63 1 -0.2499 2.0082 0.0000 0.0000 0.0000 0.0000
2 -0.4938 3.8686 0.0000 0.0000 0.0000 0.0000
3 -0.7437 5.8767 0.0000 0.0000 0.0000 0.0000
64 1 -0.1720 2.1398 0.0000 0.0000 0.0000 0.0000
2 -0.3462 4.1267 0.0000 0.0000 0.0000 0.0000
3 -0.5182 6.2665 0.0000 0.0000 0.0000 0.0000
65 1 -0.0453 2.3008 0.0000 0.0000 0.0000 0.0000
2 -0.1054 4.4283 0.0000 0.0000 0.0000 0.0000
3 -0.1507 6.7291 0.0000 0.0000 0.0000 0.0000
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 9
JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = SPACE
------------------
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
66 1 0.0814 2.2597 0.0000 0.0000 0.0000 0.0000
2 0.1355 4.3519 0.0000 0.0000 0.0000 0.0000
3 0.2169 6.6116 0.0000 0.0000 0.0000 0.0000
67 1 0.2997 2.2361 0.0000 0.0000 0.0000 0.0000
2 0.5510 4.3048 0.0000 0.0000 0.0000 0.0000
3 0.8508 6.5409 0.0000 0.0000 0.0000 0.0000
68 1 0.5181 1.8366 0.0000 0.0000 0.0000 0.0000
2 0.9666 3.5517 0.0000 0.0000 0.0000 0.0000
3 1.4847 5.3883 0.0000 0.0000 0.0000 0.0000
69 1 0.7434 1.4775 0.0000 0.0000 0.0000 0.0000
2 1.3967 2.8611 0.0000 0.0000 0.0000 0.0000
3 2.1401 4.3386 0.0000 0.0000 0.0000 0.0000
70 1 0.9688 0.7276 0.0000 0.0000 0.0000 0.0000
2 1.8267 1.4199 0.0000 0.0000 0.0000 0.0000
3 2.7955 2.1475 0.0000 0.0000 0.0000 0.0000
71 1 1.1248 -0.1008 0.0000 0.0000 0.0000 0.0000
2 2.1240 -0.1746 0.0000 0.0000 0.0000 0.0000
3 3.2488 -0.2754 0.0000 0.0000 0.0000 0.0000
72 1 1.2809 -1.5736 0.0000 0.0000 0.0000 0.0000
2 2.4212 -2.9843 0.0000 0.0000 0.0000 0.0000
3 3.7021 -4.5579 0.0000 0.0000 0.0000 0.0000
73 1 1.5063 -3.1249 0.0000 0.0000 0.0000 0.0000
2 2.8500 -5.9493 0.0000 0.0000 0.0000 0.0000
3 4.3563 -9.0742 0.0000 0.0000 0.0000 0.0000
74 1 1.7316 -5.0670 0.0000 0.0000 0.0000 0.0000
2 3.2789 -9.6657 0.0000 0.0000 0.0000 0.0000
3 5.0105 -14.7326 0.0000 0.0000 0.0000 0.0000
75 1 1.9499 -6.9687 0.0000 0.0000 0.0000 0.0000
2 3.6900 -13.3149 0.0000 0.0000 0.0000 0.0000
3 5.6399 -20.2836 0.0000 0.0000 0.0000 0.0000
76 1 2.1683 -9.2463 0.0000 0.0000 0.0000 0.0000
2 4.1010 -17.6605 0.0000 0.0000 0.0000 0.0000
3 6.2693 -26.9068 0.0000 0.0000 0.0000 0.0000
77 1 2.2950 -11.5064 0.0000 0.0000 0.0000 0.0000
2 4.3362 -21.9932 0.0000 0.0000 0.0000 0.0000
3 6.6312 -33.4996 0.0000 0.0000 0.0000 0.0000
78 1 2.4216 -13.9686 0.0000 0.0000 0.0000 0.0000
2 4.5714 -26.6984 0.0000 0.0000 0.0000 0.0000
3 6.9931 -40.6670 0.0000 0.0000 0.0000 0.0000
79 1 2.4996 -16.4014 0.0000 0.0000 0.0000 0.0000
2 4.7107 -31.3415 0.0000 0.0000 0.0000 0.0000
3 7.2103 -47.7429 0.0000 0.0000 0.0000 0.0000
80 1 2.5775 -18.9447 0.0000 0.0000 0.0000 0.0000
2 4.8500 -36.1689 0.0000 0.0000 0.0000 0.0000
3 7.4276 -55.1136 0.0000 0.0000 0.0000 0.0000
81 1 2.6264 -21.4677 0.0000 0.0000 0.0000 0.0000
2 4.9304 -40.9982 0.0000 0.0000 0.0000 0.0000
3 7.5567 -62.4660 0.0000 0.0000 0.0000 0.0000
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 10
JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = SPACE
------------------
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
82 1 2.6752 -24.0497 0.0000 0.0000 0.0000 0.0000
2 5.0107 -45.9151 0.0000 0.0000 0.0000 0.0000
3 7.6859 -69.9648 0.0000 0.0000 0.0000 0.0000
83 1 2.7036 -26.5996 0.0000 0.0000 0.0000 0.0000
2 5.0441 -50.7394 0.0000 0.0000 0.0000 0.0000
3 7.7478 -77.3390 0.0000 0.0000 0.0000 0.0000
84 1 2.7321 -29.1759 0.0000 0.0000 0.0000 0.0000
2 5.0776 -55.5342 0.0000 0.0000 0.0000 0.0000
3 7.8097 -84.7101 0.0000 0.0000 0.0000 0.0000
85 1 2.7385 -31.7332 0.0000 0.0000 0.0000 0.0000
2 5.0797 -60.3637 0.0000 0.0000 0.0000 0.0000
3 7.8182 -92.0969 0.0000 0.0000 0.0000 0.0000
86 1 2.7449 -34.2784 0.0000 0.0000 0.0000 0.0000
2 5.0819 -65.1397 0.0000 0.0000 0.0000 0.0000
3 7.8268 -99.4181 0.0000 0.0000 0.0000 0.0000
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 11
SUPPORT REACTIONS -UNIT KG MMS STRUCTURE TYPE = SPACE
-----------------
JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM Z
1 1 0.00 0.00 0.00 0.00 0.00 0.00
2 0.00 -7976.24 0.00 0.00 0.00 0.00
3 0.00 -7976.23 0.00 0.00 0.00 0.00
18 1 0.00 235354.48 0.00 0.00 0.00 0.00
2 0.00 416246.25 0.00 0.00 0.00 0.00
3 0.00 651600.75 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 12
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
1 1 1 0.00 945.88 0.00 0.00 0.00 0.00
2 0.00 945.88 0.00 0.00 0.00 0.00
2 1 0.00 0.00 0.00 0.00 0.00 0.00
2 0.00 0.00 0.00 0.00 0.00 0.00
3 1 0.00 945.88 0.00 0.00 0.00 0.00
2 0.00 945.88 0.00 0.00 0.00 0.00
2 1 2 9154.41 945.88 0.00 0.00 0.00 0.00
3 -9154.41 945.88 0.00 0.00 0.00 0.00
2 2 21648.42 0.00 0.00 0.00 0.00 0.00
3 -21648.42 0.00 0.00 0.00 0.00 0.00
3 2 30802.83 945.88 0.00 0.00 0.00 0.00
3 -30802.83 945.88 0.00 0.00 0.00 0.00
3 1 3 9154.41 945.88 0.00 0.00 0.00 0.00
4 -9154.41 945.88 0.00 0.00 0.00 0.00
2 3 21648.42 0.00 0.00 0.00 0.00 0.00
4 -21648.42 0.00 0.00 0.00 0.00 0.00
3 3 30802.83 945.88 0.00 0.00 0.00 0.00
4 -30802.83 945.88 0.00 0.00 0.00 0.00
5 1 6 31884.02 1049.48 0.00 0.00 0.00 0.00
7 -31884.02 1049.48 0.00 0.00 0.00 0.00
2 6 64324.40 0.00 0.00 0.00 0.00 0.00
7 -64324.40 0.00 0.00 0.00 0.00 0.00
3 6 96208.42 1049.48 0.00 0.00 0.00 0.00
7 -96208.42 1049.48 0.00 0.00 0.00 0.00
6 1 7 66126.52 1225.15 0.00 0.00 0.00 0.00
8 -66126.52 1225.15 0.00 0.00 0.00 0.00
2 7 129355.09 0.00 0.00 0.00 0.00 0.00
8-129355.09 0.00 0.00 0.00 0.00 0.00
3 7 195481.62 1225.15 0.00 0.00 0.00 0.00
8-195481.62 1225.15 0.00 0.00 0.00 0.00
7 1 8 66126.52 1225.15 0.00 0.00 0.00 0.00
9 -66126.52 1225.15 0.00 0.00 0.00 0.00
2 8 129355.09 0.00 0.00 0.00 0.00 0.00
9-129355.09 0.00 0.00 0.00 0.00 0.00
3 8 195481.62 1225.15 0.00 0.00 0.00 0.00
9-195481.62 1225.15 0.00 0.00 0.00 0.00
8 1 9 112523.38 1279.20 0.00 0.00 0.00 0.00
10-112523.38 1279.20 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 13
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 9 218546.28 0.00 0.00 0.00 0.00 0.00
10-218546.28 0.00 0.00 0.00 0.00 0.00
3 9 331069.66 1279.20 0.00 0.00 0.00 0.00
10-331069.66 1279.20 0.00 0.00 0.00 0.00
9 1 10 112523.38 1279.20 0.00 0.00 0.00 0.00
11-112523.38 1279.20 0.00 0.00 0.00 0.00
2 10 218546.28 0.00 0.00 0.00 0.00 0.00
11-218546.28 0.00 0.00 0.00 0.00 0.00
3 10 331069.66 1279.20 0.00 0.00 0.00 0.00
11-331069.66 1279.20 0.00 0.00 0.00 0.00
10 1 11 171099.38 1225.15 0.00 0.00 0.00 0.00
12-171099.38 1225.15 0.00 0.00 0.00 0.00
2 11 330092.19 0.00 0.00 0.00 0.00 0.00
12-330092.19 0.00 0.00 0.00 0.00 0.00
3 11 501191.56 1225.15 0.00 0.00 0.00 0.00
12-501191.56 1225.15 0.00 0.00 0.00 0.00
11 1 12 171099.38 1225.15 0.00 0.00 0.00 0.00
13-171099.38 1225.15 0.00 0.00 0.00 0.00
2 12 330092.19 0.00 0.00 0.00 0.00 0.00
13-330092.19 0.00 0.00 0.00 0.00 0.00
3 12 501191.56 1225.15 0.00 0.00 0.00 0.00
13-501191.56 1225.15 0.00 0.00 0.00 0.00
12 1 13 241829.72 1049.48 0.00 0.00 0.00 0.00
14-241829.72 1049.48 0.00 0.00 0.00 0.00
2 13 465798.56 0.00 0.00 0.00 0.00 0.00
14-465798.56 0.00 0.00 0.00 0.00 0.00
3 13 707628.25 1049.48 0.00 0.00 0.00 0.00
14-707628.25 1049.48 0.00 0.00 0.00 0.00
13 1 14 241829.72 1049.48 0.00 0.00 0.00 0.00
15-241829.72 1049.48 0.00 0.00 0.00 0.00
2 14 465798.56 0.00 0.00 0.00 0.00 0.00
15-465798.56 0.00 0.00 0.00 0.00 0.00
3 14 707628.25 1049.48 0.00 0.00 0.00 0.00
15-707628.25 1049.48 0.00 0.00 0.00 0.00
14 1 15 324072.97 945.88 0.00 0.00 0.00 0.00
16-324072.97 945.88 0.00 0.00 0.00 0.00
2 15 623859.62 0.00 0.00 0.00 0.00 0.00
16-623859.62 0.00 0.00 0.00 0.00 0.00
3 15 947932.56 945.88 0.00 0.00 0.00 0.00
16-947932.56 945.88 0.00 0.00 0.00 0.00
15 1 16 324072.97 945.89 0.00 0.00 0.00 0.00
17-324072.97 945.89 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 14
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 16 623859.62 0.00 0.00 0.00 0.00 0.00
17-623859.62 0.00 0.00 0.00 0.00 0.00
3 16 947932.56 945.89 0.00 0.00 0.00 0.00
17-947932.56 945.89 0.00 0.00 0.00 0.00
16 1 17 409191.94 945.88 0.00 0.00 0.00 0.00
18-409191.94 945.88 0.00 0.00 0.00 0.00
2 17 782857.31 0.00 0.00 0.00 0.00 0.00
18-782857.31 0.00 0.00 0.00 0.00 0.00
3 171192049.12 945.88 0.00 0.00 0.00 0.00
18********** 945.88 0.00 0.00 0.00 0.00
17 1 18 409191.94 945.88 0.00 0.00 0.00 0.00
19-409191.94 945.88 0.00 0.00 0.00 0.00
2 18 782857.31 0.00 0.00 0.00 0.00 0.00
19-782857.31 0.00 0.00 0.00 0.00 0.00
3 181192049.12 945.88 0.00 0.00 0.00 0.00
19********** 945.88 0.00 0.00 0.00 0.00
18 1 19 324073.00 945.88 0.00 0.00 0.00 0.00
20-324073.00 945.88 0.00 0.00 0.00 0.00
2 19 621417.44 0.00 0.00 0.00 0.00 0.00
20-621417.44 0.00 0.00 0.00 0.00 0.00
3 19 945490.50 945.88 0.00 0.00 0.00 0.00
20-945490.50 945.88 0.00 0.00 0.00 0.00
19 1 20 324073.00 945.88 0.00 0.00 0.00 0.00
21-324073.00 945.88 0.00 0.00 0.00 0.00
2 20 621417.44 0.00 0.00 0.00 0.00 0.00
21-621417.44 0.00 0.00 0.00 0.00 0.00
3 20 945490.50 945.88 0.00 0.00 0.00 0.00
21-945490.50 945.88 0.00 0.00 0.00 0.00
20 1 21 241829.77 1049.48 0.00 0.00 0.00 0.00
22-241829.77 1049.48 0.00 0.00 0.00 0.00
2 21 461247.75 0.00 0.00 0.00 0.00 0.00
22-461247.75 0.00 0.00 0.00 0.00 0.00
3 21 703077.50 1049.48 0.00 0.00 0.00 0.00
22-703077.50 1049.48 0.00 0.00 0.00 0.00
21 1 22 241829.77 1049.48 0.00 0.00 0.00 0.00
23-241829.77 1049.48 0.00 0.00 0.00 0.00
2 22 461247.75 0.00 0.00 0.00 0.00 0.00
23-461247.75 0.00 0.00 0.00 0.00 0.00
3 22 703077.50 1049.48 0.00 0.00 0.00 0.00
23-703077.50 1049.48 0.00 0.00 0.00 0.00
22 1 23 171099.41 1225.15 0.00 0.00 0.00 0.00
24-171099.41 1225.15 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 15
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 23 321791.84 0.00 0.00 0.00 0.00 0.00
24-321791.84 0.00 0.00 0.00 0.00 0.00
3 23 492891.25 1225.15 0.00 0.00 0.00 0.00
24-492891.25 1225.15 0.00 0.00 0.00 0.00
23 1 24 171099.41 1225.15 0.00 0.00 0.00 0.00
25-171099.41 1225.15 0.00 0.00 0.00 0.00
2 24 321791.84 0.00 0.00 0.00 0.00 0.00
25-321791.84 0.00 0.00 0.00 0.00 0.00
3 24 492891.25 1225.15 0.00 0.00 0.00 0.00
25-492891.25 1225.15 0.00 0.00 0.00 0.00
24 1 25 112523.41 1279.20 0.00 0.00 0.00 0.00
26-112523.41 1279.20 0.00 0.00 0.00 0.00
2 25 207033.36 0.00 0.00 0.00 0.00 0.00
26-207033.36 0.00 0.00 0.00 0.00 0.00
3 25 319556.78 1279.20 0.00 0.00 0.00 0.00
26-319556.78 1279.20 0.00 0.00 0.00 0.00
25 1 26 112523.41 1279.20 0.00 0.00 0.00 0.00
27-112523.41 1279.20 0.00 0.00 0.00 0.00
2 26 207033.36 0.00 0.00 0.00 0.00 0.00
27-207033.36 0.00 0.00 0.00 0.00 0.00
3 26 319556.78 1279.20 0.00 0.00 0.00 0.00
27-319556.78 1279.20 0.00 0.00 0.00 0.00
26 1 27 66126.55 1225.15 0.00 0.00 0.00 0.00
28 -66126.55 1225.15 0.00 0.00 0.00 0.00
2 27 112988.66 0.00 0.00 0.00 0.00 0.00
28-112988.66 0.00 0.00 0.00 0.00 0.00
3 27 179115.22 1225.15 0.00 0.00 0.00 0.00
28-179115.22 1225.15 0.00 0.00 0.00 0.00
27 1 28 66126.55 1225.15 0.00 0.00 0.00 0.00
29 -66126.55 1225.15 0.00 0.00 0.00 0.00
2 28 112988.66 0.00 0.00 0.00 0.00 0.00
29-112988.66 0.00 0.00 0.00 0.00 0.00
3 28 179115.22 1225.15 0.00 0.00 0.00 0.00
29-179115.22 1225.15 0.00 0.00 0.00 0.00
28 1 29 31884.05 1049.48 0.00 0.00 0.00 0.00
30 -31884.05 1049.48 0.00 0.00 0.00 0.00
2 29 45692.97 0.00 0.00 0.00 0.00 0.00
30 -45692.97 0.00 0.00 0.00 0.00 0.00
3 29 77577.02 1049.48 0.00 0.00 0.00 0.00
30 -77577.02 1049.48 0.00 0.00 0.00 0.00
29 1 30 31884.05 1049.48 0.00 0.00 0.00 0.00
31 -31884.05 1049.48 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 16
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 30 45692.97 0.00 0.00 0.00 0.00 0.00
31 -45692.97 0.00 0.00 0.00 0.00 0.00
3 30 77577.02 1049.48 0.00 0.00 0.00 0.00
31 -77577.02 1049.48 0.00 0.00 0.00 0.00
30 1 31 9154.41 945.89 0.00 0.00 0.00 0.00
32 -9154.41 945.89 0.00 0.00 0.00 0.00
2 31 13831.06 0.00 0.00 0.00 0.00 0.00
32 -13831.06 0.00 0.00 0.00 0.00 0.00
3 31 22985.47 945.89 0.00 0.00 0.00 0.00
32 -22985.47 945.89 0.00 0.00 0.00 0.00
31 1 32 9154.41 945.88 0.00 0.00 0.00 0.00
33 -9154.41 945.88 0.00 0.00 0.00 0.00
2 32 13831.06 0.00 0.00 0.00 0.00 0.00
33 -13831.06 0.00 0.00 0.00 0.00 0.00
3 32 22985.47 945.88 0.00 0.00 0.00 0.00
33 -22985.47 945.88 0.00 0.00 0.00 0.00
32 1 33 0.00 945.88 0.00 0.00 0.00 0.00
34 0.00 945.88 0.00 0.00 0.00 0.00
2 33 0.00 0.00 0.00 0.00 0.00 0.00
34 0.00 0.00 0.00 0.00 0.00 0.00
3 33 0.00 945.88 0.00 0.00 0.00 0.00
34 0.00 945.88 0.00 0.00 0.00 0.00
33 1 1 -945.88 0.00 0.00 0.00 0.00 0.00
35 4382.79 0.00 0.00 0.00 0.00 0.00
2 1 -14296.24 0.00 0.00 0.00 0.00 0.00
35 14296.24 0.00 0.00 0.00 0.00 0.00
3 1 -15242.12 0.00 0.00 0.00 0.00 0.00
35 18679.03 0.00 0.00 0.00 0.00 0.00
34 1 2 257.67 0.00 0.00 0.00 0.00 0.00
36 295.56 0.00 0.00 0.00 0.00 0.00
2 2 -3405.34 0.00 0.00 0.00 0.00 0.00
36 3405.34 0.00 0.00 0.00 0.00 0.00
3 2 -3147.67 0.00 0.00 0.00 0.00 0.00
36 3700.91 0.00 0.00 0.00 0.00 0.00
35 1 3 -1891.77 0.00 0.00 0.00 0.00 0.00
37 2445.00 0.00 0.00 0.00 0.00 0.00
2 3 -12640.00 0.00 0.00 0.00 0.00 0.00
37 12640.00 0.00 0.00 0.00 0.00 0.00
3 3 -14531.77 0.00 0.00 0.00 0.00 0.00
37 15085.00 0.00 0.00 0.00 0.00 0.00
36 1 6 -2098.96 0.00 0.00 0.00 0.00 0.00
38 2652.20 0.00 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 17
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 6 -12640.00 0.00 0.00 0.00 0.00 0.00
38 12640.00 0.00 0.00 0.00 0.00 0.00
3 6 -14738.96 0.00 0.00 0.00 0.00 0.00
38 15292.20 0.00 0.00 0.00 0.00 0.00
37 1 8 -2450.29 0.00 0.00 0.00 0.00 0.00
39 3003.53 0.00 0.00 0.00 0.00 0.00
2 8 -12640.00 0.00 0.00 0.00 0.00 0.00
39 12640.00 0.00 0.00 0.00 0.00 0.00
3 8 -15090.29 0.00 0.00 0.00 0.00 0.00
39 15643.52 0.00 0.00 0.00 0.00 0.00
38 1 10 -2558.39 0.00 0.00 0.00 0.00 0.00
40 3111.63 0.00 0.00 0.00 0.00 0.00
2 10 -12640.00 0.00 0.00 0.00 0.00 0.00
40 12640.00 0.00 0.00 0.00 0.00 0.00
3 10 -15198.39 0.00 0.00 0.00 0.00 0.00
40 15751.63 0.00 0.00 0.00 0.00 0.00
39 1 12 -2450.29 0.00 0.00 0.00 0.00 0.00
41 3003.53 0.00 0.00 0.00 0.00 0.00
2 12 -12640.00 0.00 0.00 0.00 0.00 0.00
41 12640.00 0.00 0.00 0.00 0.00 0.00
3 12 -15090.29 0.00 0.00 0.00 0.00 0.00
41 15643.52 0.00 0.00 0.00 0.00 0.00
40 1 14 -2098.96 0.00 0.00 0.00 0.00 0.00
42 2652.20 0.00 0.00 0.00 0.00 0.00
2 14 -12640.00 0.00 0.00 0.00 0.00 0.00
42 12640.00 0.00 0.00 0.00 0.00 0.00
3 14 -14738.96 0.00 0.00 0.00 0.00 0.00
42 15292.20 0.00 0.00 0.00 0.00 0.00
41 1 16 -1891.77 0.00 0.00 0.00 0.00 0.00
43 2445.00 0.00 0.00 0.00 0.00 0.00
2 16 -12640.00 0.00 0.00 0.00 0.00 0.00
43 12640.00 0.00 0.00 0.00 0.00 0.00
3 16 -14531.77 0.00 0.00 0.00 0.00 0.00
43 15085.00 0.00 0.00 0.00 0.00 0.00
42 1 17 -11372.23 0.00 0.00 0.00 0.00 0.00
44 11925.46 0.00 0.00 0.00 0.00 0.00
2 17 -25243.48 0.00 0.00 0.00 0.00 0.00
44 25243.48 0.00 0.00 0.00 0.00 0.00
3 17 -36615.71 0.00 0.00 0.00 0.00 0.00
44 37168.94 0.00 0.00 0.00 0.00 0.00
43 1 18 233462.70 0.00 0.00 0.00 0.00 0.00
45-230025.80 0.00 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 18
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 18 409926.25 0.00 0.00 0.00 0.00 0.00
45-409926.25 0.00 0.00 0.00 0.00 0.00
3 18 643388.94 0.00 0.00 0.00 0.00 0.00
45-639952.06 0.00 0.00 0.00 0.00 0.00
44 1 19 -11372.23 0.00 0.00 0.00 0.00 0.00
46 11925.46 0.00 0.00 0.00 0.00 0.00
2 19 -25464.38 0.00 0.00 0.00 0.00 0.00
46 25464.38 0.00 0.00 0.00 0.00 0.00
3 19 -36836.61 0.00 0.00 0.00 0.00 0.00
46 37389.84 0.00 0.00 0.00 0.00 0.00
45 1 20 -1891.77 0.00 0.00 0.00 0.00 0.00
47 2445.00 0.00 0.00 0.00 0.00 0.00
2 20 -12340.00 0.00 0.00 0.00 0.00 0.00
47 12340.00 0.00 0.00 0.00 0.00 0.00
3 20 -14231.77 0.00 0.00 0.00 0.00 0.00
47 14785.00 0.00 0.00 0.00 0.00 0.00
46 1 22 -2098.96 0.00 0.00 0.00 0.00 0.00
48 2652.20 0.00 0.00 0.00 0.00 0.00
2 22 -12340.00 0.00 0.00 0.00 0.00 0.00
48 12340.00 0.00 0.00 0.00 0.00 0.00
3 22 -14438.96 0.00 0.00 0.00 0.00 0.00
48 14992.20 0.00 0.00 0.00 0.00 0.00
47 1 24 -2450.29 0.00 0.00 0.00 0.00 0.00
49 3003.53 0.00 0.00 0.00 0.00 0.00
2 24 -12340.00 0.00 0.00 0.00 0.00 0.00
49 12340.00 0.00 0.00 0.00 0.00 0.00
3 24 -14790.29 0.00 0.00 0.00 0.00 0.00
49 15343.53 0.00 0.00 0.00 0.00 0.00
48 1 26 -2558.39 0.00 0.00 0.00 0.00 0.00
50 3111.63 0.00 0.00 0.00 0.00 0.00
2 26 -12340.00 0.00 0.00 0.00 0.00 0.00
50 12340.00 0.00 0.00 0.00 0.00 0.00
3 26 -14898.39 0.00 0.00 0.00 0.00 0.00
50 15451.63 0.00 0.00 0.00 0.00 0.00
49 1 28 -2450.29 0.00 0.00 0.00 0.00 0.00
51 3003.53 0.00 0.00 0.00 0.00 0.00
2 28 -12340.00 0.00 0.00 0.00 0.00 0.00
51 12340.00 0.00 0.00 0.00 0.00 0.00
3 28 -14790.29 0.00 0.00 0.00 0.00 0.00
51 15343.53 0.00 0.00 0.00 0.00 0.00
50 1 30 -2098.96 0.00 0.00 0.00 0.00 0.00
52 2652.20 0.00 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 19
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 30 -21800.00 0.00 0.00 0.00 0.00 0.00
52 21800.00 0.00 0.00 0.00 0.00 0.00
3 30 -23898.96 0.00 0.00 0.00 0.00 0.00
52 24452.20 0.00 0.00 0.00 0.00 0.00
51 1 32 -1891.77 0.00 0.00 0.00 0.00 0.00
53 2445.00 0.00 0.00 0.00 0.00 0.00
2 32 -11120.00 0.00 0.00 0.00 0.00 0.00
53 11120.00 0.00 0.00 0.00 0.00 0.00
3 32 -13011.77 0.00 0.00 0.00 0.00 0.00
53 13565.00 0.00 0.00 0.00 0.00 0.00
52 1 33 257.67 0.00 0.00 0.00 0.00 0.00
54 295.56 0.00 0.00 0.00 0.00 0.00
2 33 1003.76 0.00 0.00 0.00 0.00 0.00
54 -1003.76 0.00 0.00 0.00 0.00 0.00
3 33 1261.43 0.00 0.00 0.00 0.00 0.00
54 -708.20 0.00 0.00 0.00 0.00 0.00
53 1 34 -945.88 0.00 0.00 0.00 0.00 0.00
55 4382.79 0.00 0.00 0.00 0.00 0.00
2 34 -4410.00 0.00 0.00 0.00 0.00 0.00
55 4410.00 0.00 0.00 0.00 0.00 0.00
3 34 -5355.88 0.00 0.00 0.00 0.00 0.00
55 8792.79 0.00 0.00 0.00 0.00 0.00
54 1 36 -550.05 0.00 0.00 0.00 0.00 0.00
56 1103.29 0.00 0.00 0.00 0.00 0.00
2 36 -3405.34 0.00 0.00 0.00 0.00 0.00
56 3405.34 0.00 0.00 0.00 0.00 0.00
3 36 -3955.40 0.00 0.00 0.00 0.00 0.00
56 4508.63 0.00 0.00 0.00 0.00 0.00
55 1 35 -3604.37 628.61 0.00 0.00 0.00 0.00
56 4970.91 628.61 0.00 0.00 0.00 0.00
2 35 -9713.03 0.00 0.00 0.00 0.00 0.00
56 9713.03 0.00 0.00 0.00 0.00 0.00
3 35 -13317.40 628.61 0.00 0.00 0.00 0.00
56 14683.94 628.61 0.00 0.00 0.00 0.00
56 1 56 -9180.29 890.93 0.00 0.00 0.00 0.00
57 9180.29 890.93 0.00 0.00 0.00 0.00
2 56 -16285.45 0.00 0.00 0.00 0.00 0.00
57 16285.45 0.00 0.00 0.00 0.00 0.00
3 56 -25465.74 890.93 0.00 0.00 0.00 0.00
57 25465.74 890.93 0.00 0.00 0.00 0.00
57 1 57 -9180.29 890.93 0.00 0.00 0.00 0.00
58 9180.29 890.93 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 20
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 57 -16285.45 0.00 0.00 0.00 0.00 0.00
58 16285.45 0.00 0.00 0.00 0.00 0.00
3 57 -25465.74 890.93 0.00 0.00 0.00 0.00
58 25465.74 890.93 0.00 0.00 0.00 0.00
58 1 58 -31472.27 685.00 0.00 0.00 0.00 0.00
59 31472.27 685.00 0.00 0.00 0.00 0.00
2 58 -58058.57 0.00 0.00 0.00 0.00 0.00
59 58058.57 0.00 0.00 0.00 0.00 0.00
3 58 -89530.83 685.00 0.00 0.00 0.00 0.00
59 89530.83 685.00 0.00 0.00 0.00 0.00
59 1 59 -31472.27 685.00 0.00 0.00 0.00 0.00
60 31472.27 685.00 0.00 0.00 0.00 0.00
2 59 -58058.57 0.00 0.00 0.00 0.00 0.00
60 58058.57 0.00 0.00 0.00 0.00 0.00
3 59 -89530.83 685.00 0.00 0.00 0.00 0.00
60 89530.83 685.00 0.00 0.00 0.00 0.00
60 1 60 -65844.26 835.26 0.00 0.00 0.00 0.00
61 65844.26 835.26 0.00 0.00 0.00 0.00
2 60-123992.12 0.00 0.00 0.00 0.00 0.00
61 123992.12 0.00 0.00 0.00 0.00 0.00
3 60-189836.39 835.26 0.00 0.00 0.00 0.00
61 189836.39 835.26 0.00 0.00 0.00 0.00
61 1 61 -65844.26 835.26 0.00 0.00 0.00 0.00
62 65844.26 835.26 0.00 0.00 0.00 0.00
2 61-123992.12 0.00 0.00 0.00 0.00 0.00
62 123992.12 0.00 0.00 0.00 0.00 0.00
3 61-189836.39 835.26 0.00 0.00 0.00 0.00
62 189836.39 835.26 0.00 0.00 0.00 0.00
62 1 62-112089.74 890.93 0.00 0.00 0.00 0.00
63 112089.74 890.93 0.00 0.00 0.00 0.00
2 62-212280.45 0.00 0.00 0.00 0.00 0.00
63 212280.45 0.00 0.00 0.00 0.00 0.00
3 62-324370.22 890.93 0.00 0.00 0.00 0.00
63 324370.22 890.93 0.00 0.00 0.00 0.00
63 1 63-112089.74 890.93 0.00 0.00 0.00 0.00
64 112089.74 890.93 0.00 0.00 0.00 0.00
2 63-212280.45 0.00 0.00 0.00 0.00 0.00
64 212280.45 0.00 0.00 0.00 0.00 0.00
3 63-324370.22 890.93 0.00 0.00 0.00 0.00
64 324370.22 890.93 0.00 0.00 0.00 0.00
64 1 64-170817.12 835.26 0.00 0.00 0.00 0.00
65 170817.12 835.26 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 21
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 64-324729.22 0.00 0.00 0.00 0.00 0.00
65 324729.22 0.00 0.00 0.00 0.00 0.00
3 64-495546.34 835.26 0.00 0.00 0.00 0.00
65 495546.34 835.26 0.00 0.00 0.00 0.00
65 1 65-170817.12 835.26 0.00 0.00 0.00 0.00
66 170817.12 835.26 0.00 0.00 0.00 0.00
2 65-324729.22 0.00 0.00 0.00 0.00 0.00
66 324729.22 0.00 0.00 0.00 0.00 0.00
3 65-495546.34 835.26 0.00 0.00 0.00 0.00
66 495546.34 835.26 0.00 0.00 0.00 0.00
66 1 66-241417.95 685.00 0.00 0.00 0.00 0.00
67 241417.95 685.00 0.00 0.00 0.00 0.00
2 66-459532.72 0.00 0.00 0.00 0.00 0.00
67 459532.72 0.00 0.00 0.00 0.00 0.00
3 66-700950.69 685.00 0.00 0.00 0.00 0.00
67 700950.69 685.00 0.00 0.00 0.00 0.00
67 1 67-241417.95 685.00 0.00 0.00 0.00 0.00
68 241417.95 685.00 0.00 0.00 0.00 0.00
2 67-459532.72 0.00 0.00 0.00 0.00 0.00
68 459532.72 0.00 0.00 0.00 0.00 0.00
3 67-700950.69 685.00 0.00 0.00 0.00 0.00
68 700950.69 685.00 0.00 0.00 0.00 0.00
68 1 68-324098.84 890.93 0.00 0.00 0.00 0.00
69 324098.84 890.93 0.00 0.00 0.00 0.00
2 68-618496.69 0.00 0.00 0.00 0.00 0.00
69 618496.69 0.00 0.00 0.00 0.00 0.00
3 68-942595.50 890.93 0.00 0.00 0.00 0.00
69 942595.50 890.93 0.00 0.00 0.00 0.00
69 1 69-324098.84 890.93 0.00 0.00 0.00 0.00
70 324098.84 890.93 0.00 0.00 0.00 0.00
2 69-618496.69 0.00 0.00 0.00 0.00 0.00
70 618496.69 0.00 0.00 0.00 0.00 0.00
3 69-942595.50 890.93 0.00 0.00 0.00 0.00
70 942595.50 890.93 0.00 0.00 0.00 0.00
70 1 70-432168.94 1715.20 0.00 0.00 0.00 0.00
71 432168.94 1715.20 0.00 0.00 0.00 0.00
2 70-823039.44 0.00 0.00 0.00 0.00 0.00
71 823039.44 0.00 0.00 0.00 0.00 0.00
3 70********** 1715.20 0.00 0.00 0.00 0.00
711255208.38 1715.20 0.00 0.00 0.00 0.00
71 1 71-432168.94 1715.20 0.00 0.00 0.00 0.00
72 432168.94 1715.20 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 22
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 71-823039.44 0.00 0.00 0.00 0.00 0.00
72 823039.44 0.00 0.00 0.00 0.00 0.00
3 71********** 1715.20 0.00 0.00 0.00 0.00
721255208.38 1715.20 0.00 0.00 0.00 0.00
72 1 72-324098.88 890.93 0.00 0.00 0.00 0.00
73 324098.88 890.93 0.00 0.00 0.00 0.00
2 72-616736.94 0.00 0.00 0.00 0.00 0.00
73 616736.94 0.00 0.00 0.00 0.00 0.00
3 72-940835.88 890.93 0.00 0.00 0.00 0.00
73 940835.88 890.93 0.00 0.00 0.00 0.00
73 1 73-324098.88 890.93 0.00 0.00 0.00 0.00
74 324098.88 890.93 0.00 0.00 0.00 0.00
2 73-616736.94 0.00 0.00 0.00 0.00 0.00
74 616736.94 0.00 0.00 0.00 0.00 0.00
3 73-940835.88 890.93 0.00 0.00 0.00 0.00
74 940835.88 890.93 0.00 0.00 0.00 0.00
74 1 74-241418.02 685.00 0.00 0.00 0.00 0.00
75 241418.02 685.00 0.00 0.00 0.00 0.00
2 74-454575.44 0.00 0.00 0.00 0.00 0.00
75 454575.44 0.00 0.00 0.00 0.00 0.00
3 74-695993.44 685.00 0.00 0.00 0.00 0.00
75 695993.44 685.00 0.00 0.00 0.00 0.00
75 1 75-241418.02 685.00 0.00 0.00 0.00 0.00
76 241418.02 685.00 0.00 0.00 0.00 0.00
2 75-454575.44 0.00 0.00 0.00 0.00 0.00
76 454575.44 0.00 0.00 0.00 0.00 0.00
3 75-695993.44 685.00 0.00 0.00 0.00 0.00
76 695993.44 685.00 0.00 0.00 0.00 0.00
76 1 76-170817.14 835.26 0.00 0.00 0.00 0.00
77 170817.14 835.26 0.00 0.00 0.00 0.00
2 76-317111.34 0.00 0.00 0.00 0.00 0.00
77 317111.34 0.00 0.00 0.00 0.00 0.00
3 76-487928.53 835.26 0.00 0.00 0.00 0.00
77 487928.53 835.26 0.00 0.00 0.00 0.00
77 1 77-170817.14 835.26 0.00 0.00 0.00 0.00
78 170817.14 835.26 0.00 0.00 0.00 0.00
2 77-317111.34 0.00 0.00 0.00 0.00 0.00
78 317111.34 0.00 0.00 0.00 0.00 0.00
3 77-487928.53 835.26 0.00 0.00 0.00 0.00
78 487928.53 835.26 0.00 0.00 0.00 0.00
78 1 78-112089.77 890.93 0.00 0.00 0.00 0.00
79 112089.77 890.93 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 23
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 78-200361.06 0.00 0.00 0.00 0.00 0.00
79 200361.06 0.00 0.00 0.00 0.00 0.00
3 78-312450.84 890.93 0.00 0.00 0.00 0.00
79 312450.84 890.93 0.00 0.00 0.00 0.00
79 1 79-112089.77 890.93 0.00 0.00 0.00 0.00
80 112089.77 890.93 0.00 0.00 0.00 0.00
2 79-200361.06 0.00 0.00 0.00 0.00 0.00
80 200361.06 0.00 0.00 0.00 0.00 0.00
3 79-312450.84 890.93 0.00 0.00 0.00 0.00
80 312450.84 890.93 0.00 0.00 0.00 0.00
80 1 80 -65844.30 835.26 0.00 0.00 0.00 0.00
81 65844.30 835.26 0.00 0.00 0.00 0.00
2 80-108308.16 0.00 0.00 0.00 0.00 0.00
81 108308.16 0.00 0.00 0.00 0.00 0.00
3 80-174152.45 835.26 0.00 0.00 0.00 0.00
81 174152.45 835.26 0.00 0.00 0.00 0.00
81 1 81 -65844.30 835.26 0.00 0.00 0.00 0.00
82 65844.30 835.26 0.00 0.00 0.00 0.00
2 81-108308.16 0.00 0.00 0.00 0.00 0.00
82 108308.16 0.00 0.00 0.00 0.00 0.00
3 81-174152.45 835.26 0.00 0.00 0.00 0.00
82 174152.45 835.26 0.00 0.00 0.00 0.00
82 1 82 -31472.29 685.00 0.00 0.00 0.00 0.00
83 31472.29 685.00 0.00 0.00 0.00 0.00
2 82 -36969.07 0.00 0.00 0.00 0.00 0.00
83 36969.07 0.00 0.00 0.00 0.00 0.00
3 82 -68441.36 685.00 0.00 0.00 0.00 0.00
83 68441.36 685.00 0.00 0.00 0.00 0.00
83 1 83 -31472.29 685.00 0.00 0.00 0.00 0.00
84 31472.29 685.00 0.00 0.00 0.00 0.00
2 83 -36969.07 0.00 0.00 0.00 0.00 0.00
84 36969.07 0.00 0.00 0.00 0.00 0.00
3 83 -68441.36 685.00 0.00 0.00 0.00 0.00
84 68441.36 685.00 0.00 0.00 0.00 0.00
84 1 84 -9180.29 890.93 0.00 0.00 0.00 0.00
85 9180.29 890.93 0.00 0.00 0.00 0.00
2 84 -3133.74 0.00 0.00 0.00 0.00 0.00
85 3133.74 0.00 0.00 0.00 0.00 0.00
3 84 -12314.03 890.93 0.00 0.00 0.00 0.00
85 12314.03 890.93 0.00 0.00 0.00 0.00
85 1 85 -9180.29 890.93 0.00 0.00 0.00 0.00
86 9180.29 890.93 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 24
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 85 -3133.74 0.00 0.00 0.00 0.00 0.00
86 3133.74 0.00 0.00 0.00 0.00 0.00
3 85 -12314.03 890.93 0.00 0.00 0.00 0.00
86 12314.03 890.93 0.00 0.00 0.00 0.00
86 1 86 -4970.91 628.61 0.00 0.00 0.00 0.00
55 3604.37 628.61 0.00 0.00 0.00 0.00
2 86 -2996.20 0.00 0.00 0.00 0.00 0.00
55 2996.20 0.00 0.00 0.00 0.00 0.00
3 86 -7967.12 628.61 0.00 0.00 0.00 0.00
55 6600.58 628.61 0.00 0.00 0.00 0.00
87 1 35 3739.30 504.47 0.00 0.00 0.00 0.00
2 -4835.98 504.47 0.00 0.00 0.00 0.00
2 35 9713.03 0.00 0.00 0.00 0.00 0.00
2 -9713.03 0.00 0.00 0.00 0.00 0.00
3 35 13452.33 504.47 0.00 0.00 0.00 0.00
2 -14549.01 504.47 0.00 0.00 0.00 0.00
88 1 2 -8684.92 504.47 0.00 0.00 0.00 0.00
37 9781.59 504.47 0.00 0.00 0.00 0.00
2 2 -22261.29 0.00 0.00 0.00 0.00 0.00
37 22261.29 0.00 0.00 0.00 0.00 0.00
3 2 -30946.21 504.47 0.00 0.00 0.00 0.00
37 32042.88 504.47 0.00 0.00 0.00 0.00
89 1 37 13995.70 504.47 0.00 0.00 0.00 0.00
4 -15092.38 504.47 0.00 0.00 0.00 0.00
2 37 22928.05 0.00 0.00 0.00 0.00 0.00
4 -22928.05 0.00 0.00 0.00 0.00 0.00
3 37 36923.75 504.47 0.00 0.00 0.00 0.00
4 -38020.42 504.47 0.00 0.00 0.00 0.00
90 1 4 -18615.92 378.35 0.00 0.00 0.00 0.00
38 19438.43 378.35 0.00 0.00 0.00 0.00
2 4 -40103.57 0.00 0.00 0.00 0.00 0.00
38 40103.57 0.00 0.00 0.00 0.00 0.00
3 4 -58719.50 378.35 0.00 0.00 0.00 0.00
38 59542.01 378.35 0.00 0.00 0.00 0.00
91 1 38 22635.05 378.35 0.00 0.00 0.00 0.00
7 -23457.56 378.35 0.00 0.00 0.00 0.00
2 38 39436.81 0.00 0.00 0.00 0.00 0.00
7 -39436.81 0.00 0.00 0.00 0.00 0.00
3 38 62071.86 378.35 0.00 0.00 0.00 0.00
7 -62894.38 378.35 0.00 0.00 0.00 0.00
92 1 7 -27186.53 315.29 0.00 0.00 0.00 0.00
39 27871.95 315.29 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 25
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 7 -56612.34 0.00 0.00 0.00 0.00 0.00
39 56612.34 0.00 0.00 0.00 0.00 0.00
3 7 -83798.87 315.29 0.00 0.00 0.00 0.00
39 84484.29 315.29 0.00 0.00 0.00 0.00
93 1 39 31586.67 315.29 0.00 0.00 0.00 0.00
9 -32272.10 315.29 0.00 0.00 0.00 0.00
2 39 57279.09 0.00 0.00 0.00 0.00 0.00
9 -57279.09 0.00 0.00 0.00 0.00 0.00
3 39 88865.77 315.29 0.00 0.00 0.00 0.00
9 -89551.19 315.29 0.00 0.00 0.00 0.00
94 1 9 -36255.20 315.29 0.00 0.00 0.00 0.00
40 36940.62 315.29 0.00 0.00 0.00 0.00
2 9 -74454.63 0.00 0.00 0.00 0.00 0.00
40 74454.63 0.00 0.00 0.00 0.00 0.00
3 9-110709.83 315.29 0.00 0.00 0.00 0.00
40 111395.26 315.29 0.00 0.00 0.00 0.00
95 1 40 40580.86 315.29 0.00 0.00 0.00 0.00
11 -41266.29 315.29 0.00 0.00 0.00 0.00
2 40 73787.86 0.00 0.00 0.00 0.00 0.00
11 -73787.86 0.00 0.00 0.00 0.00 0.00
3 40 114368.72 315.29 0.00 0.00 0.00 0.00
11-115054.15 315.29 0.00 0.00 0.00 0.00
96 1 11 -45249.38 315.29 0.00 0.00 0.00 0.00
41 45934.81 315.29 0.00 0.00 0.00 0.00
2 11 -90963.38 0.00 0.00 0.00 0.00 0.00
41 90963.38 0.00 0.00 0.00 0.00 0.00
3 11-136212.77 315.29 0.00 0.00 0.00 0.00
41 136898.19 315.29 0.00 0.00 0.00 0.00
97 1 41 49649.53 315.29 0.00 0.00 0.00 0.00
13 -50334.96 315.29 0.00 0.00 0.00 0.00
2 41 91630.15 0.00 0.00 0.00 0.00 0.00
13 -91630.15 0.00 0.00 0.00 0.00 0.00
3 41 141279.69 315.29 0.00 0.00 0.00 0.00
13-141965.09 315.29 0.00 0.00 0.00 0.00
98 1 13 -54063.93 378.35 0.00 0.00 0.00 0.00
42 54886.43 378.35 0.00 0.00 0.00 0.00
2 13-108805.66 0.00 0.00 0.00 0.00 0.00
42 108805.66 0.00 0.00 0.00 0.00 0.00
3 13-162869.59 378.35 0.00 0.00 0.00 0.00
42 163692.09 378.35 0.00 0.00 0.00 0.00
99 1 42 58083.05 378.35 0.00 0.00 0.00 0.00
15 -58905.55 378.35 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 27
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 21 109899.91 0.00 0.00 0.00 0.00 0.00
48-109899.91 0.00 0.00 0.00 0.00 0.00
3 21 168805.47 378.35 0.00 0.00 0.00 0.00
48-167982.97 378.35 0.00 0.00 0.00 0.00
107 1 48 -54886.44 378.35 0.00 0.00 0.00 0.00
23 54063.93 378.35 0.00 0.00 0.00 0.00
2 48-111370.84 0.00 0.00 0.00 0.00 0.00
23 111370.84 0.00 0.00 0.00 0.00 0.00
3 48-166257.28 378.35 0.00 0.00 0.00 0.00
23 165434.77 378.35 0.00 0.00 0.00 0.00
108 1 23 50334.96 315.29 0.00 0.00 0.00 0.00
49 -49649.54 315.29 0.00 0.00 0.00 0.00
2 23 94602.95 0.00 0.00 0.00 0.00 0.00
49 -94602.95 0.00 0.00 0.00 0.00 0.00
3 23 144937.91 315.29 0.00 0.00 0.00 0.00
49-144252.50 315.29 0.00 0.00 0.00 0.00
109 1 49 -45934.81 315.29 0.00 0.00 0.00 0.00
25 45249.39 315.29 0.00 0.00 0.00 0.00
2 49 -93132.03 0.00 0.00 0.00 0.00 0.00
25 93132.03 0.00 0.00 0.00 0.00 0.00
3 49-139066.84 315.29 0.00 0.00 0.00 0.00
25 138381.42 315.29 0.00 0.00 0.00 0.00
110 1 25 41266.29 315.29 0.00 0.00 0.00 0.00
50 -40580.87 315.29 0.00 0.00 0.00 0.00
2 25 76364.16 0.00 0.00 0.00 0.00 0.00
50 -76364.16 0.00 0.00 0.00 0.00 0.00
3 25 117630.45 315.29 0.00 0.00 0.00 0.00
50-116945.02 315.29 0.00 0.00 0.00 0.00
111 1 50 -36940.62 315.29 0.00 0.00 0.00 0.00
27 36255.20 315.29 0.00 0.00 0.00 0.00
2 50 -77835.09 0.00 0.00 0.00 0.00 0.00
27 77835.09 0.00 0.00 0.00 0.00 0.00
3 50-114775.71 315.29 0.00 0.00 0.00 0.00
27 114090.29 315.29 0.00 0.00 0.00 0.00
112 1 27 32272.11 315.29 0.00 0.00 0.00 0.00
51 -31586.68 315.29 0.00 0.00 0.00 0.00
2 27 61067.21 0.00 0.00 0.00 0.00 0.00
51 -61067.21 0.00 0.00 0.00 0.00 0.00
3 27 93339.31 315.29 0.00 0.00 0.00 0.00
51 -92653.88 315.29 0.00 0.00 0.00 0.00
113 1 51 -27871.96 315.29 0.00 0.00 0.00 0.00
29 27186.53 315.29 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 28
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 51 -59596.29 0.00 0.00 0.00 0.00 0.00
29 59596.29 0.00 0.00 0.00 0.00 0.00
3 51 -87468.24 315.29 0.00 0.00 0.00 0.00
29 86782.82 315.29 0.00 0.00 0.00 0.00
114 1 29 23457.56 378.35 0.00 0.00 0.00 0.00
52 -22635.05 378.35 0.00 0.00 0.00 0.00
2 29 39798.23 0.00 0.00 0.00 0.00 0.00
52 -39798.23 0.00 0.00 0.00 0.00 0.00
3 29 63255.79 378.35 0.00 0.00 0.00 0.00
52 -62433.29 378.35 0.00 0.00 0.00 0.00
115 1 52 -19438.44 378.35 0.00 0.00 0.00 0.00
31 18615.93 378.35 0.00 0.00 0.00 0.00
2 52 -37872.09 0.00 0.00 0.00 0.00 0.00
31 37872.09 0.00 0.00 0.00 0.00 0.00
3 52 -57310.54 378.35 0.00 0.00 0.00 0.00
31 56488.02 378.35 0.00 0.00 0.00 0.00
116 1 31 15092.39 504.47 0.00 0.00 0.00 0.00
53 -13995.72 504.47 0.00 0.00 0.00 0.00
2 31 9187.35 0.00 0.00 0.00 0.00 0.00
53 -9187.35 0.00 0.00 0.00 0.00 0.00
3 31 24279.74 504.47 0.00 0.00 0.00 0.00
53 -23183.06 504.47 0.00 0.00 0.00 0.00
117 1 53 -9781.59 504.47 0.00 0.00 0.00 0.00
33 8684.92 504.47 0.00 0.00 0.00 0.00
2 53 -17432.02 0.00 0.00 0.00 0.00 0.00
33 17432.02 0.00 0.00 0.00 0.00 0.00
3 53 -27213.61 504.47 0.00 0.00 0.00 0.00
33 26116.93 504.47 0.00 0.00 0.00 0.00
118 1 33 4835.98 504.47 0.00 0.00 0.00 0.00
55 -3739.30 504.47 0.00 0.00 0.00 0.00
2 33 2996.20 0.00 0.00 0.00 0.00 0.00
55 -2996.20 0.00 0.00 0.00 0.00 0.00
3 33 7832.19 504.47 0.00 0.00 0.00 0.00
55 -6735.51 504.47 0.00 0.00 0.00 0.00
119 1 37 2335.10 0.00 0.00 0.00 0.00 0.00
57 -1781.87 0.00 0.00 0.00 0.00 0.00
2 37 0.00 0.00 0.00 0.00 0.00 0.00
57 0.00 0.00 0.00 0.00 0.00 0.00
3 37 2335.10 0.00 0.00 0.00 0.00 0.00
57 -1781.87 0.00 0.00 0.00 0.00 0.00
120 1 38 1923.24 0.00 0.00 0.00 0.00 0.00
59 -1370.00 0.00 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 30
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 45 0.00 0.00 0.00 0.00 0.00 0.00
71 0.00 0.00 0.00 0.00 0.00 0.00
3 45 7159.11 0.00 0.00 0.00 0.00 0.00
71 -3430.41 0.00 0.00 0.00 0.00 0.00
128 1 46 -12179.95 0.00 0.00 0.00 0.00 0.00
72 12733.18 0.00 0.00 0.00 0.00 0.00
2 46 -25464.38 0.00 0.00 0.00 0.00 0.00
72 25464.38 0.00 0.00 0.00 0.00 0.00
3 46 -37644.33 0.00 0.00 0.00 0.00 0.00
72 38197.56 0.00 0.00 0.00 0.00 0.00
129 1 47 2335.10 0.00 0.00 0.00 0.00 0.00
73 -1781.87 0.00 0.00 0.00 0.00 0.00
2 47 0.00 0.00 0.00 0.00 0.00 0.00
73 0.00 0.00 0.00 0.00 0.00 0.00
3 47 2335.10 0.00 0.00 0.00 0.00 0.00
73 -1781.87 0.00 0.00 0.00 0.00 0.00
130 1 48 1923.24 0.00 0.00 0.00 0.00 0.00
75 -1370.00 0.00 0.00 0.00 0.00 0.00
2 48 0.00 0.00 0.00 0.00 0.00 0.00
75 0.00 0.00 0.00 0.00 0.00 0.00
3 48 1923.24 0.00 0.00 0.00 0.00 0.00
75 -1370.00 0.00 0.00 0.00 0.00 0.00
131 1 49 2223.76 0.00 0.00 0.00 0.00 0.00
77 -1670.52 0.00 0.00 0.00 0.00 0.00
2 49 0.00 0.00 0.00 0.00 0.00 0.00
77 0.00 0.00 0.00 0.00 0.00 0.00
3 49 2223.76 0.00 0.00 0.00 0.00 0.00
77 -1670.52 0.00 0.00 0.00 0.00 0.00
132 1 50 2335.10 0.00 0.00 0.00 0.00 0.00
79 -1781.87 0.00 0.00 0.00 0.00 0.00
2 50 0.00 0.00 0.00 0.00 0.00 0.00
79 0.00 0.00 0.00 0.00 0.00 0.00
3 50 2335.10 0.00 0.00 0.00 0.00 0.00
79 -1781.87 0.00 0.00 0.00 0.00 0.00
133 1 51 2223.76 0.00 0.00 0.00 0.00 0.00
81 -1670.52 0.00 0.00 0.00 0.00 0.00
2 51 0.00 0.00 0.00 0.00 0.00 0.00
81 0.00 0.00 0.00 0.00 0.00 0.00
3 51 2223.76 0.00 0.00 0.00 0.00 0.00
81 -1670.52 0.00 0.00 0.00 0.00 0.00
134 1 52 1923.24 0.00 0.00 0.00 0.00 0.00
83 -1370.00 0.00 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 31
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 52 0.00 0.00 0.00 0.00 0.00 0.00
83 0.00 0.00 0.00 0.00 0.00 0.00
3 52 1923.24 0.00 0.00 0.00 0.00 0.00
83 -1370.00 0.00 0.00 0.00 0.00 0.00
135 1 53 2335.10 0.00 0.00 0.00 0.00 0.00
85 -1781.87 0.00 0.00 0.00 0.00 0.00
2 53 0.00 0.00 0.00 0.00 0.00 0.00
85 0.00 0.00 0.00 0.00 0.00 0.00
3 53 2335.10 0.00 0.00 0.00 0.00 0.00
85 -1781.87 0.00 0.00 0.00 0.00 0.00
136 1 54 -550.05 0.00 0.00 0.00 0.00 0.00
86 1103.29 0.00 0.00 0.00 0.00 0.00
2 54 1003.76 0.00 0.00 0.00 0.00 0.00
86 -1003.76 0.00 0.00 0.00 0.00 0.00
3 54 453.71 0.00 0.00 0.00 0.00 0.00
86 99.52 0.00 0.00 0.00 0.00 0.00
137 1 35 0.00 254.49 0.00 0.00 0.00 0.00
36 0.00 254.49 0.00 0.00 0.00 0.00
2 35 0.00 0.00 0.00 0.00 0.00 0.00
36 0.00 0.00 0.00 0.00 0.00 0.00
3 35 0.00 254.49 0.00 0.00 0.00 0.00
36 0.00 254.49 0.00 0.00 0.00 0.00
138 1 56 8723.14 504.47 0.00 0.00 0.00 0.00
37 -9819.81 504.47 0.00 0.00 0.00 0.00
2 56 14340.29 0.00 0.00 0.00 0.00 0.00
37 -14340.29 0.00 0.00 0.00 0.00 0.00
3 56 23063.42 504.47 0.00 0.00 0.00 0.00
37 -24160.10 504.47 0.00 0.00 0.00 0.00
139 1 37 -13957.48 504.47 0.00 0.00 0.00 0.00
58 15054.15 504.47 0.00 0.00 0.00 0.00
2 37 -30849.05 0.00 0.00 0.00 0.00 0.00
58 30849.05 0.00 0.00 0.00 0.00 0.00
3 37 -44806.53 504.47 0.00 0.00 0.00 0.00
58 45903.21 504.47 0.00 0.00 0.00 0.00
140 1 58 18007.77 378.35 0.00 0.00 0.00 0.00
38 -18830.28 378.35 0.00 0.00 0.00 0.00
2 58 30849.06 0.00 0.00 0.00 0.00 0.00
38 -30849.06 0.00 0.00 0.00 0.00 0.00
3 58 48856.82 378.35 0.00 0.00 0.00 0.00
38 -49679.34 378.35 0.00 0.00 0.00 0.00
141 1 38 -23243.20 378.35 0.00 0.00 0.00 0.00
60 24065.71 378.35 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 32
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 38 -48691.34 0.00 0.00 0.00 0.00 0.00
60 48691.34 0.00 0.00 0.00 0.00 0.00
3 38 -71934.53 378.35 0.00 0.00 0.00 0.00
60 72757.05 378.35 0.00 0.00 0.00 0.00
142 1 60 26769.63 315.29 0.00 0.00 0.00 0.00
39 -27455.06 315.29 0.00 0.00 0.00 0.00
2 60 48691.34 0.00 0.00 0.00 0.00 0.00
39 -48691.34 0.00 0.00 0.00 0.00 0.00
3 60 75460.96 315.29 0.00 0.00 0.00 0.00
39 -76146.39 315.29 0.00 0.00 0.00 0.00
143 1 39 -32003.57 315.29 0.00 0.00 0.00 0.00
62 32688.99 315.29 0.00 0.00 0.00 0.00
2 39 -65200.10 0.00 0.00 0.00 0.00 0.00
62 65200.10 0.00 0.00 0.00 0.00 0.00
3 39 -97203.66 315.29 0.00 0.00 0.00 0.00
62 97889.09 315.29 0.00 0.00 0.00 0.00
144 1 62 35614.73 315.29 0.00 0.00 0.00 0.00
40 -36300.16 315.29 0.00 0.00 0.00 0.00
2 62 65200.11 0.00 0.00 0.00 0.00 0.00
40 -65200.11 0.00 0.00 0.00 0.00 0.00
3 62 100814.84 315.29 0.00 0.00 0.00 0.00
40-101500.27 315.29 0.00 0.00 0.00 0.00
145 1 40 -41221.33 315.29 0.00 0.00 0.00 0.00
64 41906.75 315.29 0.00 0.00 0.00 0.00
2 40 -83042.38 0.00 0.00 0.00 0.00 0.00
64 83042.38 0.00 0.00 0.00 0.00 0.00
3 40-124263.71 315.29 0.00 0.00 0.00 0.00
64 124949.14 315.29 0.00 0.00 0.00 0.00
146 1 64 44832.49 315.29 0.00 0.00 0.00 0.00
41 -45517.91 315.29 0.00 0.00 0.00 0.00
2 64 83042.38 0.00 0.00 0.00 0.00 0.00
41 -83042.38 0.00 0.00 0.00 0.00 0.00
3 64 127874.88 315.29 0.00 0.00 0.00 0.00
41-128560.30 315.29 0.00 0.00 0.00 0.00
147 1 41 -50066.43 315.29 0.00 0.00 0.00 0.00
66 50751.85 315.29 0.00 0.00 0.00 0.00
2 41 -99551.15 0.00 0.00 0.00 0.00 0.00
66 99551.15 0.00 0.00 0.00 0.00 0.00
3 41-149617.58 315.29 0.00 0.00 0.00 0.00
66 150303.00 315.29 0.00 0.00 0.00 0.00
148 1 66 53455.77 378.35 0.00 0.00 0.00 0.00
42 -54278.28 378.35 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 33
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 66 99551.15 0.00 0.00 0.00 0.00 0.00
42 -99551.15 0.00 0.00 0.00 0.00 0.00
3 66 153006.92 378.35 0.00 0.00 0.00 0.00
42-153829.42 378.35 0.00 0.00 0.00 0.00
149 1 42 -58691.20 378.35 0.00 0.00 0.00 0.00
68 59513.71 378.35 0.00 0.00 0.00 0.00
2 42-117393.42 0.00 0.00 0.00 0.00 0.00
68 117393.42 0.00 0.00 0.00 0.00 0.00
3 42-176084.62 378.35 0.00 0.00 0.00 0.00
68 176907.14 378.35 0.00 0.00 0.00 0.00
150 1 68 62467.32 504.47 0.00 0.00 0.00 0.00
43 -63564.01 504.47 0.00 0.00 0.00 0.00
2 68 117393.42 0.00 0.00 0.00 0.00 0.00
43-117393.42 0.00 0.00 0.00 0.00 0.00
3 68 179860.75 504.47 0.00 0.00 0.00 0.00
43-180957.44 504.47 0.00 0.00 0.00 0.00
151 1 43 -67701.70 504.47 0.00 0.00 0.00 0.00
70 68798.38 504.47 0.00 0.00 0.00 0.00
2 43-133902.25 0.00 0.00 0.00 0.00 0.00
70 133902.25 0.00 0.00 0.00 0.00 0.00
3 43-201603.95 504.47 0.00 0.00 0.00 0.00
70 202700.61 504.47 0.00 0.00 0.00 0.00
152 1 70 90684.20 628.61 0.00 0.00 0.00 0.00
45 -92050.73 628.61 0.00 0.00 0.00 0.00
2 70 168203.61 0.00 0.00 0.00 0.00 0.00
45-168203.61 0.00 0.00 0.00 0.00 0.00
3 70 258887.80 628.61 0.00 0.00 0.00 0.00
45-260254.33 628.61 0.00 0.00 0.00 0.00
153 1 45 92050.74 628.61 0.00 0.00 0.00 0.00
72 -90684.20 628.61 0.00 0.00 0.00 0.00
2 45 169653.31 0.00 0.00 0.00 0.00 0.00
72-169653.31 0.00 0.00 0.00 0.00 0.00
3 45 261704.06 628.61 0.00 0.00 0.00 0.00
72-260337.50 628.61 0.00 0.00 0.00 0.00
154 1 72 -68798.35 504.47 0.00 0.00 0.00 0.00
47 67701.67 504.47 0.00 0.00 0.00 0.00
2 72-135051.73 0.00 0.00 0.00 0.00 0.00
47 135051.73 0.00 0.00 0.00 0.00 0.00
3 72-203850.08 504.47 0.00 0.00 0.00 0.00
47 202753.41 504.47 0.00 0.00 0.00 0.00
155 1 47 63564.01 504.47 0.00 0.00 0.00 0.00
74 -62467.33 504.47 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 34
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 47 119754.77 0.00 0.00 0.00 0.00 0.00
74-119754.77 0.00 0.00 0.00 0.00 0.00
3 47 183318.78 504.47 0.00 0.00 0.00 0.00
74-182222.09 504.47 0.00 0.00 0.00 0.00
156 1 74 -59513.72 378.35 0.00 0.00 0.00 0.00
48 58691.21 378.35 0.00 0.00 0.00 0.00
2 74-119754.77 0.00 0.00 0.00 0.00 0.00
48 119754.77 0.00 0.00 0.00 0.00 0.00
3 74-179268.48 378.35 0.00 0.00 0.00 0.00
48 178445.98 378.35 0.00 0.00 0.00 0.00
157 1 48 54278.29 378.35 0.00 0.00 0.00 0.00
76 -53455.77 378.35 0.00 0.00 0.00 0.00
2 48 101515.98 0.00 0.00 0.00 0.00 0.00
76-101515.98 0.00 0.00 0.00 0.00 0.00
3 48 155794.25 378.35 0.00 0.00 0.00 0.00
76-154971.75 378.35 0.00 0.00 0.00 0.00
158 1 76 -50751.85 315.29 0.00 0.00 0.00 0.00
49 50066.43 315.29 0.00 0.00 0.00 0.00
2 76-101515.98 0.00 0.00 0.00 0.00 0.00
49 101515.98 0.00 0.00 0.00 0.00 0.00
3 76-152267.83 315.29 0.00 0.00 0.00 0.00
49 151582.41 315.29 0.00 0.00 0.00 0.00
159 1 49 45517.92 315.29 0.00 0.00 0.00 0.00
78 -44832.50 315.29 0.00 0.00 0.00 0.00
2 49 86219.02 0.00 0.00 0.00 0.00 0.00
78 -86219.02 0.00 0.00 0.00 0.00 0.00
3 49 131736.94 315.29 0.00 0.00 0.00 0.00
78-131051.52 315.29 0.00 0.00 0.00 0.00
160 1 78 -41906.76 315.29 0.00 0.00 0.00 0.00
50 41221.34 315.29 0.00 0.00 0.00 0.00
2 78 -86219.02 0.00 0.00 0.00 0.00 0.00
50 86219.02 0.00 0.00 0.00 0.00 0.00
3 78-128125.78 315.29 0.00 0.00 0.00 0.00
50 127440.35 315.29 0.00 0.00 0.00 0.00
161 1 50 36300.16 315.29 0.00 0.00 0.00 0.00
80 -35614.73 315.29 0.00 0.00 0.00 0.00
2 50 67980.22 0.00 0.00 0.00 0.00 0.00
80 -67980.22 0.00 0.00 0.00 0.00 0.00
3 50 104280.38 315.29 0.00 0.00 0.00 0.00
80-103594.95 315.29 0.00 0.00 0.00 0.00
162 1 80 -32689.00 315.29 0.00 0.00 0.00 0.00
51 32003.57 315.29 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 35
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 80 -67980.22 0.00 0.00 0.00 0.00 0.00
51 67980.22 0.00 0.00 0.00 0.00 0.00
3 80-100669.21 315.29 0.00 0.00 0.00 0.00
51 99983.80 315.29 0.00 0.00 0.00 0.00
163 1 51 27455.06 315.29 0.00 0.00 0.00 0.00
82 -26769.64 315.29 0.00 0.00 0.00 0.00
2 51 52683.27 0.00 0.00 0.00 0.00 0.00
82 -52683.27 0.00 0.00 0.00 0.00 0.00
3 51 80138.33 315.29 0.00 0.00 0.00 0.00
82 -79452.91 315.29 0.00 0.00 0.00 0.00
164 1 82 -24065.72 378.35 0.00 0.00 0.00 0.00
52 23243.21 378.35 0.00 0.00 0.00 0.00
2 82 -52683.27 0.00 0.00 0.00 0.00 0.00
52 52683.27 0.00 0.00 0.00 0.00 0.00
3 82 -76748.98 378.35 0.00 0.00 0.00 0.00
52 75926.48 378.35 0.00 0.00 0.00 0.00
165 1 52 18830.28 378.35 0.00 0.00 0.00 0.00
84 -18007.78 378.35 0.00 0.00 0.00 0.00
2 52 24987.06 0.00 0.00 0.00 0.00 0.00
84 -24987.06 0.00 0.00 0.00 0.00 0.00
3 52 43817.34 378.35 0.00 0.00 0.00 0.00
84 -42994.84 378.35 0.00 0.00 0.00 0.00
166 1 84 -15054.17 504.47 0.00 0.00 0.00 0.00
53 13957.50 504.47 0.00 0.00 0.00 0.00
2 84 -24987.08 0.00 0.00 0.00 0.00 0.00
53 24987.08 0.00 0.00 0.00 0.00 0.00
3 84 -40041.26 504.47 0.00 0.00 0.00 0.00
53 38944.58 504.47 0.00 0.00 0.00 0.00
167 1 53 9819.81 504.47 0.00 0.00 0.00 0.00
86 -8723.13 504.47 0.00 0.00 0.00 0.00
2 53 1632.27 0.00 0.00 0.00 0.00 0.00
86 -1632.27 0.00 0.00 0.00 0.00 0.00
3 53 11452.08 504.47 0.00 0.00 0.00 0.00
86 -10355.40 504.47 0.00 0.00 0.00 0.00
168 1 4 31884.02 1049.48 0.00 0.00 0.00 0.00
6 -31884.02 1049.48 0.00 0.00 0.00 0.00
2 4 64324.40 0.00 0.00 0.00 0.00 0.00
6 -64324.40 0.00 0.00 0.00 0.00 0.00
3 4 96208.42 1049.48 0.00 0.00 0.00 0.00
6 -96208.42 1049.48 0.00 0.00 0.00 0.00
169 1 55 0.00 254.49 0.00 0.00 0.00 0.00
54 0.00 254.49 0.00 0.00 0.00 0.00
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DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 36
MEMBER END FORCES STRUCTURE TYPE = SPACE
-----------------
ALL UNITS ARE -- KG MMS
MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
2 55 0.00 0.00 0.00 0.00 0.00 0.00
54 0.00 0.00 0.00 0.00 0.00 0.00
3 55 0.00 254.49 0.00 0.00 0.00 0.00
54 0.00 254.49 0.00 0.00 0.00 0.00
170 1 44 0.00 254.49 0.00 0.00 0.00 0.00
45 0.00 254.49 0.00 0.00 0.00 0.00
2 44 0.00 0.00 0.00 0.00 0.00 0.00
45 0.00 0.00 0.00 0.00 0.00 0.00
3 44 0.00 254.49 0.00 0.00 0.00 0.00
45 0.00 254.49 0.00 0.00 0.00 0.00
171 1 45 0.00 254.49 0.00 0.00 0.00 0.00
46 0.00 254.49 0.00 0.00 0.00 0.00
2 45 0.00 0.00 0.00 0.00 0.00 0.00
46 0.00 0.00 0.00 0.00 0.00 0.00
3 45 0.00 254.49 0.00 0.00 0.00 0.00
46 0.00 254.49 0.00 0.00 0.00 0.00
************** END OF LATEST ANALYSIS RESULT **************
150. FINISH
*********** END OF THE STAAD.Pro RUN ***********
**** DATE= FEB 1,2008 TIME= 17:31:20 ****
*********************************************************
* For questions on STAAD.Pro, please contact : *
* By Email - North America : [email protected] *
* By Email - International : [email protected] *
* Tel. (USA) : 714-974-2500 ; Fax (USA) : 714-974-4771 *
*********************************************************
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Software licensed to (
Job Title
Client
Cantilever Erection Span 92m
RVNL
Print Time/Date: 02/02/2008 10:26 STAAD.Pro for Windows Release 2003
56 656463626160595857 66
49484746
67 77 7876
45
7574737271706968
44
13 222120193181716151412 2311109876432 24
434241403938373635
1 25
X
Y
Z
Whole Structure
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BOTTOM CHORD L0-L3
Section element Rotationangle
Mirror Material E (kg/mm^2)
Sheet 20 x 750 Steel 20897.044Sheet 20 x 750 Steel 20897.044Sheet 150 x 20 Steel 20897.044Sheet 150 x 20 Steel 20897.044
Sheet 150 x 20 Steel 20897.044Sheet 150 x 20 Steel 20897.044
The overall dimentions of the section are 650.0 x 750.0 mm
Basic geometry of the sectionParameter Value
A Sectional area 42000.0 mm2
Angle of principal inertia axes -90.0 deg
Iy Inertia moment about centroidal Y1-axis parallel with Y-axis 3005350000.04
Iz Inertia moment about centroidal Z1-axis parallel with Z-axis 3635050000.04
It Torsional moment of inertia (St. Venant) 5226666.667 mm4
iy Radius of inertia about Y1-axis 267.499 mm
iz Radius of inertia about Z1-axis 294.192 mm
Wu+ Maximum resisting moment about U-axis11184769.231
3
Wu- Minimum resisting moment about U-axis 11184769.2313
Wv+ Maximum resisting moment about V-axis 8014266.667 mm3
Wv- Minimum resisting moment about V-axis 8014266.667 mm3
Wpl,u Plastic resisting moment about U-axis 12210000.0 mm3
Wpl,v Plastic resisting moment about V-axis 10003539.6 mm3
Iu Maximum inertia moment 3635050000.04
Iv Minimum inertia moment 3005350000.04
iu Maximum radius of inertia 294.192 mm
iv Minimum radius of inertia 267.499 mm
au+ Middle point along positive direction of Y(U)-axis 190.816 mm
au- Middle point along negative direction of Y(U)-axis 190.816 mm
av+ Middle point along positive direction of Z(V)-axis 266.304 mm
av- Middle point along negative direction of Z(V)-axis 266.304 mm
yM Coordinate of the center of gravity along Y-axis325.0
mm
zM Coordinate of the center of gravity along Z-axis -375.0 mm
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L0-L1.sec
U
V
Z
Y
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BOTTOM CHORD L5-L7
Section element Rotationangle
Mirror Material E (kg/mm^2)
Sheet 16 x 750 Steel 20897.044Sheet 16 x 750 Steel 20897.044Sheet 150 x 16 Steel 20897.044Sheet 150 x 16 Steel 20897.044
Sheet 150 x 16 Steel 20897.044Sheet 150 x 16 Steel 20897.044Sheet 16 x 650 Steel 20897.044Sheet 16 x 650 Steel 20897.044
The overall dimentions of the section are 650.0 x 750.0 mm
Basic geometry of the sectionParameter Value
A Sectional area 54400.0 mm2
Angle of principal inertia axes -90.0 deg
Iy Inertia moment about centroidal Y1-axis parallel with Y-axis 3150552533.333 04
Iz Inertia moment about centroidal Z1-axis parallel with Z-axis 4840850133.333 04
It Torsional moment of inertia (St. Venant) 4362226.554 mm4
iy Radius of inertia about Y1-axis240.654
mm
iz Radius of inertia about Z1-axis 298.306 mm
Wu+ Maximum resisting moment about U-axis 14894923.4873
Wu- Minimum resisting moment about U-axis 14894923.4873
Wv+ Maximum resisting moment about V-axis 8401473.422 mm3
Wv- Minimum resisting moment about V-axis 8401473.422 mm3
Wpl,u Plastic resisting moment about U-axis 16116163.2 mm3
Wpl,v Plastic resisting moment about V-axis 11404105.92 mm3
Iu Maximum inertia moment 4840850133.333 04
Iv Minimum inertia moment 3150552533.333 04
iu Maximum radius of inertia 298.306 mm
iv Minimum radius of inertia 240.654 mm
au+ Middle point along positive direction of Y(U)-axis 154.439 mm
au- Middle point along negative direction of Y(U)-axis 154.439 mm
av+ Middle point along positive direction of Z(V)-axis273.804
mm
av- Middle point along negative direction of Z(V)-axis 273.804 mm
yM Coordinate of the center of gravity along Y-axis 325.0 mm
zM Coordinate of the center of gravity along Z-axis -375.0 mm
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L5-L7.sec
U
V
Z
Y
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BOTTOM CHORD L7-L9
Section element Rotationangle
Mirror Material E (kg/mm^2)
Sheet 16 x 750 Steel 20897.044Sheet 16 x 750 Steel 20897.044Sheet 150 x 20 Steel 20897.044Sheet 150 x 20 Steel 20897.044
Sheet 150 x 20 Steel 20897.044Sheet 150 x 20 Steel 20897.044Sheet 16 x 650 Steel 20897.044Sheet 16 x 650 Steel 20897.044
The overall dimentions of the section are 650.0 x 750.0 mm
Basic geometry of the sectionParameter Value
A Sectional area 56800.0 mm2
Angle of principal inertia axes -90.0 deg
Iy Inertia moment about centroidal Y1-axis parallel with Y-axis 3456433333.333 04
Iz Inertia moment about centroidal Z1-axis parallel with Z-axis 4976764533.333 04
It Torsional moment of inertia (St. Venant) 5061605.754 mm4
iy Radius of inertia about Y1-axis246.683
mm
iz Radius of inertia about Z1-axis 296.005 mm
Wu+ Maximum resisting moment about U-axis 15313121.6413
Wu- Minimum resisting moment about U-axis 15313121.6413
Wv+ Maximum resisting moment about V-axis 9217155.556 mm3
Wv- Minimum resisting moment about V-axis 9217155.556 mm3
Wpl,u Plastic resisting moment about U-axis 16677763.2 mm3
Wpl,v Plastic resisting moment about V-axis 12260620.32 mm3
Iu Maximum inertia moment 4976764533.333 04
Iv Minimum inertia moment 3456433333.333 04
iu Maximum radius of inertia 296.005 mm
iv Minimum radius of inertia 246.683 mm
au+ Middle point along positive direction of Y(U)-axis 162.274 mm
au- Middle point along negative direction of Y(U)-axis 162.274 mm
av+ Middle point along positive direction of Z(V)-axis269.597
mm
av- Middle point along negative direction of Z(V)-axis 269.597 mm
yM Coordinate of the center of gravity along Y-axis 325.0 mm
zM Coordinate of the center of gravity along Z-axis -375.0 mm
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L7-L9.sec
U
V
Z
Y
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UPPER CHORD U1-U3
Section element Rotationangle
Mirror Material E (kg/mm^2)
Sheet 650 x 20 Steel 20897.044Sheet 16 x 680 Steel 20897.044Sheet 16 x 680 Steel 20897.044Sheet 150 x 16 Steel 20897.044
Sheet 150 x 16 Steel 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm
Basic geometry of the sectionParameter Value
A Sectional area 39560.0 mm2
Angle of principal inertia axes -90.0 deg
Iy Inertia moment about centroidal Y1-axis parallel with Y-axis 2739658426.424 04
Iz Inertia moment about centroidal Z1-axis parallel with Z-axis 2916641986.667 04
It Torsional moment of inertia (St. Venant) 3759516.755 mm4
iy Radius of inertia about Y1-axis 263.16 mm
iz Radius of inertia about Z1-axis271.527
mm
Wu+ Maximum resisting moment about U-axis 8974283.036 mm3
Wu- Minimum resisting moment about U-axis 8974283.036 mm3
Wv+ Maximum resisting moment about V-axis 6605851.68 mm3
Wv- Minimum resisting moment about V-axis 9603807.407 mm3
Wpl,u Plastic resisting moment about U-axis 10133620.0 mm3
Wpl,v Plastic resisting moment about V-axis 9407411.743 mm3
Iu Maximum inertia moment 2916641986.667 04
Iv Minimum inertia moment 2739658426.424 04
iu Maximum radius of inertia 271.527 mm
iv Minimum radius of inertia 263.16 mm
au+ Middle point along positive direction of Y(U)-axis 166.983 mm
au- Middle point along negative direction of Y(U)-axis 242.766 mm
av+ Middle point along positive direction of Z(V)-axis 226.852 mm
av- Middle point along negative direction of Z(V)-axis226.852
mm
yM Coordinate of the center of gravity along Y-axis 325.0 mm
zM Coordinate of the center of gravity along Z-axis -414.732 mm
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\U1-U3.sec
V
Z
Y
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UPPER CHORD U3-U5
Section element Rotationangle
Mirror Material E (kg/mm^2)
Sheet 650 x 16 Steel 20897.044Sheet 12 x 684 Steel 20897.044Sheet 12 x 684 Steel 20897.044Sheet 150 x 12 Steel 20897.044
Sheet 150 x 12 Steel 208