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
PROJ ECT PROJ ECT PROJ ECT PROJ ECT
RAIL VIKAS NIGAM LIMITED PMC : 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
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
Tension allowed = 630x2130x1.25 = 1677 t > 1256 t ok
EXTENSION PIECE ACROSS PIN HOLE Net area req’ :
= . 475 cm2 Try 2 additional plate 660x12 and 660x10 with each gusset with 250φ pin Gross area of main section Add. PL 2x66x(1.2+1) Deduction for holes 2x25x7.8 8x7.8x2.15
= 761.6 cm2 = 290.4 cm2 = 1052.0 cm2 =-390.00 cm2 =-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
LINK ACROSS PIN HOLE
Gross area of main section Add. PL 2x66x(1.2+1) Deduction for holes 2x25x7.8 8x7.8x2.35
= 761.6 cm2 = 290.4 cm2 = 1052.0 cm2 =-390.00 cm2 =-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
LINK PIN Material : carbon steel class 4 to IS-1875 or equivalent
LINK ARRANGEMENT (IN PLAN) e=
+ 4 = 90 mm
w1 = (½ x 1256) / 9.4
=66.81 t/cm
w2 = (½ x 1256) / 7.8
= 80.51 t/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)/( π x 253/32) = 3287 kg/cm2 < 2990 (table 1 ) x 1.25 (ok)
Shear stress on pin = 1256000/(2 x π/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 cm2 Bearing Stress on H.T.S Steel plate = 1256000/(2x195) = 3220 kg/cm2 < 2600 (table 1) x 1.25=3250 kg/cm2
BUFFER SLAB Material : Grade 58HTC to I.S 961 or equivalent with γst = 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/cm MA = (11.92 x 17.52) / 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/cm2 ∴t=
=
.
= 10.22 cm, Provide t= 100 mm
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
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
B.M
= 7.0 x
.
= 8631 cm3
+ 0.7 x
.
=11.38 + 3.7 = 15.08 tm Bending Stress = (15.08 x 105) / 8631 = 175 kg/cm2 < (2250 kg/cm2 (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
= 91.28 cm2
Area
= 2 x 45.64
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
LINK SHORTENING As per computer output , enclosed. Deflection at free end of cantilever span = 106.71 cm Shortening of link to neutralize this deflection = δ * h/L
where,
δ = 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
Saturday, February 02, 2008, 10:29 AM PAGE NO.
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**************************************************** * * * STAAD.Pro * * Version 2003 Bld 1001.US * * Proprietary Program of * * Research Engineers, Intl. * * Date= FEB 1, 2008 * * Time= 17:31:20 * * * * USER ID: * ****************************************************
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STAAD SPACE DXF IMPORT OF ACAD-89 SPAN.DXF START JOB INFORMATION JOB NAME CANTILEVER ERECTION SPAN 92M JOB CLIENT RVNL JOB NO AA JOB PART 0 JOB REF 0 ENGINEER NAME ADHI T ENGINEER DATE 31-JAN-08 END JOB INFORMATION INPUT WIDTH 79 OUTPUT WIDTH 118 OUTPUT WIDTH 72 UNIT METER KG JOINT COORDINATES 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 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 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 20 103.5 0 0; 21 109.25 0 0; 22 115 0 0; 23 120.75 0 0; 24 126.5 0 0 25 132.25 0 0; 26 138 0 0; 27 143.75 0 0; 28 149.5 0 0; 29 155.25 0 0 30 161 0 0; 31 166.75 0 0; 32 172.5 0 0; 33 178.25 0 0; 34 184 0 0 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 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 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 50 138 6.25 0; 51 149.5 6.25 0; 52 161 6.25 0; 53 172.5 6.25 0 54 178.25 6.25 0; 55 184 6.25 0; 56 5.75 12.5 0; 57 11.5 12.5 0 58 17.25 12.5 0; 59 23 12.5 0; 60 28.75 12.5 0; 61 34.5 12.5 0 62 40.25 12.5 0; 63 46 12.5 0; 64 51.75 12.5 0; 65 57.5 12.5 0 66 63.25 12.5 0; 67 69 12.5 0; 68 74.75 12.5 0; 69 80.5 12.5 0 70 86.25 12.5 0; 71 92 12.5 0; 72 97.75 12.5 0; 73 103.5 12.5 0 74 109.25 12.5 0; 75 115 12.5 0; 76 120.75 12.5 0; 77 126.5 12.5 0 78 132.25 12.5 0; 79 138 12.5 0; 80 143.75 12.5 0; 81 149.5 12.5 0 82 155.25 12.5 0; 83 161 12.5 0; 84 166.75 12.5 0; 85 172.5 12.5 0 86 178.25 12.5 0 MEMBER INCIDENCES 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 12 13 14; 13 14 15; 14 15 16; 15 16 17; 16 17 18; 17 18 19; 18 19 20; 19 20 21 20 21 22; 21 22 23; 22 23 24; 23 24 25; 24 25 26; 25 26 27; 26 27 28; 27 28 29 28 29 30; 29 30 31; 30 31 32; 31 32 33; 32 33 34; 33 1 35; 34 2 36; 35 3 37 36 6 38; 37 8 39; 38 10 40; 39 12 41; 40 14 42; 41 16 43; 42 17 44; 43 18 45 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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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF 42. 43. 44. 45. 46. 47. 48. 49. 50. 51. 52. 53. 54. 55. 56. 57. 58. 59. 60. 61. 62. 63. 64. 65. 66. 67. 68. 69. 70. 71. 72. 73. 74. 75. 76. 77. 78. 79. 80. 81. 82. 83. 84. 85. 86. 87. 88. 89. 90. 91. 92. 93. 94. 95. 96. 97.
-- PAGE NO.
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52 33 54; 53 34 55; 54 36 56; 55 35 56; 56 56 57; 57 57 58; 58 58 59; 59 59 60 60 61; 61 61 62; 62 62 63; 63 63 64; 64 64 65; 65 65 66; 66 66 67; 67 67 68 68 69; 69 69 70; 70 70 71; 71 71 72; 72 72 73; 73 73 74; 74 74 75; 75 75 76 76 77; 77 77 78; 78 78 79; 79 79 80; 80 80 81; 81 81 82; 82 82 83; 83 83 84 84 85; 85 85 86; 86 86 55; 87 35 2; 88 2 37; 89 37 4; 90 4 38; 91 38 7 92 7 39; 93 39 9; 94 9 40; 95 40 11; 96 11 41; 97 41 13; 98 13 42; 99 42 15 100 15 43; 101 43 17; 102 17 45; 103 45 19; 104 19 47; 105 47 21; 106 21 48 107 48 23; 108 23 49; 109 49 25; 110 25 50; 111 50 27; 112 27 51; 113 51 29 114 29 52; 115 52 31; 116 31 53; 117 53 33; 118 33 55; 119 37 57; 120 38 59 121 39 61; 122 40 63; 123 41 65; 124 42 67; 125 43 69; 126 44 70; 127 45 71 128 46 72; 129 47 73; 130 48 75; 131 49 77; 132 50 79; 133 51 81; 134 52 83 135 53 85; 136 54 86; 137 35 36; 138 56 37; 139 37 58; 140 58 38; 141 38 60 142 60 39; 143 39 62; 144 62 40; 145 40 64; 146 64 41; 147 41 66; 148 66 42 149 42 68; 150 68 43; 151 43 70; 152 70 45; 153 45 72; 154 72 47; 155 47 74 156 74 48; 157 48 76; 158 76 49; 159 49 78; 160 78 50; 161 50 80; 162 80 51 163 51 82; 164 82 52; 165 52 84; 166 84 53; 167 53 86; 168 4 6; 169 55 54 170 44 45; 171 45 46 UNIT MMS KG DEFINE MATERIAL START ISOTROPIC STEEL E 20904.2 POISSON 0.3 DENSITY 7.83341E-006 ALPHA 6.5E-006 DAMP 0.03 END DEFINE MATERIAL CONSTANTS MATERIAL STEEL MEMB 1 TO 3 5 TO 171 START USER TABLE TABLE 1 UNIT METER KG PRISMATIC L0-L1 0.042 0.00300535 0.003635 5.227E-006 0 0 0.75 0.65 L3-L5 0.0466 0.002876 0.004157 3.101E-006 0 0 0.75 0.65 L5-L7 0.0544 0.00315055 0.00484085 4.362E-006 0 0 0.75 0.65 L7-L9 0.0568 0.003456 0.004977 5.06161E-006 0 0 0.75 0.65 U1-U3 0.03956 0.00273966 0.00291664 3.75952E-006 0 0 0.7 0.65 U3-U5 0.030416 0.00212652 0.00224754 1.73941E-006 0 0 0.7 0.65 U5-U7 0.037088 0.00255131 0.00283797 2.97484E-006 0 0 0.7 0.65 U7-U9 0.03956 0.00273966 0.00291664 3.75952E-006 0 0 0.7 0.65 M0-L0 0.0702 0.00390456 0.00557558 8.78136E-006 0 0 0.7 0.65 M0-U1 0.027912 0.0019362 0.00216577 1.26135E-006 0 0 0.7 0.65 VERT 0.0113 2.60942E-005 0.000720414 3.54516E-007 0 0 0.25 0.65 DIL0-L3 0.0224 0.000524766 0.00183019 1.79125E-006 0 0 0.4 0.65
60 68 76 84
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF 98. 99. 100. 101. 102. 103. 104. 105. 106. 107. 108. 109. 110. 111. 112. 113. 114. 115. 116. 117. 118. 119. 120. 121. 122. 123. 124. 125. 126. 127. 128. 129. 130. 131. 132. 133. 134. 135. 136. 137. 138. 139. 140. 141. 142. 143. 144. 145. 146. 147. 148.
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3
DIL3-L5 0.0168 0.000399066 0.00139836 7.57914E-007 0 0 0.4 0.65 DIL5-L8 0.014 0.000334867 0.00117612 4.38745E-007 0 0 0.4 0.65 LINK 0.07616 0.0029347 0.0067379 8.56867E-006 0 0 0.68 0.65 END UNIT MMS KG MEMBER PROPERTY AMERICAN 1 TO 3 14 TO 19 30 TO 32 UPTABLE 1 L0-L1 5 12 13 20 21 28 29 168 UPTABLE 1 L3-L5 MEMBER PROPERTY AMERICAN 6 7 10 11 22 23 26 27 UPTABLE 1 L5-L7 8 9 24 25 UPTABLE 1 L7-L9 56 57 68 69 72 73 84 85 UPTABLE 1 U1-U3 58 59 66 67 74 75 82 83 UPTABLE 1 U3-U5 60 61 64 65 76 77 80 81 UPTABLE 1 U5-U7 62 63 78 79 UPTABLE 1 U7-U9 33 43 53 UPTABLE 1 M0-L0 55 86 152 153 UPTABLE 1 M0-U1 34 TO 42 44 TO 52 54 119 TO 126 128 TO 137 169 TO 171 UPTABLE 1 VERT 87 TO 89 100 TO 105 116 TO 118 138 139 150 151 154 155 166 167 UPTABLE 1 DIL0-L3 90 91 98 99 106 107 114 115 140 141 148 149 156 157 164 165 UPTABLE 1 DIL3-L5 92 TO 97 108 TO 113 142 TO 147 158 TO 163 UPTABLE 1 DIL5-L8 70 71 127 UPTABLE 1 LINK SUPPORTS 1 PINNED 18 FIXED BUT FX MX MY MZ UNIT METER KG MEMBER TRUSS 1 TO 3 5 TO 171 UNIT MMS KG LOAD 1 LOAD 1 DEAD LOAD SELFWEIGHT Y -1 LOAD 2 LOAD 2 ERECTION JOINT LOAD 1 18 FY -6320 2 TO 4 6 TO 17 FY -12640 19 TO 28 FY -12340 29 FY -14570 30 FY -21800 31 FY -21110 32 FY -11120 33 FY -9620 34 FY -4410 UNIT METER KG LOAD COMB 3 LOAD COMBINATION 1 1.0 2 1.0 UNIT MMS KG PERFORM ANALYSIS
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Saturday, February 02, 2008, 10:29 AM 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
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
JOINT DISPLACEMENT (CM -----------------JOINT
1
2
3
4
6
7
8
9
10
11
12
13
14
15
16
17
LOAD
1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3
X-TRANS
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 -0.0060 -0.0142 -0.0202 -0.0120 -0.0284 -0.0403 -0.0308 -0.0663 -0.0971 -0.0496 -0.1043 -0.1539 -0.0831 -0.1697 -0.2528 -0.1165 -0.2351 -0.3516 -0.1710 -0.3409 -0.5119 -0.2255 -0.4468 -0.6723 -0.3120 -0.6137 -0.9257 -0.3985 -0.7806 -1.1791 -0.5413 -1.0555 -1.5968 -0.6840 -1.3305 -2.0145 -0.8962 -1.7391 -2.6353 -1.1085 -2.1476 -3.2561
-- PAGE NO.
RADIANS)
Y-TRANS
0.0000 0.0000 0.0000 0.2373 0.4570 0.6944 0.4833 0.9161 1.3994 0.7428 1.4176 2.1604 1.0129 1.9287 2.9416 1.2741 2.4347 3.7088 1.5422 2.9445 4.4867 1.7806 3.4034 5.1840 2.0061 3.8351 5.8412 2.1635 4.1363 6.2998 2.2988 4.3949 6.6936 2.3067 4.4158 6.7225 2.2341 4.2713 6.5055 1.9247 3.6857 5.6104 1.4772 2.8276 4.3049 0.6638 1.2863 1.9502
5
STRUCTURE TYPE = SPACE
Z-TRANS
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
X-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
Y-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
Z-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
JOINT DISPLACEMENT (CM -----------------JOINT
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
LOAD
1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3
X-TRANS
-1.3765 -2.6603 -4.0368 -1.6445 -3.1730 -4.8175 -1.8567 -3.5800 -5.4367 -2.0689 -3.9870 -6.0559 -2.2117 -4.2592 -6.4709 -2.3544 -4.5315 -6.8859 -2.4409 -4.6942 -7.1352 -2.5274 -4.8569 -7.3844 -2.5819 -4.9572 -7.5391 -2.6364 -5.0574 -7.6939 -2.6699 -5.1146 -7.7844 -2.7033 -5.1717 -7.8750 -2.7221 -5.1987 -7.9208 -2.7409 -5.2256 -7.9666 -2.7469 -5.2347 -7.9816 -2.7529 -5.2438 -7.9967
-- PAGE NO.
RADIANS)
Y-TRANS
0.0000 0.0000 0.0000 -1.6374 -3.1190 -4.7564 -3.1252 -5.9820 -9.1071 -4.9789 -9.5248 -14.5037 -6.9707 -13.3475 -20.3182 -9.1993 -17.6107 -26.8100 -11.5084 -22.0259 -33.5343 -13.9449 -26.6694 -40.6143 -16.4035 -31.3741 -47.7776 -18.9302 -36.2038 -55.1340 -21.4698 -41.0309 -62.5007 -24.0391 -45.8920 -69.9311 -26.6015 -50.7971 -77.3986 -29.1728 -55.6300 -84.8028 -31.7335 -60.3931 -92.1266 -34.2807 -65.1344 -99.4151
6
STRUCTURE TYPE = SPACE
Z-TRANS
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
X-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
Y-ROTAN
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Z-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 6 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
JOINT DISPLACEMENT (CM -----------------JOINT
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
LOAD
1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3
X-TRANS
-- PAGE NO.
RADIANS)
Y-TRANS
-2.7529 -36.8192 -5.2438 -69.8954 -7.9967 -106.7146 -0.2452 0.0011 -0.4641 0.0061 -0.7094 0.0072 -0.2452 0.2374 -0.4641 0.4660 -0.7094 0.7034 -0.2489 0.4890 -0.4757 0.9495 -0.7245 1.4386 -0.2444 1.0192 -0.4771 1.9622 -0.7215 2.9813 -0.2309 1.5494 -0.4521 2.9779 -0.6830 4.5274 -0.2130 2.0136 -0.4216 3.8686 -0.6345 5.8822 -0.1850 2.3060 -0.3743 4.4283 -0.5592 6.7343 -0.1319 2.2404 -0.2713 4.3048 -0.4032 6.5452 -0.0351 1.4830 -0.0985 2.8611 -0.1336 4.3441 -0.1258 0.6946 -0.2681 1.3531 -0.3939 2.0478 -0.1258 -0.0987 -0.2681 -0.1746 -0.3939 -0.2733 -0.1258 -1.6066 -0.2681 -3.0516 -0.3939 -4.6582 -0.2165 -3.1194 -0.4399 -5.9493 -0.6564 -9.0687 -0.1197 -6.9644 -0.2599 -13.3149 -0.3796 -20.2792 -0.0666 -11.5012 -0.1733 -21.9932 -0.2400 -33.4944
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STRUCTURE TYPE = SPACE
Z-TRANS
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
X-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
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C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 7 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
JOINT DISPLACEMENT (CM -----------------JOINT
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
LOAD
1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3
X-TRANS
-- PAGE NO.
RADIANS)
Y-TRANS
-0.0387 -16.3960 -0.1059 -31.3415 -0.1445 -47.7374 -0.0207 -21.4626 -0.1079 -40.9982 -0.1286 -62.4608 -0.0072 -26.5952 -0.0450 -50.7394 -0.0522 -77.3346 -0.0028 -31.7278 -0.1050 -60.3637 -0.1077 -92.0915 -0.0064 -34.2806 -0.0788 -65.1370 -0.0852 -99.4176 -0.0064 -36.8181 -0.0788 -69.8935 -0.0852 -106.7116 -0.4952 0.2396 -0.9530 0.4750 -1.4482 0.7146 -0.4888 0.4836 -0.9417 0.9495 -1.4305 1.4331 -0.4824 0.7397 -0.9303 1.4438 -1.4128 2.1835 -0.4540 1.0148 -0.8778 1.9622 -1.3318 2.9770 -0.4255 1.2635 -0.8253 2.4425 -1.2508 3.7060 -0.3767 1.5443 -0.7334 2.9779 -1.1100 4.5222 -0.3278 1.7662 -0.6414 3.4092 -0.9693 5.1754 -0.2499 2.0082 -0.4938 3.8686 -0.7437 5.8767 -0.1720 2.1398 -0.3462 4.1267 -0.5182 6.2665 -0.0453 2.3008 -0.1054 4.4283 -0.1507 6.7291
8
STRUCTURE TYPE = SPACE
Z-TRANS
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
X-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
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Z-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 8 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
JOINT DISPLACEMENT (CM -----------------JOINT
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
LOAD
1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3
X-TRANS
0.0814 0.1355 0.2169 0.2997 0.5510 0.8508 0.5181 0.9666 1.4847 0.7434 1.3967 2.1401 0.9688 1.8267 2.7955 1.1248 2.1240 3.2488 1.2809 2.4212 3.7021 1.5063 2.8500 4.3563 1.7316 3.2789 5.0105 1.9499 3.6900 5.6399 2.1683 4.1010 6.2693 2.2950 4.3362 6.6312 2.4216 4.5714 6.9931 2.4996 4.7107 7.2103 2.5775 4.8500 7.4276 2.6264 4.9304 7.5567
-- PAGE NO.
RADIANS)
Y-TRANS
2.2597 4.3519 6.6116 2.2361 4.3048 6.5409 1.8366 3.5517 5.3883 1.4775 2.8611 4.3386 0.7276 1.4199 2.1475 -0.1008 -0.1746 -0.2754 -1.5736 -2.9843 -4.5579 -3.1249 -5.9493 -9.0742 -5.0670 -9.6657 -14.7326 -6.9687 -13.3149 -20.2836 -9.2463 -17.6605 -26.9068 -11.5064 -21.9932 -33.4996 -13.9686 -26.6984 -40.6670 -16.4014 -31.3415 -47.7429 -18.9447 -36.1689 -55.1136 -21.4677 -40.9982 -62.4660
9
STRUCTURE TYPE = SPACE
Z-TRANS
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
X-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
Y-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
Z-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 9 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
JOINT DISPLACEMENT (CM -----------------JOINT
82
83
84
85
86
LOAD
1 2 3 1 2 3 1 2 3 1 2 3 1 2 3
X-TRANS
2.6752 5.0107 7.6859 2.7036 5.0441 7.7478 2.7321 5.0776 7.8097 2.7385 5.0797 7.8182 2.7449 5.0819 7.8268
-- PAGE NO.
RADIANS)
Y-TRANS
-24.0497 -45.9151 -69.9648 -26.5996 -50.7394 -77.3390 -29.1759 -55.5342 -84.7101 -31.7332 -60.3637 -92.0969 -34.2784 -65.1397 -99.4181
10
STRUCTURE TYPE = SPACE
Z-TRANS
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
X-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
Y-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
Z-ROTAN
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 10 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
SUPPORT REACTIONS -UNIT KG ----------------JOINT
1
18
LOAD
1 2 3 1 2 3
FORCE-X
-- PAGE NO.
MMS
11
STRUCTURE TYPE = SPACE
FORCE-Y
FORCE-Z
MOM-X
MOM-Y
MOM Z
0.00 0.00 0.00 -7976.24 0.00 -7976.23 0.00 235354.48 0.00 416246.25 0.00 651600.75
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 11 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
1
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
1
1 2 1 2 1 2
0.00 0.00 0.00 0.00 0.00 0.00
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
2 9154.41 3 -9154.41 2 21648.42 3 -21648.42 2 30802.83 3 -30802.83
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
3 9154.41 4 -9154.41 3 21648.42 4 -21648.42 3 30802.83 4 -30802.83
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
6 31884.02 7 -31884.02 6 64324.40 7 -64324.40 6 96208.42 7 -96208.42
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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1225.15 1225.15 0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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8 66126.52 9 -66126.52 8 129355.09 9-129355.09 8 195481.62 9-195481.62
1225.15 1225.15 0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
9 112523.38 10-112523.38
1279.20 1279.20
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
1
3
1 2 3
1 2 3
6
1 2 3
7
1 2 3
8
MMS AXIAL
2
5
STRUCTURE TYPE = SPACE
JT
3
3
12
LOAD
2
2
-- PAGE NO.
1
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 12 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
9
1 2 3
10
1 2 3
11
1 2 3
12
1 2 3
13
1 2 3
14
1 2 3
15
1
JT
-- PAGE NO.
13
STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
9 218546.28 10-218546.28 9 331069.66 10-331069.66
0.00 0.00 1279.20 1279.20
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
10 112523.38 11-112523.38 10 218546.28 11-218546.28 10 331069.66 11-331069.66
1279.20 1279.20 0.00 0.00 1279.20 1279.20
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
11 171099.38 12-171099.38 11 330092.19 12-330092.19 11 501191.56 12-501191.56
1225.15 1225.15 0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
12 171099.38 13-171099.38 12 330092.19 13-330092.19 12 501191.56 13-501191.56
1225.15 1225.15 0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
13 241829.72 14-241829.72 13 465798.56 14-465798.56 13 707628.25 14-707628.25
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
14 241829.72 15-241829.72 14 465798.56 15-465798.56 14 707628.25 15-707628.25
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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15 324072.97 16-324072.97 15 623859.62 16-623859.62 15 947932.56 16-947932.56
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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16 324072.97 17-324072.97
945.89 945.89
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 13 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
16
1 2 3
17
1 2 3
18
1 2 3
19
1 2 3
20
1 2 3
21
1 2 3
22
1
JT
-- PAGE NO.
14
STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
16 623859.62 17-623859.62 16 947932.56 17-947932.56
0.00 0.00 945.89 945.89
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
17 409191.94 18-409191.94 17 782857.31 18-782857.31 171192049.12 18**********
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
18 409191.94 19-409191.94 18 782857.31 19-782857.31 181192049.12 19**********
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
19 324073.00 20-324073.00 19 621417.44 20-621417.44 19 945490.50 20-945490.50
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
20 324073.00 21-324073.00 20 621417.44 21-621417.44 20 945490.50 21-945490.50
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
21 241829.77 22-241829.77 21 461247.75 22-461247.75 21 703077.50 22-703077.50
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
22 241829.77 23-241829.77 22 461247.75 23-461247.75 22 703077.50 23-703077.50
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
23 171099.41 24-171099.41
1225.15 1225.15
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
23 321791.84 24-321791.84 23 492891.25 24-492891.25
0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
24 171099.41 25-171099.41 24 321791.84 25-321791.84 24 492891.25 25-492891.25
1225.15 1225.15 0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
25 112523.41 26-112523.41 25 207033.36 26-207033.36 25 319556.78 26-319556.78
1279.20 1279.20 0.00 0.00 1279.20 1279.20
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
26 112523.41 27-112523.41 26 207033.36 27-207033.36 26 319556.78 27-319556.78
1279.20 1279.20 0.00 0.00 1279.20 1279.20
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
27 66126.55 28 -66126.55 27 112988.66 28-112988.66 27 179115.22 28-179115.22
1225.15 1225.15 0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
28 66126.55 29 -66126.55 28 112988.66 29-112988.66 28 179115.22 29-179115.22
1225.15 1225.15 0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
29 31884.05 30 -31884.05 29 45692.97 30 -45692.97 29 77577.02 30 -77577.02
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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30 31884.05 31 -31884.05
1049.48 1049.48
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 15 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
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LOAD
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
30 45692.97 31 -45692.97 30 77577.02 31 -77577.02
0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
31 9154.41 32 -9154.41 31 13831.06 32 -13831.06 31 22985.47 32 -22985.47
945.89 945.89 0.00 0.00 945.89 945.89
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
32 9154.41 33 -9154.41 32 13831.06 33 -13831.06 32 22985.47 33 -22985.47
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
33 34 33 34 33 34
0.00 0.00 0.00 0.00 0.00 0.00
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
1 -945.88 35 4382.79 1 -14296.24 35 14296.24 1 -15242.12 35 18679.03
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
2 36 2 36 2 36
257.67 295.56 -3405.34 3405.34 -3147.67 3700.91
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
3 -1891.77 37 2445.00 3 -12640.00 37 12640.00 3 -14531.77 37 15085.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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6 38
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-2098.96 2652.20
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Page 16 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
6 -12640.00 38 12640.00 6 -14738.96 38 15292.20
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
8 -2450.29 39 3003.53 8 -12640.00 39 12640.00 8 -15090.29 39 15643.52
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
10 -2558.39 40 3111.63 10 -12640.00 40 12640.00 10 -15198.39 40 15751.63
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
12 -2450.29 41 3003.53 12 -12640.00 41 12640.00 12 -15090.29 41 15643.52
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
14 -2098.96 42 2652.20 14 -12640.00 42 12640.00 14 -14738.96 42 15292.20
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
16 -1891.77 43 2445.00 16 -12640.00 43 12640.00 16 -14531.77 43 15085.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
17 -11372.23 44 11925.46 17 -25243.48 44 25243.48 17 -36615.71 44 37168.94
0.00 0.00 0.00 0.00 0.00 0.00
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18 233462.70 45-230025.80
0.00 0.00
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0.00 0.00
0.00 0.00
0.00 0.00
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Page 17 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
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LOAD
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STRUCTURE TYPE = SPACE MMS AXIAL
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TORSION
MOM-Y
MOM-Z
18 409926.25 45-409926.25 18 643388.94 45-639952.06
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
19 -11372.23 46 11925.46 19 -25464.38 46 25464.38 19 -36836.61 46 37389.84
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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20 -1891.77 47 2445.00 20 -12340.00 47 12340.00 20 -14231.77 47 14785.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
22 -2098.96 48 2652.20 22 -12340.00 48 12340.00 22 -14438.96 48 14992.20
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
24 -2450.29 49 3003.53 24 -12340.00 49 12340.00 24 -14790.29 49 15343.53
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
26 -2558.39 50 3111.63 26 -12340.00 50 12340.00 26 -14898.39 50 15451.63
0.00 0.00 0.00 0.00 0.00 0.00
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28 -2450.29 51 3003.53 28 -12340.00 51 12340.00 28 -14790.29 51 15343.53
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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30 52
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0.00 0.00
-2098.96 2652.20
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
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STRUCTURE TYPE = SPACE MMS AXIAL
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SHEAR-Z
TORSION
MOM-Y
MOM-Z
30 -21800.00 52 21800.00 30 -23898.96 52 24452.20
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
32 -1891.77 53 2445.00 32 -11120.00 53 11120.00 32 -13011.77 53 13565.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
33 54 33 54 33 54
257.67 295.56 1003.76 -1003.76 1261.43 -708.20
0.00 0.00 0.00 0.00 0.00 0.00
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34 55 34 55 34 55
-945.88 4382.79 -4410.00 4410.00 -5355.88 8792.79
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36 56 36 56 36 56
-550.05 1103.29 -3405.34 3405.34 -3955.40 4508.63
0.00 0.00 0.00 0.00 0.00 0.00
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35 -3604.37 56 4970.91 35 -9713.03 56 9713.03 35 -13317.40 56 14683.94
628.61 628.61 0.00 0.00 628.61 628.61
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56 -9180.29 57 9180.29 56 -16285.45 57 16285.45 56 -25465.74 57 25465.74
890.93 890.93 0.00 0.00 890.93 890.93
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57 58
890.93 890.93
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-9180.29 9180.29
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
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LOAD
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
57 -16285.45 58 16285.45 57 -25465.74 58 25465.74
0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
58 -31472.27 59 31472.27 58 -58058.57 59 58058.57 58 -89530.83 59 89530.83
685.00 685.00 0.00 0.00 685.00 685.00
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59 -31472.27 60 31472.27 59 -58058.57 60 58058.57 59 -89530.83 60 89530.83
685.00 685.00 0.00 0.00 685.00 685.00
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60 -65844.26 61 65844.26 60-123992.12 61 123992.12 60-189836.39 61 189836.39
835.26 835.26 0.00 0.00 835.26 835.26
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61 -65844.26 62 65844.26 61-123992.12 62 123992.12 61-189836.39 62 189836.39
835.26 835.26 0.00 0.00 835.26 835.26
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62-112089.74 63 112089.74 62-212280.45 63 212280.45 62-324370.22 63 324370.22
890.93 890.93 0.00 0.00 890.93 890.93
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63-112089.74 64 112089.74 63-212280.45 64 212280.45 63-324370.22 64 324370.22
890.93 890.93 0.00 0.00 890.93 890.93
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64-170817.12 65 170817.12
835.26 835.26
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0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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LOAD
2 3
65
1 2 3
66
1 2 3
67
1 2 3
68
1 2 3
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
64-324729.22 65 324729.22 64-495546.34 65 495546.34
0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00
65-170817.12 66 170817.12 65-324729.22 66 324729.22 65-495546.34 66 495546.34
835.26 835.26 0.00 0.00 835.26 835.26
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66-241417.95 67 241417.95 66-459532.72 67 459532.72 66-700950.69 67 700950.69
685.00 685.00 0.00 0.00 685.00 685.00
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67-241417.95 68 241417.95 67-459532.72 68 459532.72 67-700950.69 68 700950.69
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
68-324098.84 69 324098.84 68-618496.69 69 618496.69 68-942595.50 69 942595.50
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
69-324098.84 70 324098.84 69-618496.69 70 618496.69 69-942595.50 70 942595.50
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
70-432168.94 71 432168.94 70-823039.44 71 823039.44 70********** 711255208.38
1715.20 1715.20 0.00 0.00 1715.20 1715.20
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
71-432168.94 72 432168.94
1715.20 1715.20
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 21 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
72
1 2 3
73
1 2 3
74
1 2 3
75
1 2 3
76
1 2 3
77
1 2 3
78
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
71-823039.44 72 823039.44 71********** 721255208.38
0.00 0.00 1715.20 1715.20
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
72-324098.88 73 324098.88 72-616736.94 73 616736.94 72-940835.88 73 940835.88
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
73-324098.88 74 324098.88 73-616736.94 74 616736.94 73-940835.88 74 940835.88
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
74-241418.02 75 241418.02 74-454575.44 75 454575.44 74-695993.44 75 695993.44
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
75-241418.02 76 241418.02 75-454575.44 76 454575.44 75-695993.44 76 695993.44
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
76-170817.14 77 170817.14 76-317111.34 77 317111.34 76-487928.53 77 487928.53
835.26 835.26 0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
77-170817.14 78 170817.14 77-317111.34 78 317111.34 77-487928.53 78 487928.53
835.26 835.26 0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
78-112089.77 79 112089.77
890.93 890.93
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 22 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
79
1 2 3
80
1 2 3
81
1 2 3
82
1 2 3
83
1 2 3
84
1 2 3
85
1
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-- PAGE NO.
23
STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
78-200361.06 79 200361.06 78-312450.84 79 312450.84
0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
79-112089.77 80 112089.77 79-200361.06 80 200361.06 79-312450.84 80 312450.84
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
80 -65844.30 81 65844.30 80-108308.16 81 108308.16 80-174152.45 81 174152.45
835.26 835.26 0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
81 -65844.30 82 65844.30 81-108308.16 82 108308.16 81-174152.45 82 174152.45
835.26 835.26 0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
82 -31472.29 83 31472.29 82 -36969.07 83 36969.07 82 -68441.36 83 68441.36
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
83 -31472.29 84 31472.29 83 -36969.07 84 36969.07 83 -68441.36 84 68441.36
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
84 -9180.29 85 9180.29 84 -3133.74 85 3133.74 84 -12314.03 85 12314.03
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
85 86
890.93 890.93
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
-9180.29 9180.29
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 23 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
86
1 2 3
87
1 2 3
88
1 2 3
89
1 2 3
90
1 2 3
91
1 2 3
92
1
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-- PAGE NO.
24
STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
85 -3133.74 86 3133.74 85 -12314.03 86 12314.03
0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
86 55 86 55 86 55
-4970.91 3604.37 -2996.20 2996.20 -7967.12 6600.58
628.61 628.61 0.00 0.00 628.61 628.61
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
35 3739.30 2 -4835.98 35 9713.03 2 -9713.03 35 13452.33 2 -14549.01
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
2 -8684.92 37 9781.59 2 -22261.29 37 22261.29 2 -30946.21 37 32042.88
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
37 13995.70 4 -15092.38 37 22928.05 4 -22928.05 37 36923.75 4 -38020.42
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
4 -18615.92 38 19438.43 4 -40103.57 38 40103.57 4 -58719.50 38 59542.01
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
38 22635.05 7 -23457.56 38 39436.81 7 -39436.81 38 62071.86 7 -62894.38
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
7 -27186.53 39 27871.95
315.29 315.29
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 24 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
93
1 2 3
94
1 2 3
95
1 2 3
96
1 2 3
97
1 2 3
98
1 2 3
99
1
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-- PAGE NO.
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
7 -56612.34 39 56612.34 7 -83798.87 39 84484.29
0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
39 31586.67 9 -32272.10 39 57279.09 9 -57279.09 39 88865.77 9 -89551.19
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
9 -36255.20 40 36940.62 9 -74454.63 40 74454.63 9-110709.83 40 111395.26
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
40 40580.86 11 -41266.29 40 73787.86 11 -73787.86 40 114368.72 11-115054.15
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
11 -45249.38 41 45934.81 11 -90963.38 41 90963.38 11-136212.77 41 136898.19
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
41 49649.53 13 -50334.96 41 91630.15 13 -91630.15 41 141279.69 13-141965.09
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
13 -54063.93 42 54886.43 13-108805.66 42 108805.66 13-162869.59 42 163692.09
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
42 58083.05 15 -58905.55
378.35 378.35
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 25 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
100
1 2 3
101
1 2 3
102
1 2 3
103
1 2 3
104
1 2 3
105
1 2 3
106
1
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-- PAGE NO.
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
42 108138.91 15-108138.91 42 166221.95 15-167044.45
0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
15 -62429.11 43 63525.78 15-125314.43 43 125314.43 15-187743.53 43 188840.22
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
43 67739.92 17 -68836.60 43 125981.26 17-125981.26 43 193721.19 17-194817.86
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
17 -56882.54 45 57979.21 17-108855.30 45 108855.30 17-165737.83 45 166834.52
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
45 -57979.21 19 56882.54 45-110305.00 19 110305.00 45-168284.22 19 167187.53
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
19 68836.57 47 -67739.89 19 128138.71 47-128138.71 19 196975.28 47-195878.59
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
47 -63525.79 21 62429.11 47-126667.79 21 126667.79 47-190193.58 21 189096.91
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
21 58905.56 48 -58083.05
378.35 378.35
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 26 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
107
1 2 3
108
1 2 3
109
1 2 3
110
1 2 3
111
1 2 3
112
1 2 3
113
1
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-- PAGE NO.
27
STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
21 109899.91 48-109899.91 21 168805.47 48-167982.97
0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
48 -54886.44 23 54063.93 48-111370.84 23 111370.84 48-166257.28 23 165434.77
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
23 50334.96 49 -49649.54 23 94602.95 49 -94602.95 23 144937.91 49-144252.50
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
49 -45934.81 25 45249.39 49 -93132.03 25 93132.03 49-139066.84 25 138381.42
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
25 41266.29 50 -40580.87 25 76364.16 50 -76364.16 25 117630.45 50-116945.02
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
50 -36940.62 27 36255.20 50 -77835.09 27 77835.09 50-114775.71 27 114090.29
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
27 32272.11 51 -31586.68 27 61067.21 51 -61067.21 27 93339.31 51 -92653.88
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
51 -27871.96 29 27186.53
315.29 315.29
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 27 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
114
1 2 3
115
1 2 3
116
1 2 3
117
1 2 3
118
1 2 3
119
1 2 3
120
1
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-- PAGE NO.
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
51 -59596.29 29 59596.29 51 -87468.24 29 86782.82
0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
29 23457.56 52 -22635.05 29 39798.23 52 -39798.23 29 63255.79 52 -62433.29
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
52 -19438.44 31 18615.93 52 -37872.09 31 37872.09 52 -57310.54 31 56488.02
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
31 15092.39 53 -13995.72 31 9187.35 53 -9187.35 31 24279.74 53 -23183.06
504.47 504.47 0.00 0.00 504.47 504.47
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38 59 38 59
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0.00 0.00 0.00 0.00
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40 63 40 63 40 63
2335.10 -1781.87 0.00 0.00 2335.10 -1781.87
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2223.76 -1670.52 0.00 0.00 2223.76 -1670.52
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45 71
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
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1
1 2 3
1 2 3
124
1 2 3
125
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3
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45 71 45 71
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2335.10 -1781.87 0.00 0.00 2335.10 -1781.87
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1 2 3
1 2 3
131
1 2 3
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52 83 52 83
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35 36 35 36 35 36
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254.49 254.49 0.00 0.00 254.49 254.49
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378.35 378.35
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0.00 0.00
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1
1 2 3
1 2 3
138
1 2 3
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141
MMS AXIAL
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STRUCTURE TYPE = SPACE
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38 -48691.34 60 48691.34 38 -71934.53 60 72757.05
0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
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60 26769.63 39 -27455.06 60 48691.34 39 -48691.34 60 75460.96 39 -76146.39
315.29 315.29 0.00 0.00 315.29 315.29
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315.29 315.29 0.00 0.00 315.29 315.29
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66 53455.77 42 -54278.28
378.35 378.35
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
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66 99551.15 42 -99551.15 66 153006.92 42-153829.42
0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
42 -58691.20 68 59513.71 42-117393.42 68 117393.42 42-176084.62 68 176907.14
378.35 378.35 0.00 0.00 378.35 378.35
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47 119754.77 74-119754.77 47 183318.78 74-182222.09
0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
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378.35 378.35 0.00 0.00 378.35 378.35
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378.35 378.35 0.00 0.00 378.35 378.35
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315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
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315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
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164
1 2 3
165
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MOM-Y
MOM-Z
80 -67980.22 51 67980.22 80-100669.21 51 99983.80
0.00 0.00 315.29 315.29
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82 -24065.72 52 23243.21 82 -52683.27 52 52683.27 82 -76748.98 52 75926.48
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0.00 0.00 0.00 0.00 0.00 0.00
52 18830.28 84 -18007.78 52 24987.06 84 -24987.06 52 43817.34 84 -42994.84
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
84 -15054.17 53 13957.50 84 -24987.08 53 24987.08 84 -40041.26 53 38944.58
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
53 9819.81 86 -8723.13 53 1632.27 86 -1632.27 53 11452.08 86 -10355.40
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
4 31884.02 6 -31884.02 4 64324.40 6 -64324.40 4 96208.42 6 -96208.42
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
254.49 254.49
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
55 54
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 35 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
STRUCTURE TYPE = SPACE MMS
JT
AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
2
55 54 55 54
0.00 0.00 0.00 0.00
0.00 0.00 254.49 254.49
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
44 45 44 45 44 45
0.00 0.00 0.00 0.00 0.00 0.00
254.49 254.49 0.00 0.00 254.49 254.49
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
45 46 45 46 45 46
0.00 0.00 0.00 0.00 0.00 0.00
254.49 254.49 0.00 0.00 254.49 254.49
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
1 2 3
171
36
LOAD
3
170
-- PAGE NO.
1 2 3
************** 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 * *********************************************************
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 36 of 36
Job No
Sheet No
Rev
2
AA Part 0
Software licensed to (ñ Job Title
Client
Cantilever Erection Span 92m
RVNL
Ref
0
By
Adhi T
File
structure span 92.std
Date31-Jan-08 Date/Time
Chd
01-Feb-2008 17:31
56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 35 36 37 1
2
3
38 4
6
39 7
8
40 9
41
42
43 44 45 46 47
48
50
51
52
53 54 55
10 11 12 13 14 15 16 17 318 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34
Load 3
Y Z
49
X
Whole Structure Print Time/Date: 02/02/2008 10:26
STAAD.Pro for Windows Release 2003
Print Run 2 of 2
Z
V
U
Y
BOTTOM CHORD L0-L3 Section element
Rotation angle
Mirror
Sheet 20 x 750 Sheet 20 x 750 Sheet 150 x 20 Sheet 150 x 20 Sheet 150 x 20 Sheet 150 x 20
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 750.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 42000.0 -90.0 3005350000.0 3635050000.0 5226666.667 267.499 294.192 11184769.231 11184769.231 8014266.667 8014266.667 12210000.0 10003539.6 3635050000.0 3005350000.0 294.192 267.499 190.816 190.816 266.304 266.304 325.0 -375.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L0-L1.sec
2
mm deg 4 4
mm4 mm mm 3 3
mm3 3 mm 3 mm mm3 4 4
mm mm mm mm mm mm mm mm
Z
V
U
Y
BOTTOM CHORD L3-L5 Section element
Rotation angle
Mirror
Sheet 16 x 750 Sheet 16 x 750 Sheet 150 x 16 Sheet 150 x 16 Sheet 150 x 16 Sheet 150 x 16 Sheet 10 x 650 Sheet 10 x 650
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 750.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 46600.0 -90.0 2875927533.333 4157421933.333 3100614.214 248.425 298.689 12792067.487 12792067.487 7669140.089 7669140.089 13807008.0 10135825.8 4157421933.333 2875927533.333 298.689 248.425 164.574 164.574 274.508 274.508 325.0 -375.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L3-L5.sec
mm2 deg 04 04 4 mm mm mm 3 3 3
mm mm3 mm3 3 mm 4 0 04 mm mm mm mm mm mm mm mm
Z
V
U
Y
BOTTOM CHORD L5-L7 Section element
Rotation angle
Mirror
Sheet 16 x 750 Sheet 16 x 750 Sheet 150 x 16 Sheet 150 x 16 Sheet 150 x 16 Sheet 150 x 16 Sheet 16 x 650 Sheet 16 x 650
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 750.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 54400.0 -90.0 3150552533.333 4840850133.333 4362226.554 240.654 298.306 14894923.487 14894923.487 8401473.422 8401473.422 16116163.2 11404105.92 4840850133.333 3150552533.333 298.306 240.654 154.439 154.439 273.804 273.804 325.0 -375.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L5-L7.sec
mm2 deg 04 04 4 mm mm mm 3 3 3
mm mm3 mm3 3 mm 4 0 04 mm mm mm mm mm mm mm mm
Z
V
U
Y
BOTTOM CHORD L7-L9 Section element
Rotation angle
Mirror
Sheet 16 x 750 Sheet 16 x 750 Sheet 150 x 20 Sheet 150 x 20 Sheet 150 x 20 Sheet 150 x 20 Sheet 16 x 650 Sheet 16 x 650
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 750.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 56800.0 -90.0 3456433333.333 4976764533.333 5061605.754 246.683 296.005 15313121.641 15313121.641 9217155.556 9217155.556 16677763.2 12260620.32 4976764533.333 3456433333.333 296.005 246.683 162.274 162.274 269.597 269.597 325.0 -375.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L7-L9.sec
mm2 deg 04 04 4 mm mm mm 3 3 3
mm mm3 mm3 3 mm 4 0 04 mm mm mm mm mm mm mm mm
Z
V
U
Y
UPPER CHORD U1-U3 Section element
Rotation angle
Mirror
Sheet 650 x 20 Sheet 16 x 680 Sheet 16 x 680 Sheet 150 x 16 Sheet 150 x 16
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 39560.0 -90.0 2739658426.424 2916641986.667 3759516.755 263.16 271.527 8974283.036 8974283.036 6605851.68 9603807.407 10133620.0 9407411.743 2916641986.667 2739658426.424 271.527 263.16 166.983 242.766 226.852 226.852 325.0 -414.732
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\U1-U3.sec
2
mm deg 4 0 04 mm4 mm mm mm3 mm3 3 mm 3 mm mm3 mm3 4 0 4 0 mm mm mm mm mm mm mm mm
Z
V
U
Y
UPPER CHORD U3-U5 Section element
Rotation angle
Mirror
Sheet 650 x 16 Sheet 12 x 684 Sheet 12 x 684 Sheet 150 x 12 Sheet 150 x 12
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 30416.0 -90.0 2126515801.968 2247540634.667 1739410.241 264.413 271.833 6915509.645 6915509.645 5040267.891 7646732.934 7783504.0 7265618.315 2247540634.667 2126515801.968 271.833 264.413 165.711 251.405 227.364 227.364 325.0 -421.905
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\U3-U5.sec
2
mm deg 4 0 04 mm4 mm mm mm3 mm3 3 mm 3 mm mm3 mm3 4 0 4 0 mm mm mm mm mm mm mm mm
Z
V
U
Y
UPPER CHORD U5-U7 Section element
Rotation angle
Mirror
Sheet 650 x 16 Sheet 16 x 684 Sheet 16 x 684 Sheet 150 x 16 Sheet 150 x 16
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 37088.0 -90.0 2551305361.486 2837965642.667 2974837.708 262.28 276.622 8732201.977 8732201.977 6427788.991 8417872.515 9751696.0 8773774.159 2837965642.667 2551305361.486 276.622 262.28 173.312 226.97 235.445 235.445 325.0 -396.918
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\U5-U7.sec
2
mm deg 4 0 4 0 mm4 mm mm 3 mm mm3 mm3 3 mm 3 mm mm3 04 4 0 mm mm mm mm mm mm mm mm
Z
V
U
Y
UPPER CHORD U7-U9 Section element
Rotation angle
Mirror
Sheet 650 x 20 Sheet 16 x 680 Sheet 16 x 680 Sheet 150 x 16 Sheet 150 x 16
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 39560.0 -90.0 2739658426.424 2916641986.667 3759516.755 263.16 271.527 8974283.036 8974283.036 6605851.68 9603807.407 10133620.0 9407411.743 2916641986.667 2739658426.424 271.527 263.16 166.983 242.766 226.852 226.852 325.0 -414.732
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\U7-U9.sec
2
mm deg 4 0 4 0 mm4 mm mm 3 mm mm3 mm3 3 mm 3 mm mm3 04 4 0 mm mm mm mm mm mm mm mm
Z
V
U
Y
DIAGONAL BEAM L0-L3 Section element
Rotation angle
Mirror
Sheet 16 x 400 Sheet 16 x 400 Sheet 150 x 16 Sheet 150 x 16 Sheet 150 x 16 Sheet 150 x 16
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 400.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 22400.0 -90.0 524765866.667 1830189866.667 1791252.17 153.059 285.841 5631353.436 5631353.436 2623829.333 2623829.333 6304000.0 3122585.6 1830189866.667 524765866.667 285.841 153.059 117.135 117.135 251.4 251.4 325.0 -200.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\DiL0-L3.sec
2
mm deg 4
4
0 mm4 mm mm mm3 mm3 mm3 3 mm mm3 mm3 04 4
mm mm mm mm mm mm mm mm
Z
V
U
Y
DIAGONAL L3-L5 Section element
Rotation angle
Mirror
Sheet 12 x 400 Sheet 12 x 400 Sheet 150 x 12 Sheet 150 x 12 Sheet 150 x 12 Sheet 150 x 12
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 400.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 16800.0 -90.0 399065600.0 1398357600.0 757913.6 154.123 288.506 4302638.769 4302638.769 1995328.0 1995328.0 4776000.0 2356334.4 1398357600.0 399065600.0 288.506 154.123 118.77 118.77 256.109 256.109 325.0 -200.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\DiL3-L5.sec
2
mm deg 4 mm 4
mm4 mm mm 3 mm mm3 mm3 3 mm 3 mm mm3 4
mm mm mm mm mm mm mm mm mm
4
Z
V
U
Y
DIAGONAL BEAM L5-L8 Section element
Rotation angle
Mirror
Sheet 10 x 400 Sheet 10 x 400 Sheet 150 x 10 Sheet 150 x 10 Sheet 150 x 10 Sheet 150 x 10
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 400.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 14000.0 -90.0 334866666.667 1176116666.667 438745.455 154.658 289.842 3618820.513 3618820.513 1674333.333 1674333.333 4000000.0 1969610.0 1176116666.667 334866666.667 289.842 154.658 119.595 119.595 258.487 258.487 325.0 -200.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\DiL5-L8.sec
2
mm deg 4
4
0 mm4 mm mm 3 mm mm3 mm3 3 mm 3 mm mm3 04 4
mm mm mm mm mm mm mm mm
Z
V
Y
U
VERTICAL BEAM Section element
Rotation angle
Mirror
Sheet 10 x 250 Sheet 10 x 250 Sheet 630 x 10
Material
E (kg/mm^2)
Steel Steel Steel
20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 250.0 mm Basic geometry of the section Parameter Value 11300.0 A Sectional area -90.0 Angle of principal inertia axes α Iy Inertia moment about centroidal Y1-axis parallel 26094166.667 with Y-axis Iz Inertia moment about centroidal Z1-axis parallel 720414166.667 with Z-axis 354516.061 It Torsional moment of inertia (St. Venant) 48.054 iy Radius of inertia about Y1-axis 252.494 iz Radius of inertia about Z1-axis 2216658.974 W u+ Maximum resisting moment about U-axis 2216658.974 W u- Minimum resisting moment about U-axis 208753.333 W v+ Maximum resisting moment about V-axis 208753.333 Wv- Minimum resisting moment about V-axis 2592250.0 W pl,u Plastic resisting moment about U-axis 328250.0 W pl,v Plastic resisting moment about V-axis 720414166.667 Iu Maximum inertia moment 26094166.667 Iv Minimum inertia moment 252.494 iu Maximum radius of inertia 48.054 iv Minimum radius of inertia au+ Middle point along positive direction of Y(U)-axis 18.474 auMiddle point along negative direction of Y(U)-axis18.474 av+ Middle point along positive direction of Z(V)-axis 196.165 avMiddle point along negative direction of Z(V)-axis196.165 yM Coordinate of the center of gravity along Y-axis 325.0 zM Coordinate of the center of gravity along Z-axis -125.0
mm2 deg 4
4
mm4 mm mm mm3 mm3 3 mm 3 mm mm3 mm3 4
4
mm mm mm mm mm mm mm mm
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\vert.sec
Z
V
U
Y
END RAKER M0-L0 Section element
Rotation angle
Mirror
Sheet 20 x 680 Sheet 650 x 20 Sheet 150 x 20 Sheet 150 x 20 Sheet 20 x 600 Sheet 20 x 600 Sheet 20 x 680
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 70200.0 -90.0 3904559943.02 5575585000.0 8781357.576 235.84 281.823 17155646.154 17155646.154 10274387.435 12202836.257 19140500.0 14575120.628 5575585000.0 3904559943.02 281.823 235.84 146.359 173.83 244.382 244.382 325.0 -380.028
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\M0-L0.sec
mm2 deg 4
4
mm mm mm
4
3 3 3 3
mm 3 4 4
mm mm mm mm mm mm mm mm
3
Z
V
U
Y
END RAKER M0-U1 Section element
Rotation angle
Mirror
Sheet 12 x 688 Sheet 12 x 688 Sheet 650 x 12 Sheet 150 x 12 Sheet 150 x 12
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 27912.0 -90.0 1936201066.786 2165769176.0 1261351.68 263.378 278.555 6663905.157 6663905.157 4862221.705 6415791.989 7391627.88 6628764.883 2165769176.0 1936201066.786 278.555 263.378 174.198 229.858 238.747 238.747 325.0 -398.213
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\M0-U1.sec
2
mm deg 4 0 4
mm4 mm mm mm3 mm3 3 mm 3 mm mm3 mm3 4
4
0 mm mm mm mm mm mm mm mm
Z
V
U
Y
LINK MEMBER Section element
Rotation angle
Mirror
Sheet 20 x 680 Sheet 20 x 680 Sheet 20 x 680 Sheet 20 x 680 Sheet 16 x 680 Sheet 16 x 680
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 680.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Value 76160.0 Sectional area -90.0 Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis2934698666.667 Inertia moment about centroidal Z1-axis parallel with Z-axis 6737900586.667 8568673.021 Torsional moment of inertia (St. Venant) 196.299 Radius of inertia about Y1-axis 297.44 Radius of inertia about Z1-axis 20732001.805 Maximum resisting moment about U-axis 20732001.805 Minimum resisting moment about U-axis 8631466.667 Maximum resisting moment about V-axis 8631466.667 Minimum resisting moment about V-axis 22619520.0 Plastic resisting moment about U-axis 12947198.88 Plastic resisting moment about V-axis 6737900586.667 Maximum inertia moment 2934698666.667 Minimum inertia moment 297.44 Maximum radius of inertia 196.299 Minimum radius of inertia 113.333 Middle point along positive direction of Y(U)-axis 113.333 Middle point along negative direction of Y(U)-axis 272.216 Middle point along positive direction of Z(V)-axis 272.216 Middle point along negative direction of Z(V)-axis 325.0 Coordinate of the center of gravity along Y-axis -340.0 Coordinate of the center of gravity along Z-axis
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\link.sec
2
mm deg 4 0 04 mm4 mm mm 3 3 3
mm 3 mm mm3 mm3 4 0 4 0 mm mm mm mm mm mm mm mm
EAST COAST RAILWAY
PROJ ECT PROJ ECT PROJ ECT PROJ ECT
RAIL VIKAS NIGAM LIMITED PMC : 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
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
Tension allowed = 630x2130x1.25 = 1677 t > 1256 t ok
EXTENSION PIECE ACROSS PIN HOLE Net area req’ :
= . 475 cm2 Try 2 additional plate 660x12 and 660x10 with each gusset with 250φ pin Gross area of main section Add. PL 2x66x(1.2+1) Deduction for holes 2x25x7.8 8x7.8x2.15
= 761.6 cm2 = 290.4 cm2 = 1052.0 cm2 =-390.00 cm2 =-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
LINK ACROSS PIN HOLE
Gross area of main section Add. PL 2x66x(1.2+1) Deduction for holes 2x25x7.8 8x7.8x2.35
= 761.6 cm2 = 290.4 cm2 = 1052.0 cm2 =-390.00 cm2 =-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
LINK PIN Material : carbon steel class 4 to IS-1875 or equivalent
LINK ARRANGEMENT (IN PLAN) e=
+ 4 = 90 mm
w1 = (½ x 1256) / 9.4
=66.81 t/cm
w2 = (½ x 1256) / 7.8
= 80.51 t/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)/( π x 253/32) = 3287 kg/cm2 < 2990 (table 1 ) x 1.25 (ok)
Shear stress on pin = 1256000/(2 x π/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 cm2 Bearing Stress on H.T.S Steel plate = 1256000/(2x195) = 3220 kg/cm2 < 2600 (table 1) x 1.25=3250 kg/cm2
BUFFER SLAB Material : Grade 58HTC to I.S 961 or equivalent with γst = 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/cm MA = (11.92 x 17.52) / 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/cm2 ∴t=
=
.
= 10.22 cm, Provide t= 100 mm
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
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
B.M
= 7.0 x
.
= 8631 cm3
+ 0.7 x
.
=11.38 + 3.7 = 15.08 tm Bending Stress = (15.08 x 105) / 8631 = 175 kg/cm2 < (2250 kg/cm2 (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
= 91.28 cm2
Area
= 2 x 45.64
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
LINK SHORTENING As per computer output , enclosed. Deflection at free end of cantilever span = 106.71 cm Shortening of link to neutralize this deflection = δ * h/L
where,
δ = 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
Saturday, February 02, 2008, 10:29 AM 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. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. 30. 31. 32. 33. 34. 35. 36. 37. 38. 39. 40. 41.
STAAD SPACE DXF IMPORT OF ACAD-89 SPAN.DXF START JOB INFORMATION JOB NAME CANTILEVER ERECTION SPAN 92M JOB CLIENT RVNL JOB NO AA JOB PART 0 JOB REF 0 ENGINEER NAME ADHI T ENGINEER DATE 31-JAN-08 END JOB INFORMATION INPUT WIDTH 79 OUTPUT WIDTH 118 OUTPUT WIDTH 72 UNIT METER KG JOINT COORDINATES 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 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 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 20 103.5 0 0; 21 109.25 0 0; 22 115 0 0; 23 120.75 0 0; 24 126.5 0 0 25 132.25 0 0; 26 138 0 0; 27 143.75 0 0; 28 149.5 0 0; 29 155.25 0 0 30 161 0 0; 31 166.75 0 0; 32 172.5 0 0; 33 178.25 0 0; 34 184 0 0 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 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 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 50 138 6.25 0; 51 149.5 6.25 0; 52 161 6.25 0; 53 172.5 6.25 0 54 178.25 6.25 0; 55 184 6.25 0; 56 5.75 12.5 0; 57 11.5 12.5 0 58 17.25 12.5 0; 59 23 12.5 0; 60 28.75 12.5 0; 61 34.5 12.5 0 62 40.25 12.5 0; 63 46 12.5 0; 64 51.75 12.5 0; 65 57.5 12.5 0 66 63.25 12.5 0; 67 69 12.5 0; 68 74.75 12.5 0; 69 80.5 12.5 0 70 86.25 12.5 0; 71 92 12.5 0; 72 97.75 12.5 0; 73 103.5 12.5 0 74 109.25 12.5 0; 75 115 12.5 0; 76 120.75 12.5 0; 77 126.5 12.5 0 78 132.25 12.5 0; 79 138 12.5 0; 80 143.75 12.5 0; 81 149.5 12.5 0 82 155.25 12.5 0; 83 161 12.5 0; 84 166.75 12.5 0; 85 172.5 12.5 0 86 178.25 12.5 0 MEMBER INCIDENCES 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 12 13 14; 13 14 15; 14 15 16; 15 16 17; 16 17 18; 17 18 19; 18 19 20; 19 20 21 20 21 22; 21 22 23; 22 23 24; 23 24 25; 24 25 26; 25 26 27; 26 27 28; 27 28 29 28 29 30; 29 30 31; 30 31 32; 31 32 33; 32 33 34; 33 1 35; 34 2 36; 35 3 37 36 6 38; 37 8 39; 38 10 40; 39 12 41; 40 14 42; 41 16 43; 42 17 44; 43 18 45 44 19 46; 45 20 47; 46 22 48; 47 24 49; 48 26 50; 49 28 51; 50 30 52; 51 32 53
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF 42. 43. 44. 45. 46. 47. 48. 49. 50. 51. 52. 53. 54. 55. 56. 57. 58. 59. 60. 61. 62. 63. 64. 65. 66. 67. 68. 69. 70. 71. 72. 73. 74. 75. 76. 77. 78. 79. 80. 81. 82. 83. 84. 85. 86. 87. 88. 89. 90. 91. 92. 93. 94. 95. 96. 97.
-- PAGE NO.
2
52 33 54; 53 34 55; 54 36 56; 55 35 56; 56 56 57; 57 57 58; 58 58 59; 59 59 60 60 61; 61 61 62; 62 62 63; 63 63 64; 64 64 65; 65 65 66; 66 66 67; 67 67 68 68 69; 69 69 70; 70 70 71; 71 71 72; 72 72 73; 73 73 74; 74 74 75; 75 75 76 76 77; 77 77 78; 78 78 79; 79 79 80; 80 80 81; 81 81 82; 82 82 83; 83 83 84 84 85; 85 85 86; 86 86 55; 87 35 2; 88 2 37; 89 37 4; 90 4 38; 91 38 7 92 7 39; 93 39 9; 94 9 40; 95 40 11; 96 11 41; 97 41 13; 98 13 42; 99 42 15 100 15 43; 101 43 17; 102 17 45; 103 45 19; 104 19 47; 105 47 21; 106 21 48 107 48 23; 108 23 49; 109 49 25; 110 25 50; 111 50 27; 112 27 51; 113 51 29 114 29 52; 115 52 31; 116 31 53; 117 53 33; 118 33 55; 119 37 57; 120 38 59 121 39 61; 122 40 63; 123 41 65; 124 42 67; 125 43 69; 126 44 70; 127 45 71 128 46 72; 129 47 73; 130 48 75; 131 49 77; 132 50 79; 133 51 81; 134 52 83 135 53 85; 136 54 86; 137 35 36; 138 56 37; 139 37 58; 140 58 38; 141 38 60 142 60 39; 143 39 62; 144 62 40; 145 40 64; 146 64 41; 147 41 66; 148 66 42 149 42 68; 150 68 43; 151 43 70; 152 70 45; 153 45 72; 154 72 47; 155 47 74 156 74 48; 157 48 76; 158 76 49; 159 49 78; 160 78 50; 161 50 80; 162 80 51 163 51 82; 164 82 52; 165 52 84; 166 84 53; 167 53 86; 168 4 6; 169 55 54 170 44 45; 171 45 46 UNIT MMS KG DEFINE MATERIAL START ISOTROPIC STEEL E 20904.2 POISSON 0.3 DENSITY 7.83341E-006 ALPHA 6.5E-006 DAMP 0.03 END DEFINE MATERIAL CONSTANTS MATERIAL STEEL MEMB 1 TO 3 5 TO 171 START USER TABLE TABLE 1 UNIT METER KG PRISMATIC L0-L1 0.042 0.00300535 0.003635 5.227E-006 0 0 0.75 0.65 L3-L5 0.0466 0.002876 0.004157 3.101E-006 0 0 0.75 0.65 L5-L7 0.0544 0.00315055 0.00484085 4.362E-006 0 0 0.75 0.65 L7-L9 0.0568 0.003456 0.004977 5.06161E-006 0 0 0.75 0.65 U1-U3 0.03956 0.00273966 0.00291664 3.75952E-006 0 0 0.7 0.65 U3-U5 0.030416 0.00212652 0.00224754 1.73941E-006 0 0 0.7 0.65 U5-U7 0.037088 0.00255131 0.00283797 2.97484E-006 0 0 0.7 0.65 U7-U9 0.03956 0.00273966 0.00291664 3.75952E-006 0 0 0.7 0.65 M0-L0 0.0702 0.00390456 0.00557558 8.78136E-006 0 0 0.7 0.65 M0-U1 0.027912 0.0019362 0.00216577 1.26135E-006 0 0 0.7 0.65 VERT 0.0113 2.60942E-005 0.000720414 3.54516E-007 0 0 0.25 0.65 DIL0-L3 0.0224 0.000524766 0.00183019 1.79125E-006 0 0 0.4 0.65
60 68 76 84
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF 98. 99. 100. 101. 102. 103. 104. 105. 106. 107. 108. 109. 110. 111. 112. 113. 114. 115. 116. 117. 118. 119. 120. 121. 122. 123. 124. 125. 126. 127. 128. 129. 130. 131. 132. 133. 134. 135. 136. 137. 138. 139. 140. 141. 142. 143. 144. 145. 146. 147. 148.
-- PAGE NO.
3
DIL3-L5 0.0168 0.000399066 0.00139836 7.57914E-007 0 0 0.4 0.65 DIL5-L8 0.014 0.000334867 0.00117612 4.38745E-007 0 0 0.4 0.65 LINK 0.07616 0.0029347 0.0067379 8.56867E-006 0 0 0.68 0.65 END UNIT MMS KG MEMBER PROPERTY AMERICAN 1 TO 3 14 TO 19 30 TO 32 UPTABLE 1 L0-L1 5 12 13 20 21 28 29 168 UPTABLE 1 L3-L5 MEMBER PROPERTY AMERICAN 6 7 10 11 22 23 26 27 UPTABLE 1 L5-L7 8 9 24 25 UPTABLE 1 L7-L9 56 57 68 69 72 73 84 85 UPTABLE 1 U1-U3 58 59 66 67 74 75 82 83 UPTABLE 1 U3-U5 60 61 64 65 76 77 80 81 UPTABLE 1 U5-U7 62 63 78 79 UPTABLE 1 U7-U9 33 43 53 UPTABLE 1 M0-L0 55 86 152 153 UPTABLE 1 M0-U1 34 TO 42 44 TO 52 54 119 TO 126 128 TO 137 169 TO 171 UPTABLE 1 VERT 87 TO 89 100 TO 105 116 TO 118 138 139 150 151 154 155 166 167 UPTABLE 1 DIL0-L3 90 91 98 99 106 107 114 115 140 141 148 149 156 157 164 165 UPTABLE 1 DIL3-L5 92 TO 97 108 TO 113 142 TO 147 158 TO 163 UPTABLE 1 DIL5-L8 70 71 127 UPTABLE 1 LINK SUPPORTS 1 PINNED 18 FIXED BUT FX MX MY MZ UNIT METER KG MEMBER TRUSS 1 TO 3 5 TO 171 UNIT MMS KG LOAD 1 LOAD 1 DEAD LOAD SELFWEIGHT Y -1 LOAD 2 LOAD 2 ERECTION JOINT LOAD 1 18 FY -6320 2 TO 4 6 TO 17 FY -12640 19 TO 28 FY -12340 29 FY -14570 30 FY -21800 31 FY -21110 32 FY -11120 33 FY -9620 34 FY -4410 UNIT METER KG LOAD COMB 3 LOAD COMBINATION 1 1.0 2 1.0 UNIT MMS KG PERFORM ANALYSIS
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 3 of 36
Saturday, February 02, 2008, 10:29 AM 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
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 4 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
JOINT DISPLACEMENT (CM -----------------JOINT
1
2
3
4
6
7
8
9
10
11
12
13
14
15
16
17
LOAD
1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3
X-TRANS
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 -0.0060 -0.0142 -0.0202 -0.0120 -0.0284 -0.0403 -0.0308 -0.0663 -0.0971 -0.0496 -0.1043 -0.1539 -0.0831 -0.1697 -0.2528 -0.1165 -0.2351 -0.3516 -0.1710 -0.3409 -0.5119 -0.2255 -0.4468 -0.6723 -0.3120 -0.6137 -0.9257 -0.3985 -0.7806 -1.1791 -0.5413 -1.0555 -1.5968 -0.6840 -1.3305 -2.0145 -0.8962 -1.7391 -2.6353 -1.1085 -2.1476 -3.2561
-- PAGE NO.
RADIANS)
Y-TRANS
0.0000 0.0000 0.0000 0.2373 0.4570 0.6944 0.4833 0.9161 1.3994 0.7428 1.4176 2.1604 1.0129 1.9287 2.9416 1.2741 2.4347 3.7088 1.5422 2.9445 4.4867 1.7806 3.4034 5.1840 2.0061 3.8351 5.8412 2.1635 4.1363 6.2998 2.2988 4.3949 6.6936 2.3067 4.4158 6.7225 2.2341 4.2713 6.5055 1.9247 3.6857 5.6104 1.4772 2.8276 4.3049 0.6638 1.2863 1.9502
5
STRUCTURE TYPE = SPACE
Z-TRANS
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
X-ROTAN
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C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
JOINT DISPLACEMENT (CM -----------------JOINT
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
LOAD
1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3
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-- PAGE NO.
RADIANS)
Y-TRANS
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C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
JOINT DISPLACEMENT (CM -----------------JOINT
34
35
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37
38
39
40
41
42
43
44
45
46
47
48
49
LOAD
1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3
X-TRANS
-- PAGE NO.
RADIANS)
Y-TRANS
-2.7529 -36.8192 -5.2438 -69.8954 -7.9967 -106.7146 -0.2452 0.0011 -0.4641 0.0061 -0.7094 0.0072 -0.2452 0.2374 -0.4641 0.4660 -0.7094 0.7034 -0.2489 0.4890 -0.4757 0.9495 -0.7245 1.4386 -0.2444 1.0192 -0.4771 1.9622 -0.7215 2.9813 -0.2309 1.5494 -0.4521 2.9779 -0.6830 4.5274 -0.2130 2.0136 -0.4216 3.8686 -0.6345 5.8822 -0.1850 2.3060 -0.3743 4.4283 -0.5592 6.7343 -0.1319 2.2404 -0.2713 4.3048 -0.4032 6.5452 -0.0351 1.4830 -0.0985 2.8611 -0.1336 4.3441 -0.1258 0.6946 -0.2681 1.3531 -0.3939 2.0478 -0.1258 -0.0987 -0.2681 -0.1746 -0.3939 -0.2733 -0.1258 -1.6066 -0.2681 -3.0516 -0.3939 -4.6582 -0.2165 -3.1194 -0.4399 -5.9493 -0.6564 -9.0687 -0.1197 -6.9644 -0.2599 -13.3149 -0.3796 -20.2792 -0.0666 -11.5012 -0.1733 -21.9932 -0.2400 -33.4944
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C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
JOINT DISPLACEMENT (CM -----------------JOINT
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
LOAD
1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3
X-TRANS
-- PAGE NO.
RADIANS)
Y-TRANS
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C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
JOINT DISPLACEMENT (CM -----------------JOINT
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
LOAD
1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3 1 2 3
X-TRANS
0.0814 0.1355 0.2169 0.2997 0.5510 0.8508 0.5181 0.9666 1.4847 0.7434 1.3967 2.1401 0.9688 1.8267 2.7955 1.1248 2.1240 3.2488 1.2809 2.4212 3.7021 1.5063 2.8500 4.3563 1.7316 3.2789 5.0105 1.9499 3.6900 5.6399 2.1683 4.1010 6.2693 2.2950 4.3362 6.6312 2.4216 4.5714 6.9931 2.4996 4.7107 7.2103 2.5775 4.8500 7.4276 2.6264 4.9304 7.5567
-- PAGE NO.
RADIANS)
Y-TRANS
2.2597 4.3519 6.6116 2.2361 4.3048 6.5409 1.8366 3.5517 5.3883 1.4775 2.8611 4.3386 0.7276 1.4199 2.1475 -0.1008 -0.1746 -0.2754 -1.5736 -2.9843 -4.5579 -3.1249 -5.9493 -9.0742 -5.0670 -9.6657 -14.7326 -6.9687 -13.3149 -20.2836 -9.2463 -17.6605 -26.9068 -11.5064 -21.9932 -33.4996 -13.9686 -26.6984 -40.6670 -16.4014 -31.3415 -47.7429 -18.9447 -36.1689 -55.1136 -21.4677 -40.9982 -62.4660
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Z-TRANS
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C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
JOINT DISPLACEMENT (CM -----------------JOINT
82
83
84
85
86
LOAD
1 2 3 1 2 3 1 2 3 1 2 3 1 2 3
X-TRANS
2.6752 5.0107 7.6859 2.7036 5.0441 7.7478 2.7321 5.0776 7.8097 2.7385 5.0797 7.8182 2.7449 5.0819 7.8268
-- PAGE NO.
RADIANS)
Y-TRANS
-24.0497 -45.9151 -69.9648 -26.5996 -50.7394 -77.3390 -29.1759 -55.5342 -84.7101 -31.7332 -60.3637 -92.0969 -34.2784 -65.1397 -99.4181
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C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
SUPPORT REACTIONS -UNIT KG ----------------JOINT
1
18
LOAD
1 2 3 1 2 3
FORCE-X
-- PAGE NO.
MMS
11
STRUCTURE TYPE = SPACE
FORCE-Y
FORCE-Z
MOM-X
MOM-Y
MOM Z
0.00 0.00 0.00 -7976.24 0.00 -7976.23 0.00 235354.48 0.00 416246.25 0.00 651600.75
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C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
1
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
1
1 2 1 2 1 2
0.00 0.00 0.00 0.00 0.00 0.00
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7
1 2 3
8
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2
5
STRUCTURE TYPE = SPACE
JT
3
3
12
LOAD
2
2
-- PAGE NO.
1
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 12 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
9
1 2 3
10
1 2 3
11
1 2 3
12
1 2 3
13
1 2 3
14
1 2 3
15
1
JT
-- PAGE NO.
13
STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
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0.00 0.00 0.00 0.00 0.00 0.00
12 171099.38 13-171099.38 12 330092.19 13-330092.19 12 501191.56 13-501191.56
1225.15 1225.15 0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
13 241829.72 14-241829.72 13 465798.56 14-465798.56 13 707628.25 14-707628.25
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
14 241829.72 15-241829.72 14 465798.56 15-465798.56 14 707628.25 15-707628.25
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
15 324072.97 16-324072.97 15 623859.62 16-623859.62 15 947932.56 16-947932.56
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
16 324072.97 17-324072.97
945.89 945.89
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
16 623859.62 17-623859.62 16 947932.56 17-947932.56
0.00 0.00 945.89 945.89
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
17 409191.94 18-409191.94 17 782857.31 18-782857.31 171192049.12 18**********
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
18 409191.94 19-409191.94 18 782857.31 19-782857.31 181192049.12 19**********
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
19 324073.00 20-324073.00 19 621417.44 20-621417.44 19 945490.50 20-945490.50
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
20 324073.00 21-324073.00 20 621417.44 21-621417.44 20 945490.50 21-945490.50
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
21 241829.77 22-241829.77 21 461247.75 22-461247.75 21 703077.50 22-703077.50
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
22 241829.77 23-241829.77 22 461247.75 23-461247.75 22 703077.50 23-703077.50
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
23 171099.41 24-171099.41
1225.15 1225.15
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 14 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
23 321791.84 24-321791.84 23 492891.25 24-492891.25
0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
24 171099.41 25-171099.41 24 321791.84 25-321791.84 24 492891.25 25-492891.25
1225.15 1225.15 0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
25 112523.41 26-112523.41 25 207033.36 26-207033.36 25 319556.78 26-319556.78
1279.20 1279.20 0.00 0.00 1279.20 1279.20
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
26 112523.41 27-112523.41 26 207033.36 27-207033.36 26 319556.78 27-319556.78
1279.20 1279.20 0.00 0.00 1279.20 1279.20
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
27 66126.55 28 -66126.55 27 112988.66 28-112988.66 27 179115.22 28-179115.22
1225.15 1225.15 0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
28 66126.55 29 -66126.55 28 112988.66 29-112988.66 28 179115.22 29-179115.22
1225.15 1225.15 0.00 0.00 1225.15 1225.15
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
29 31884.05 30 -31884.05 29 45692.97 30 -45692.97 29 77577.02 30 -77577.02
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
30 31884.05 31 -31884.05
1049.48 1049.48
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 15 of 36
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LOAD
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STRUCTURE TYPE = SPACE MMS AXIAL
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SHEAR-Z
TORSION
MOM-Y
MOM-Z
30 45692.97 31 -45692.97 30 77577.02 31 -77577.02
0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
31 9154.41 32 -9154.41 31 13831.06 32 -13831.06 31 22985.47 32 -22985.47
945.89 945.89 0.00 0.00 945.89 945.89
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
32 9154.41 33 -9154.41 32 13831.06 33 -13831.06 32 22985.47 33 -22985.47
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
33 34 33 34 33 34
0.00 0.00 0.00 0.00 0.00 0.00
945.88 945.88 0.00 0.00 945.88 945.88
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
1 -945.88 35 4382.79 1 -14296.24 35 14296.24 1 -15242.12 35 18679.03
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
2 36 2 36 2 36
257.67 295.56 -3405.34 3405.34 -3147.67 3700.91
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
3 -1891.77 37 2445.00 3 -12640.00 37 12640.00 3 -14531.77 37 15085.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
6 38
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
-2098.96 2652.20
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 16 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
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STRUCTURE TYPE = SPACE MMS AXIAL
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SHEAR-Z
TORSION
MOM-Y
MOM-Z
6 -12640.00 38 12640.00 6 -14738.96 38 15292.20
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
8 -2450.29 39 3003.53 8 -12640.00 39 12640.00 8 -15090.29 39 15643.52
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
10 -2558.39 40 3111.63 10 -12640.00 40 12640.00 10 -15198.39 40 15751.63
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
12 -2450.29 41 3003.53 12 -12640.00 41 12640.00 12 -15090.29 41 15643.52
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
14 -2098.96 42 2652.20 14 -12640.00 42 12640.00 14 -14738.96 42 15292.20
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
16 -1891.77 43 2445.00 16 -12640.00 43 12640.00 16 -14531.77 43 15085.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
17 -11372.23 44 11925.46 17 -25243.48 44 25243.48 17 -36615.71 44 37168.94
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
18 233462.70 45-230025.80
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
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Page 17 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
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LOAD
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STRUCTURE TYPE = SPACE MMS AXIAL
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SHEAR-Z
TORSION
MOM-Y
MOM-Z
18 409926.25 45-409926.25 18 643388.94 45-639952.06
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
19 -11372.23 46 11925.46 19 -25464.38 46 25464.38 19 -36836.61 46 37389.84
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
20 -1891.77 47 2445.00 20 -12340.00 47 12340.00 20 -14231.77 47 14785.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
22 -2098.96 48 2652.20 22 -12340.00 48 12340.00 22 -14438.96 48 14992.20
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
24 -2450.29 49 3003.53 24 -12340.00 49 12340.00 24 -14790.29 49 15343.53
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
26 -2558.39 50 3111.63 26 -12340.00 50 12340.00 26 -14898.39 50 15451.63
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
28 -2450.29 51 3003.53 28 -12340.00 51 12340.00 28 -14790.29 51 15343.53
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
30 52
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
-2098.96 2652.20
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Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
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LOAD
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53
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SHEAR-Z
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MOM-Y
MOM-Z
30 -21800.00 52 21800.00 30 -23898.96 52 24452.20
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
32 -1891.77 53 2445.00 32 -11120.00 53 11120.00 32 -13011.77 53 13565.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
33 54 33 54 33 54
257.67 295.56 1003.76 -1003.76 1261.43 -708.20
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
34 55 34 55 34 55
-945.88 4382.79 -4410.00 4410.00 -5355.88 8792.79
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
36 56 36 56 36 56
-550.05 1103.29 -3405.34 3405.34 -3955.40 4508.63
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
35 -3604.37 56 4970.91 35 -9713.03 56 9713.03 35 -13317.40 56 14683.94
628.61 628.61 0.00 0.00 628.61 628.61
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
56 -9180.29 57 9180.29 56 -16285.45 57 16285.45 56 -25465.74 57 25465.74
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
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57 58
890.93 890.93
0.00 0.00
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0.00 0.00
-9180.29 9180.29
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LOAD
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1 2 3
60
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61
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SHEAR-Z
TORSION
MOM-Y
MOM-Z
57 -16285.45 58 16285.45 57 -25465.74 58 25465.74
0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
58 -31472.27 59 31472.27 58 -58058.57 59 58058.57 58 -89530.83 59 89530.83
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
59 -31472.27 60 31472.27 59 -58058.57 60 58058.57 59 -89530.83 60 89530.83
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
60 -65844.26 61 65844.26 60-123992.12 61 123992.12 60-189836.39 61 189836.39
835.26 835.26 0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
61 -65844.26 62 65844.26 61-123992.12 62 123992.12 61-189836.39 62 189836.39
835.26 835.26 0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
62-112089.74 63 112089.74 62-212280.45 63 212280.45 62-324370.22 63 324370.22
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
63-112089.74 64 112089.74 63-212280.45 64 212280.45 63-324370.22 64 324370.22
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
64-170817.12 65 170817.12
835.26 835.26
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 20 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
65
1 2 3
66
1 2 3
67
1 2 3
68
1 2 3
69
1 2 3
70
1 2 3
71
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
64-324729.22 65 324729.22 64-495546.34 65 495546.34
0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
65-170817.12 66 170817.12 65-324729.22 66 324729.22 65-495546.34 66 495546.34
835.26 835.26 0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
66-241417.95 67 241417.95 66-459532.72 67 459532.72 66-700950.69 67 700950.69
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
67-241417.95 68 241417.95 67-459532.72 68 459532.72 67-700950.69 68 700950.69
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
68-324098.84 69 324098.84 68-618496.69 69 618496.69 68-942595.50 69 942595.50
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
69-324098.84 70 324098.84 69-618496.69 70 618496.69 69-942595.50 70 942595.50
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
70-432168.94 71 432168.94 70-823039.44 71 823039.44 70********** 711255208.38
1715.20 1715.20 0.00 0.00 1715.20 1715.20
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
71-432168.94 72 432168.94
1715.20 1715.20
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 21 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
72
1 2 3
73
1 2 3
74
1 2 3
75
1 2 3
76
1 2 3
77
1 2 3
78
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
71-823039.44 72 823039.44 71********** 721255208.38
0.00 0.00 1715.20 1715.20
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
72-324098.88 73 324098.88 72-616736.94 73 616736.94 72-940835.88 73 940835.88
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
73-324098.88 74 324098.88 73-616736.94 74 616736.94 73-940835.88 74 940835.88
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
74-241418.02 75 241418.02 74-454575.44 75 454575.44 74-695993.44 75 695993.44
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
75-241418.02 76 241418.02 75-454575.44 76 454575.44 75-695993.44 76 695993.44
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
76-170817.14 77 170817.14 76-317111.34 77 317111.34 76-487928.53 77 487928.53
835.26 835.26 0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
77-170817.14 78 170817.14 77-317111.34 78 317111.34 77-487928.53 78 487928.53
835.26 835.26 0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
78-112089.77 79 112089.77
890.93 890.93
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 22 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
79
1 2 3
80
1 2 3
81
1 2 3
82
1 2 3
83
1 2 3
84
1 2 3
85
1
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-- PAGE NO.
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
78-200361.06 79 200361.06 78-312450.84 79 312450.84
0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
79-112089.77 80 112089.77 79-200361.06 80 200361.06 79-312450.84 80 312450.84
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
80 -65844.30 81 65844.30 80-108308.16 81 108308.16 80-174152.45 81 174152.45
835.26 835.26 0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
81 -65844.30 82 65844.30 81-108308.16 82 108308.16 81-174152.45 82 174152.45
835.26 835.26 0.00 0.00 835.26 835.26
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
82 -31472.29 83 31472.29 82 -36969.07 83 36969.07 82 -68441.36 83 68441.36
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
83 -31472.29 84 31472.29 83 -36969.07 84 36969.07 83 -68441.36 84 68441.36
685.00 685.00 0.00 0.00 685.00 685.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
84 -9180.29 85 9180.29 84 -3133.74 85 3133.74 84 -12314.03 85 12314.03
890.93 890.93 0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
85 86
890.93 890.93
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
-9180.29 9180.29
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 23 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
86
1 2 3
87
1 2 3
88
1 2 3
89
1 2 3
90
1 2 3
91
1 2 3
92
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-- PAGE NO.
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
85 -3133.74 86 3133.74 85 -12314.03 86 12314.03
0.00 0.00 890.93 890.93
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
86 55 86 55 86 55
-4970.91 3604.37 -2996.20 2996.20 -7967.12 6600.58
628.61 628.61 0.00 0.00 628.61 628.61
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
35 3739.30 2 -4835.98 35 9713.03 2 -9713.03 35 13452.33 2 -14549.01
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
2 -8684.92 37 9781.59 2 -22261.29 37 22261.29 2 -30946.21 37 32042.88
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
37 13995.70 4 -15092.38 37 22928.05 4 -22928.05 37 36923.75 4 -38020.42
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
4 -18615.92 38 19438.43 4 -40103.57 38 40103.57 4 -58719.50 38 59542.01
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
38 22635.05 7 -23457.56 38 39436.81 7 -39436.81 38 62071.86 7 -62894.38
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
7 -27186.53 39 27871.95
315.29 315.29
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 24 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
93
1 2 3
94
1 2 3
95
1 2 3
96
1 2 3
97
1 2 3
98
1 2 3
99
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
7 -56612.34 39 56612.34 7 -83798.87 39 84484.29
0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
39 31586.67 9 -32272.10 39 57279.09 9 -57279.09 39 88865.77 9 -89551.19
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
9 -36255.20 40 36940.62 9 -74454.63 40 74454.63 9-110709.83 40 111395.26
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
40 40580.86 11 -41266.29 40 73787.86 11 -73787.86 40 114368.72 11-115054.15
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
11 -45249.38 41 45934.81 11 -90963.38 41 90963.38 11-136212.77 41 136898.19
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
41 49649.53 13 -50334.96 41 91630.15 13 -91630.15 41 141279.69 13-141965.09
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
13 -54063.93 42 54886.43 13-108805.66 42 108805.66 13-162869.59 42 163692.09
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
42 58083.05 15 -58905.55
378.35 378.35
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 25 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
100
1 2 3
101
1 2 3
102
1 2 3
103
1 2 3
104
1 2 3
105
1 2 3
106
1
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-- PAGE NO.
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
42 108138.91 15-108138.91 42 166221.95 15-167044.45
0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
15 -62429.11 43 63525.78 15-125314.43 43 125314.43 15-187743.53 43 188840.22
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
43 67739.92 17 -68836.60 43 125981.26 17-125981.26 43 193721.19 17-194817.86
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
17 -56882.54 45 57979.21 17-108855.30 45 108855.30 17-165737.83 45 166834.52
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
45 -57979.21 19 56882.54 45-110305.00 19 110305.00 45-168284.22 19 167187.53
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
19 68836.57 47 -67739.89 19 128138.71 47-128138.71 19 196975.28 47-195878.59
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
47 -63525.79 21 62429.11 47-126667.79 21 126667.79 47-190193.58 21 189096.91
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
21 58905.56 48 -58083.05
378.35 378.35
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 26 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
107
1 2 3
108
1 2 3
109
1 2 3
110
1 2 3
111
1 2 3
112
1 2 3
113
1
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-- PAGE NO.
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
21 109899.91 48-109899.91 21 168805.47 48-167982.97
0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
48 -54886.44 23 54063.93 48-111370.84 23 111370.84 48-166257.28 23 165434.77
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
23 50334.96 49 -49649.54 23 94602.95 49 -94602.95 23 144937.91 49-144252.50
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
49 -45934.81 25 45249.39 49 -93132.03 25 93132.03 49-139066.84 25 138381.42
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
25 41266.29 50 -40580.87 25 76364.16 50 -76364.16 25 117630.45 50-116945.02
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
50 -36940.62 27 36255.20 50 -77835.09 27 77835.09 50-114775.71 27 114090.29
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
27 32272.11 51 -31586.68 27 61067.21 51 -61067.21 27 93339.31 51 -92653.88
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
51 -27871.96 29 27186.53
315.29 315.29
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
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LOAD
2 3
114
1 2 3
115
1 2 3
116
1 2 3
117
1 2 3
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1 2 3
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1 2 3
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1
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
51 -59596.29 29 59596.29 51 -87468.24 29 86782.82
0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
29 23457.56 52 -22635.05 29 39798.23 52 -39798.23 29 63255.79 52 -62433.29
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
52 -19438.44 31 18615.93 52 -37872.09 31 37872.09 52 -57310.54 31 56488.02
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
31 15092.39 53 -13995.72 31 9187.35 53 -9187.35 31 24279.74 53 -23183.06
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
53 -9781.59 33 8684.92 53 -17432.02 33 17432.02 53 -27213.61 33 26116.93
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
33 55 33 55 33 55
4835.98 -3739.30 2996.20 -2996.20 7832.19 -6735.51
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
37 57 37 57 37 57
2335.10 -1781.87 0.00 0.00 2335.10 -1781.87
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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38 59
1923.24 -1370.00
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
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MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
2
38 59 38 59
0.00 0.00 1923.24 -1370.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
39 61 39 61 39 61
2223.76 -1670.52 0.00 0.00 2223.76 -1670.52
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
40 63 40 63 40 63
2335.10 -1781.87 0.00 0.00 2335.10 -1781.87
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
41 65 41 65 41 65
2223.76 -1670.52 0.00 0.00 2223.76 -1670.52
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
42 67 42 67 42 67
1923.24 -1370.00 0.00 0.00 1923.24 -1370.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
43 69 43 69 43 69
2335.10 -1781.87 0.00 0.00 2335.10 -1781.87
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
44 -12179.95 70 12733.18 44 -25243.48 70 25243.48 44 -37423.43 70 37976.66
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
45 71
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
1
1 2 3
1 2 3
124
1 2 3
125
1 2 3
126
1 2 3
127
MMS AXIAL
3
123
STRUCTURE TYPE = SPACE
JT
2
122
29
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7159.11 -3430.41
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SHEAR-Y
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TORSION
MOM-Y
MOM-Z
2
45 71 45 71
0.00 0.00 7159.11 -3430.41
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00
46 -12179.95 72 12733.18 46 -25464.38 72 25464.38 46 -37644.33 72 38197.56
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
47 73 47 73 47 73
2335.10 -1781.87 0.00 0.00 2335.10 -1781.87
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
48 75 48 75 48 75
1923.24 -1370.00 0.00 0.00 1923.24 -1370.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
49 77 49 77 49 77
2223.76 -1670.52 0.00 0.00 2223.76 -1670.52
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
50 79 50 79 50 79
2335.10 -1781.87 0.00 0.00 2335.10 -1781.87
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
51 81 51 81 51 81
2223.76 -1670.52 0.00 0.00 2223.76 -1670.52
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
52 83
1923.24 -1370.00
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
1
1 2 3
1 2 3
131
1 2 3
132
1 2 3
133
1 2 3
134
MMS AXIAL
3
130
STRUCTURE TYPE = SPACE
JT
2
129
30
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MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
2
52 83 52 83
0.00 0.00 1923.24 -1370.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
53 85 53 85 53 85
2335.10 -1781.87 0.00 0.00 2335.10 -1781.87
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
54 86 54 86 54 86
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0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
35 36 35 36 35 36
0.00 0.00 0.00 0.00 0.00 0.00
254.49 254.49 0.00 0.00 254.49 254.49
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
56 8723.14 37 -9819.81 56 14340.29 37 -14340.29 56 23063.42 37 -24160.10
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
37 -13957.48 58 15054.15 37 -30849.05 58 30849.05 37 -44806.53 58 45903.21
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
58 18007.77 38 -18830.28 58 30849.06 38 -30849.06 58 48856.82 38 -49679.34
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
38 -23243.20 60 24065.71
378.35 378.35
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
1
1 2 3
1 2 3
138
1 2 3
139
1 2 3
140
1 2 3
141
MMS AXIAL
3
137
STRUCTURE TYPE = SPACE
JT
2
136
31
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LOAD
2 3
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1 2 3
143
1 2 3
144
1 2 3
145
1 2 3
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1 2 3
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1 2 3
148
1
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
38 -48691.34 60 48691.34 38 -71934.53 60 72757.05
0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
60 26769.63 39 -27455.06 60 48691.34 39 -48691.34 60 75460.96 39 -76146.39
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
39 -32003.57 62 32688.99 39 -65200.10 62 65200.10 39 -97203.66 62 97889.09
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
62 35614.73 40 -36300.16 62 65200.11 40 -65200.11 62 100814.84 40-101500.27
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
40 -41221.33 64 41906.75 40 -83042.38 64 83042.38 40-124263.71 64 124949.14
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
64 44832.49 41 -45517.91 64 83042.38 41 -83042.38 64 127874.88 41-128560.30
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
41 -50066.43 66 50751.85 41 -99551.15 66 99551.15 41-149617.58 66 150303.00
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
66 53455.77 42 -54278.28
378.35 378.35
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
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LOAD
2 3
149
1 2 3
150
1 2 3
151
1 2 3
152
1 2 3
153
1 2 3
154
1 2 3
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
66 99551.15 42 -99551.15 66 153006.92 42-153829.42
0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
42 -58691.20 68 59513.71 42-117393.42 68 117393.42 42-176084.62 68 176907.14
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
68 62467.32 43 -63564.01 68 117393.42 43-117393.42 68 179860.75 43-180957.44
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
43 -67701.70 70 68798.38 43-133902.25 70 133902.25 43-201603.95 70 202700.61
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
70 90684.20 45 -92050.73 70 168203.61 45-168203.61 70 258887.80 45-260254.33
628.61 628.61 0.00 0.00 628.61 628.61
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
45 92050.74 72 -90684.20 45 169653.31 72-169653.31 45 261704.06 72-260337.50
628.61 628.61 0.00 0.00 628.61 628.61
0.00 0.00 0.00 0.00 0.00 0.00
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0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
72 -68798.35 47 67701.67 72-135051.73 47 135051.73 72-203850.08 47 202753.41
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
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47 63564.01 74 -62467.33
504.47 504.47
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
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LOAD
2 3
156
1 2 3
157
1 2 3
158
1 2 3
159
1 2 3
160
1 2 3
161
1 2 3
162
1
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STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
47 119754.77 74-119754.77 47 183318.78 74-182222.09
0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
74 -59513.72 48 58691.21 74-119754.77 48 119754.77 74-179268.48 48 178445.98
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
48 54278.29 76 -53455.77 48 101515.98 76-101515.98 48 155794.25 76-154971.75
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
76 -50751.85 49 50066.43 76-101515.98 49 101515.98 76-152267.83 49 151582.41
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
49 45517.92 78 -44832.50 49 86219.02 78 -86219.02 49 131736.94 78-131051.52
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
78 -41906.76 50 41221.34 78 -86219.02 50 86219.02 78-128125.78 50 127440.35
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
50 36300.16 80 -35614.73 50 67980.22 80 -67980.22 50 104280.38 80-103594.95
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
80 -32689.00 51 32003.57
315.29 315.29
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 34 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
LOAD
2 3
163
1 2 3
164
1 2 3
165
1 2 3
166
1 2 3
167
1 2 3
168
1 2 3
169
1
JT
-- PAGE NO.
35
STRUCTURE TYPE = SPACE MMS AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
80 -67980.22 51 67980.22 80-100669.21 51 99983.80
0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
51 27455.06 82 -26769.64 51 52683.27 82 -52683.27 51 80138.33 82 -79452.91
315.29 315.29 0.00 0.00 315.29 315.29
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
82 -24065.72 52 23243.21 82 -52683.27 52 52683.27 82 -76748.98 52 75926.48
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
52 18830.28 84 -18007.78 52 24987.06 84 -24987.06 52 43817.34 84 -42994.84
378.35 378.35 0.00 0.00 378.35 378.35
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
84 -15054.17 53 13957.50 84 -24987.08 53 24987.08 84 -40041.26 53 38944.58
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
53 9819.81 86 -8723.13 53 1632.27 86 -1632.27 53 11452.08 86 -10355.40
504.47 504.47 0.00 0.00 504.47 504.47
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
4 31884.02 6 -31884.02 4 64324.40 6 -64324.40 4 96208.42 6 -96208.42
1049.48 1049.48 0.00 0.00 1049.48 1049.48
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
254.49 254.49
0.00 0.00
0.00 0.00
0.00 0.00
0.00 0.00
55 54
0.00 0.00
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 35 of 36
Saturday, February 02, 2008, 10:29 AM DXF IMPORT OF ACAD-89 SPAN.DXF
MEMBER END FORCES ----------------ALL UNITS ARE -- KG MEMBER
STRUCTURE TYPE = SPACE MMS
JT
AXIAL
SHEAR-Y
SHEAR-Z
TORSION
MOM-Y
MOM-Z
2
55 54 55 54
0.00 0.00 0.00 0.00
0.00 0.00 254.49 254.49
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00
44 45 44 45 44 45
0.00 0.00 0.00 0.00 0.00 0.00
254.49 254.49 0.00 0.00 254.49 254.49
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
45 46 45 46 45 46
0.00 0.00 0.00 0.00 0.00 0.00
254.49 254.49 0.00 0.00 254.49 254.49
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.00 0.00 0.00 0.00 0.00 0.00
1 2 3
171
36
LOAD
3
170
-- PAGE NO.
1 2 3
************** 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 * *********************************************************
C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\structure span 92.anl
Page 36 of 36
Job No
Sheet No
Rev
2
AA Part 0
Software licensed to (ñ Job Title
Client
Cantilever Erection Span 92m
RVNL
Ref
0
By
Adhi T
File
structure span 92.std
Date31-Jan-08 Date/Time
Chd
01-Feb-2008 17:31
56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 35 36 37 1
2
3
38 4
6
39 7
8
40 9
41
42
43 44 45 46 47
48
50
51
52
53 54 55
10 11 12 13 14 15 16 17 318 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34
Load 3
Y Z
49
X
Whole Structure Print Time/Date: 02/02/2008 10:26
STAAD.Pro for Windows Release 2003
Print Run 2 of 2
Z
V
U
Y
BOTTOM CHORD L0-L3 Section element
Rotation angle
Mirror
Sheet 20 x 750 Sheet 20 x 750 Sheet 150 x 20 Sheet 150 x 20 Sheet 150 x 20 Sheet 150 x 20
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 750.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 42000.0 -90.0 3005350000.0 3635050000.0 5226666.667 267.499 294.192 11184769.231 11184769.231 8014266.667 8014266.667 12210000.0 10003539.6 3635050000.0 3005350000.0 294.192 267.499 190.816 190.816 266.304 266.304 325.0 -375.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L0-L1.sec
2
mm deg 4 4
mm4 mm mm 3 3
mm3 3 mm 3 mm mm3 4 4
mm mm mm mm mm mm mm mm
Z
V
U
Y
BOTTOM CHORD L3-L5 Section element
Rotation angle
Mirror
Sheet 16 x 750 Sheet 16 x 750 Sheet 150 x 16 Sheet 150 x 16 Sheet 150 x 16 Sheet 150 x 16 Sheet 10 x 650 Sheet 10 x 650
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 750.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 46600.0 -90.0 2875927533.333 4157421933.333 3100614.214 248.425 298.689 12792067.487 12792067.487 7669140.089 7669140.089 13807008.0 10135825.8 4157421933.333 2875927533.333 298.689 248.425 164.574 164.574 274.508 274.508 325.0 -375.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L3-L5.sec
mm2 deg 04 04 4 mm mm mm 3 3 3
mm mm3 mm3 3 mm 4 0 04 mm mm mm mm mm mm mm mm
Z
V
U
Y
BOTTOM CHORD L5-L7 Section element
Rotation angle
Mirror
Sheet 16 x 750 Sheet 16 x 750 Sheet 150 x 16 Sheet 150 x 16 Sheet 150 x 16 Sheet 150 x 16 Sheet 16 x 650 Sheet 16 x 650
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 750.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 54400.0 -90.0 3150552533.333 4840850133.333 4362226.554 240.654 298.306 14894923.487 14894923.487 8401473.422 8401473.422 16116163.2 11404105.92 4840850133.333 3150552533.333 298.306 240.654 154.439 154.439 273.804 273.804 325.0 -375.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L5-L7.sec
mm2 deg 04 04 4 mm mm mm 3 3 3
mm mm3 mm3 3 mm 4 0 04 mm mm mm mm mm mm mm mm
Z
V
U
Y
BOTTOM CHORD L7-L9 Section element
Rotation angle
Mirror
Sheet 16 x 750 Sheet 16 x 750 Sheet 150 x 20 Sheet 150 x 20 Sheet 150 x 20 Sheet 150 x 20 Sheet 16 x 650 Sheet 16 x 650
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 750.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 56800.0 -90.0 3456433333.333 4976764533.333 5061605.754 246.683 296.005 15313121.641 15313121.641 9217155.556 9217155.556 16677763.2 12260620.32 4976764533.333 3456433333.333 296.005 246.683 162.274 162.274 269.597 269.597 325.0 -375.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L7-L9.sec
mm2 deg 04 04 4 mm mm mm 3 3 3
mm mm3 mm3 3 mm 4 0 04 mm mm mm mm mm mm mm mm
Z
V
U
Y
UPPER CHORD U1-U3 Section element
Rotation angle
Mirror
Sheet 650 x 20 Sheet 16 x 680 Sheet 16 x 680 Sheet 150 x 16 Sheet 150 x 16
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 39560.0 -90.0 2739658426.424 2916641986.667 3759516.755 263.16 271.527 8974283.036 8974283.036 6605851.68 9603807.407 10133620.0 9407411.743 2916641986.667 2739658426.424 271.527 263.16 166.983 242.766 226.852 226.852 325.0 -414.732
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\U1-U3.sec
2
mm deg 4 0 04 mm4 mm mm mm3 mm3 3 mm 3 mm mm3 mm3 4 0 4 0 mm mm mm mm mm mm mm mm
Z
V
U
Y
UPPER CHORD U3-U5 Section element
Rotation angle
Mirror
Sheet 650 x 16 Sheet 12 x 684 Sheet 12 x 684 Sheet 150 x 12 Sheet 150 x 12
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 30416.0 -90.0 2126515801.968 2247540634.667 1739410.241 264.413 271.833 6915509.645 6915509.645 5040267.891 7646732.934 7783504.0 7265618.315 2247540634.667 2126515801.968 271.833 264.413 165.711 251.405 227.364 227.364 325.0 -421.905
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\U3-U5.sec
2
mm deg 4 0 04 mm4 mm mm mm3 mm3 3 mm 3 mm mm3 mm3 4 0 4 0 mm mm mm mm mm mm mm mm
Z
V
U
Y
UPPER CHORD U5-U7 Section element
Rotation angle
Mirror
Sheet 650 x 16 Sheet 16 x 684 Sheet 16 x 684 Sheet 150 x 16 Sheet 150 x 16
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 37088.0 -90.0 2551305361.486 2837965642.667 2974837.708 262.28 276.622 8732201.977 8732201.977 6427788.991 8417872.515 9751696.0 8773774.159 2837965642.667 2551305361.486 276.622 262.28 173.312 226.97 235.445 235.445 325.0 -396.918
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\U5-U7.sec
2
mm deg 4 0 4 0 mm4 mm mm 3 mm mm3 mm3 3 mm 3 mm mm3 04 4 0 mm mm mm mm mm mm mm mm
Z
V
U
Y
UPPER CHORD U7-U9 Section element
Rotation angle
Mirror
Sheet 650 x 20 Sheet 16 x 680 Sheet 16 x 680 Sheet 150 x 16 Sheet 150 x 16
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 39560.0 -90.0 2739658426.424 2916641986.667 3759516.755 263.16 271.527 8974283.036 8974283.036 6605851.68 9603807.407 10133620.0 9407411.743 2916641986.667 2739658426.424 271.527 263.16 166.983 242.766 226.852 226.852 325.0 -414.732
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\U7-U9.sec
2
mm deg 4 0 4 0 mm4 mm mm 3 mm mm3 mm3 3 mm 3 mm mm3 04 4 0 mm mm mm mm mm mm mm mm
Z
V
U
Y
DIAGONAL BEAM L0-L3 Section element
Rotation angle
Mirror
Sheet 16 x 400 Sheet 16 x 400 Sheet 150 x 16 Sheet 150 x 16 Sheet 150 x 16 Sheet 150 x 16
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 400.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 22400.0 -90.0 524765866.667 1830189866.667 1791252.17 153.059 285.841 5631353.436 5631353.436 2623829.333 2623829.333 6304000.0 3122585.6 1830189866.667 524765866.667 285.841 153.059 117.135 117.135 251.4 251.4 325.0 -200.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\DiL0-L3.sec
2
mm deg 4
4
0 mm4 mm mm mm3 mm3 mm3 3 mm mm3 mm3 04 4
mm mm mm mm mm mm mm mm
Z
V
U
Y
DIAGONAL L3-L5 Section element
Rotation angle
Mirror
Sheet 12 x 400 Sheet 12 x 400 Sheet 150 x 12 Sheet 150 x 12 Sheet 150 x 12 Sheet 150 x 12
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 400.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 16800.0 -90.0 399065600.0 1398357600.0 757913.6 154.123 288.506 4302638.769 4302638.769 1995328.0 1995328.0 4776000.0 2356334.4 1398357600.0 399065600.0 288.506 154.123 118.77 118.77 256.109 256.109 325.0 -200.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\DiL3-L5.sec
2
mm deg 4 mm 4
mm4 mm mm 3 mm mm3 mm3 3 mm 3 mm mm3 4
mm mm mm mm mm mm mm mm mm
4
Z
V
U
Y
DIAGONAL BEAM L5-L8 Section element
Rotation angle
Mirror
Sheet 10 x 400 Sheet 10 x 400 Sheet 150 x 10 Sheet 150 x 10 Sheet 150 x 10 Sheet 150 x 10
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 400.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 14000.0 -90.0 334866666.667 1176116666.667 438745.455 154.658 289.842 3618820.513 3618820.513 1674333.333 1674333.333 4000000.0 1969610.0 1176116666.667 334866666.667 289.842 154.658 119.595 119.595 258.487 258.487 325.0 -200.0
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\DiL5-L8.sec
2
mm deg 4
4
0 mm4 mm mm 3 mm mm3 mm3 3 mm 3 mm mm3 04 4
mm mm mm mm mm mm mm mm
Z
V
Y
U
VERTICAL BEAM Section element
Rotation angle
Mirror
Sheet 10 x 250 Sheet 10 x 250 Sheet 630 x 10
Material
E (kg/mm^2)
Steel Steel Steel
20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 250.0 mm Basic geometry of the section Parameter Value 11300.0 A Sectional area -90.0 Angle of principal inertia axes α Iy Inertia moment about centroidal Y1-axis parallel 26094166.667 with Y-axis Iz Inertia moment about centroidal Z1-axis parallel 720414166.667 with Z-axis 354516.061 It Torsional moment of inertia (St. Venant) 48.054 iy Radius of inertia about Y1-axis 252.494 iz Radius of inertia about Z1-axis 2216658.974 W u+ Maximum resisting moment about U-axis 2216658.974 W u- Minimum resisting moment about U-axis 208753.333 W v+ Maximum resisting moment about V-axis 208753.333 Wv- Minimum resisting moment about V-axis 2592250.0 W pl,u Plastic resisting moment about U-axis 328250.0 W pl,v Plastic resisting moment about V-axis 720414166.667 Iu Maximum inertia moment 26094166.667 Iv Minimum inertia moment 252.494 iu Maximum radius of inertia 48.054 iv Minimum radius of inertia au+ Middle point along positive direction of Y(U)-axis 18.474 auMiddle point along negative direction of Y(U)-axis18.474 av+ Middle point along positive direction of Z(V)-axis 196.165 avMiddle point along negative direction of Z(V)-axis196.165 yM Coordinate of the center of gravity along Y-axis 325.0 zM Coordinate of the center of gravity along Z-axis -125.0
mm2 deg 4
4
mm4 mm mm mm3 mm3 3 mm 3 mm mm3 mm3 4
4
mm mm mm mm mm mm mm mm
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\vert.sec
Z
V
U
Y
END RAKER M0-L0 Section element
Rotation angle
Mirror
Sheet 20 x 680 Sheet 650 x 20 Sheet 150 x 20 Sheet 150 x 20 Sheet 20 x 600 Sheet 20 x 600 Sheet 20 x 680
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 70200.0 -90.0 3904559943.02 5575585000.0 8781357.576 235.84 281.823 17155646.154 17155646.154 10274387.435 12202836.257 19140500.0 14575120.628 5575585000.0 3904559943.02 281.823 235.84 146.359 173.83 244.382 244.382 325.0 -380.028
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\M0-L0.sec
mm2 deg 4
4
mm mm mm
4
3 3 3 3
mm 3 4 4
mm mm mm mm mm mm mm mm
3
Z
V
U
Y
END RAKER M0-U1 Section element
Rotation angle
Mirror
Sheet 12 x 688 Sheet 12 x 688 Sheet 650 x 12 Sheet 150 x 12 Sheet 150 x 12
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 700.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Sectional area Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis Inertia moment about centroidal Z1-axis parallel with Z-axis Torsional moment of inertia (St. Venant) Radius of inertia about Y1-axis Radius of inertia about Z1-axis Maximum resisting moment about U-axis Minimum resisting moment about U-axis Maximum resisting moment about V-axis Minimum resisting moment about V-axis Plastic resisting moment about U-axis Plastic resisting moment about V-axis Maximum inertia moment Minimum inertia moment Maximum radius of inertia Minimum radius of inertia Middle point along positive direction of Y(U)-axis Middle point along negative direction of Y(U)-axis Middle point along positive direction of Z(V)-axis Middle point along negative direction of Z(V)-axis Coordinate of the center of gravity along Y-axis Coordinate of the center of gravity along Z-axis
Value 27912.0 -90.0 1936201066.786 2165769176.0 1261351.68 263.378 278.555 6663905.157 6663905.157 4862221.705 6415791.989 7391627.88 6628764.883 2165769176.0 1936201066.786 278.555 263.378 174.198 229.858 238.747 238.747 325.0 -398.213
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\M0-U1.sec
2
mm deg 4 0 4
mm4 mm mm mm3 mm3 3 mm 3 mm mm3 mm3 4
4
0 mm mm mm mm mm mm mm mm
Z
V
U
Y
LINK MEMBER Section element
Rotation angle
Mirror
Sheet 20 x 680 Sheet 20 x 680 Sheet 20 x 680 Sheet 20 x 680 Sheet 16 x 680 Sheet 16 x 680
Material
E (kg/mm^2)
Steel Steel Steel Steel Steel Steel
20897.044 20897.044 20897.044 20897.044 20897.044 20897.044
The overall dimentions of the section are 650.0 x 680.0 mm Basic geometry of the section A α Iy Iz It iy iz W u+ W uW v+ WvW pl,u W pl,v Iu Iv iu iv au+ auav+ avyM zM
Parameter Value 76160.0 Sectional area -90.0 Angle of principal inertia axes Inertia moment about centroidal Y1-axis parallel with Y-axis2934698666.667 Inertia moment about centroidal Z1-axis parallel with Z-axis 6737900586.667 8568673.021 Torsional moment of inertia (St. Venant) 196.299 Radius of inertia about Y1-axis 297.44 Radius of inertia about Z1-axis 20732001.805 Maximum resisting moment about U-axis 20732001.805 Minimum resisting moment about U-axis 8631466.667 Maximum resisting moment about V-axis 8631466.667 Minimum resisting moment about V-axis 22619520.0 Plastic resisting moment about U-axis 12947198.88 Plastic resisting moment about V-axis 6737900586.667 Maximum inertia moment 2934698666.667 Minimum inertia moment 297.44 Maximum radius of inertia 196.299 Minimum radius of inertia 113.333 Middle point along positive direction of Y(U)-axis 113.333 Middle point along negative direction of Y(U)-axis 272.216 Middle point along positive direction of Z(V)-axis 272.216 Middle point along negative direction of Z(V)-axis 325.0 Coordinate of the center of gravity along Y-axis -340.0 Coordinate of the center of gravity along Z-axis
File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\link.sec
2
mm deg 4 0 04 mm4 mm mm 3 3 3
mm 3 mm mm3 mm3 4 0 4 0 mm mm mm mm mm mm mm mm
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