Method of Design Cantilever Erection

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    DESIGN OF LINK ARRANGEMENT AND BUFFER

    FOR

    CANTILEVER ERECTION

    92M SPAN STEEL BRIDGE

    EAST COAST RAILWAY

    RAIL VIKAS NIGAM LIMITEDPMC : WILBUR SMITH ASSOCIATES LTD

    CONTRACTOR : HCIL ADHI KARYA ARSS (JV)Construction of Doubling railway line between Barang-Rajathgarh, Barang-Cuttack,and

    3rd Line Between Barang-Khurda Road

    PROJPROJPROJPROJ

    PROJPROJPROJPROJ

    PROJPROJPROJPROJ

    PROJPROJPROJPROJ

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    ARRANGEMENT OF LINK AND BUFFER

    Ref. drg. No. 9114/E/DD-22-101 (ALT-1) (R5)

    c/c of pier : 93231 mm

    c/c of bearing : 92000 mm

    c/c of bearing at pier = 93231 92000 = 1231 mm

    Distance between U15 and U1 = 2 x 5750 + 1231 = 12731 mm

    EXTENSION PIECE

    Max erection force = 1255.2 t ~ 1256 t

    Try 2PL 680x20 + 1PL 680x16 (Yst=36 kg/mm2) with each gusset

    Gross area = 4x68x2 + 2x68x1.6 = 761.6 cm2

    Holes =10x(2+2+1.6)x2.35 = 131.6 cm2

    = 630.0 cm2

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    Tension allowed = 630x2130x1.25 = 1677 t > 1256 t ok

    EXTENSION PIECE ACROSS PIN HOLE

    Net area req :

    =

    cm2Try 2 additional plate 660x12 and 660x10 with each gusset

    with 250 pin

    Gross area of main section = 761.6 cm2

    Add. PL 2x66x(1.2+1) = 290.4 cm2

    = 1052.0 cm2

    Deduction for holes

    2x25x7.8 =-390.00 cm2

    8x7.8x2.15 =-134.16 cm2

    = 527.84 cm2 > 475cm2 ok

    Longitudinal net sectional are to be provided to additional

    plate beyond pin holes

    = 2xbx7.8 = 475 cm2 b=30.5 cm

    Hence b1 (min) req

    = 30.5+2x2.15+25/2 = 47.3 cm provide b1 = 500mm

    LINK

    Pmax = 1255.2 t ~ 1256 t

    Try 2PL 680x20 + 1PL 680x16 (Yst=36 kg/mm2) with each gusset

    Gross area = 4x68x2 + 2x68x1.6 = 761.6 cm2

    Holes =10x(2+2+1.6)x2.35 = 131.6 cm2

    = 630.0 cm2

    Tension allowed = 630x2130x1.25 = 1677 t > 1256 t ok

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    LINK ACROSS PIN HOLE

    Gross area of main section = 761.6 cm2

    Add. PL 2x66x(1.2+1) = 290.4 cm2

    = 1052.0 cm2

    Deduction for holes

    2x25x7.8 =-390.00 cm2

    8x7.8x2.35 =-146.64 cm2

    = 515.36 cm2

    > 475cm2 ok

    Longitudinal net sectional are to be provided to additional plate

    beyond pin holes

    = 2xbx7.8 = 475 cm2

    b=30.5 cm

    Hence b1 (min) req

    = 30.5+2x2.15+25/2 = 47.3 cm provide b1 = 500mm

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    LINK PIN

    Material : carbon steel class 4 to IS-1875 or equivalent

    LINK ARRANGEMENT (IN PLAN)

    e =

    + 4 = 90 mm

    w1 = ( x 1256)/ 9.4 =66.81 t/cm

    w2 = ( x 1256)/ 7.8 = 80.51t/cm

    Try 250 mm dia pin

    B.M = (66.81 x 9.4) x 9.0 80.51 x

    = 5655 612 = 5043 t.cm

    Bending Stress =

    = (5043 x 1000)/( x 253/32) =3287 kg/cm2 < 2990 (table 1 ) x 1.25 (ok)

    Shear stress on pin = 1256000/(2 x /4 x 252) = 1279 kg/cm2 < 1420 x 1.25 (ok) (table 1)

    Min. bearing area provided on each side of pin = 7.8 cm x 25.0 cm = 195 cm

    2

    Bearing Stress on H.T.S Steel plate = 1256000/(2x195) = 3220 kg/cm2 < 2600 (table 1) x 1.25=3250

    kg/cm2

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    BUFFER SLAB

    Material : Grade 58HTC to I.S 961 or equivalent with st = 35 kg/mm2

    Try 1000 mm wide x 900 mm high slab

    Let t = thickness in mm.

    Length of line contract from buffer = 650 mm

    Total buffer force = 1192 t (phase 2)

    w = 1192/100 = 11.92 t/cmMA = (11.92 x 17.5

    2

    ) / 2 = 1825.25 t.cm

    RA = 1192/2 = 596.1 t

    MC = 596.1 x 32.5 11.92 x (502/2) = 19373 14900 = 4470 t.cm

    Allowable bending stress

    = 2280 x 1.25 = 2850 kg/cm2

    =2.88 t/cm

    2

    t =

    =

    = 10.22 cm, Provide t= 100 mm

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    BUFFER

    Let L= contact length of buffer = 650 mm (Ref. cl. 3.12.3 of steel Bridge code)

    Allowable working load per unit length of roller = 0.8 D kg/mm length

    Where D = diameter of roller in mm

    = 0.8D

    Or D = (1192 x 1000) / (0.8 x 650) = 2292 mm

    Provide D = 2300 mm ( i.e radius = 1150 mm)

    Check bottom chord area in bearing

    Gross area of bottom chord (L0 L1) = 420 cm2 ( increased section area )

    Bearing stress ( on H.T.S material of main bridge )

    = 1192000/420 = 2838 kg / cm2

    < 2600 * 1.25 = 3250 kg / cm2

    ( Table II for H.T.S steel ) ok

    Check Link member for crane load

    Span 6.5 m

    A . Crane wheel load = 7.0 t per wheel

    B . UDL

    Self weight of link : 4 x 0.68 x 157.0 + 2 x 0.68 x 125.6 = 598 kg / m

    Self weight of track : 0.46 / 5.75 = 80 kg / m

    = 678 kg / m ~ 0.7 t/m

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    Section used for link :

    4PL 680 x 20 + 2PL 680 x 16 (HTS)

    I xx = (4 x 2.0 + 2.0 x 1.6) x 683

    / 12 = 293470 cm4

    Zxx = 293470 / 34.0 = 8631 cm3

    B.M = 7.0 x + 0.7 x

    =11.38 + 3.7 = 15.08 tm

    Bending Stress = (15.08 x 105) / 8631 = 175 kg/cm

    2< (2250 kg/cm

    2(for HTS) x 1.25 (erection) ok.

    LINK PROP

    Loads :

    Crane wheel = 7.0 ton

    Crack Track 0.7 t/m x 6.5 m = 4.6 ton

    Self wt.say 2/ mc-300 = 2 x 12.25 m @ 35.8 kg/m = 0.9 ton

    = 12.5 ton

    Area = 2 x 45.64 = 91.28 cm2

    r xx = 11.81 cm

    l/r = (1.0 x 1225)/11.81 = 104 < 140 (cl.6.2.3)

    Ref. Table IV,, Yst = 26 kg/mm2

    (P=17.8)

    Allowable compression during erection = 91.28 x 0.794 x 1.25 = 90.5 ton > 12.5 ton o.k

    Use 2/MC-300

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    LINK SHORTENING

    As per computer output , enclosed.

    Deflection at free end of cantilever span = 106.71 cm

    Shortening of link to neutralize this deflection

    = * h/L where, = 106.71 cm

    h = 12.250 m

    L = 92.0 m

    = 106.71 x = 14.21 cm .. (1)

    Shortening of link to neutralize camber effect of Top chord

    = 4 x (5756 5750 ) + 10 x (5758 5750) = 104 mm = 10.4 cm .. (2)

    Shortening of link to keep free end at least 150 mm above top of bearing

    = 15 cm x m = 1.99 cm 2.0 cm . (3)

    Total Shortening

    = (1) + (2) + (3)

    = 14.21 + 10.4 + 2.0 = 26.61 cm 270 mm

    Nominal length of link between pin centers (ref. page 1)

    = 12731 2 x 1000 = 10731 mm

    Actual length to be fabricated

    = 10731 270 = 10461 mm 10470 mm

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    PAGE NO. 1

    ****************************************************

    * *

    * STAAD.Pro *

    * Version 2003 Bld 1001.US *

    * Proprietary Program of *

    * Research Engineers, Intl. *

    * Date= FEB 1, 2008 *

    * Time= 17:31:20 *

    * *

    * USER ID: *

    ****************************************************

    1. STAAD SPACE DXF IMPORT OF ACAD-89 SPAN.DXF

    2. START JOB INFORMATION

    3. JOB NAME CANTILEVER ERECTION SPAN 92M

    4. JOB CLIENT RVNL

    5. JOB NO AA

    6. JOB PART 0

    7. JOB REF 0

    8. ENGINEER NAME ADHI T

    9. ENGINEER DATE 31-JAN-08

    10. END JOB INFORMATION

    11. INPUT WIDTH 79

    12. OUTPUT WIDTH 118

    13. OUTPUT WIDTH 72

    14. UNIT METER KG

    15. JOINT COORDINATES

    16. 1 0 0 0; 2 5.75 0 0; 3 11.5 0 0; 4 17.25 0 0; 6 23 0 0; 7 28.75 0 0

    17. 8 34.5 0 0; 9 40.25 0 0; 10 46 0 0; 11 51.75 0 0; 12 57.5 0 0; 13 63.25 0 0

    18. 14 69 0 0; 15 74.75 0 0; 16 80.5 0 0; 17 86.25 0 0; 18 92 0 0; 19 97.75 0 0

    19. 20 103.5 0 0; 21 109.25 0 0; 22 115 0 0; 23 120.75 0 0; 24 126.5 0 0

    20. 25 132.25 0 0; 26 138 0 0; 27 143.75 0 0; 28 149.5 0 0; 29 155.25 0 0

    21. 30 161 0 0; 31 166.75 0 0; 32 172.5 0 0; 33 178.25 0 0; 34 184 0 0

    22. 35 0 6.25 0; 36 5.75 6.25 0; 37 11.5 6.25 0; 38 23 6.25 0; 39 34.5 6.25 0

    23. 40 46 6.25 0; 41 57.5 6.25 0; 42 69 6.25 0; 43 80.5 6.25 0; 44 86.25 6.25 0

    24. 45 92 6.25 0; 46 97.75 6.25 0; 47 103.5 6.25 0; 48 115 6.25 0; 49 126.5 6.25 0

    25. 50 138 6.25 0; 51 149.5 6.25 0; 52 161 6.25 0; 53 172.5 6.25 0

    26. 54 178.25 6.25 0; 55 184 6.25 0; 56 5.75 12.5 0; 57 11.5 12.5 0

    27. 58 17.25 12.5 0; 59 23 12.5 0; 60 28.75 12.5 0; 61 34.5 12.5 0

    28. 62 40.25 12.5 0; 63 46 12.5 0; 64 51.75 12.5 0; 65 57.5 12.5 0

    29. 66 63.25 12.5 0; 67 69 12.5 0; 68 74.75 12.5 0; 69 80.5 12.5 0

    30. 70 86.25 12.5 0; 71 92 12.5 0; 72 97.75 12.5 0; 73 103.5 12.5 0

    31. 74 109.25 12.5 0; 75 115 12.5 0; 76 120.75 12.5 0; 77 126.5 12.5 0

    32. 78 132.25 12.5 0; 79 138 12.5 0; 80 143.75 12.5 0; 81 149.5 12.5 0

    33. 82 155.25 12.5 0; 83 161 12.5 0; 84 166.75 12.5 0; 85 172.5 12.5 0

    34. 86 178.25 12.5 0

    35. MEMBER INCIDENCES

    36. 1 1 2; 2 2 3; 3 3 4; 5 6 7; 6 7 8; 7 8 9; 8 9 10; 9 10 11; 10 11 12; 11 12 13

    37. 12 13 14; 13 14 15; 14 15 16; 15 16 17; 16 17 18; 17 18 19; 18 19 20; 19 20 21

    38. 20 21 22; 21 22 23; 22 23 24; 23 24 25; 24 25 26; 25 26 27; 26 27 28; 27 28 29

    39. 28 29 30; 29 30 31; 30 31 32; 31 32 33; 32 33 34; 33 1 35; 34 2 36; 35 3 37

    40. 36 6 38; 37 8 39; 38 10 40; 39 12 41; 40 14 42; 41 16 43; 42 17 44; 43 18 45

    41. 44 19 46; 45 20 47; 46 22 48; 47 24 49; 48 26 50; 49 28 51; 50 30 52; 51 32 53

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 2

    42. 52 33 54; 53 34 55; 54 36 56; 55 35 56; 56 56 57; 57 57 58; 58 58 59; 59 59 60

    43. 60 60 61; 61 61 62; 62 62 63; 63 63 64; 64 64 65; 65 65 66; 66 66 67; 67 67 68

    44. 68 68 69; 69 69 70; 70 70 71; 71 71 72; 72 72 73; 73 73 74; 74 74 75; 75 75 76

    45. 76 76 77; 77 77 78; 78 78 79; 79 79 80; 80 80 81; 81 81 82; 82 82 83; 83 83 84

    46. 84 84 85; 85 85 86; 86 86 55; 87 35 2; 88 2 37; 89 37 4; 90 4 38; 91 38 7

    47. 92 7 39; 93 39 9; 94 9 40; 95 40 11; 96 11 41; 97 41 13; 98 13 42; 99 42 15

    48. 100 15 43; 101 43 17; 102 17 45; 103 45 19; 104 19 47; 105 47 21; 106 21 48

    49. 107 48 23; 108 23 49; 109 49 25; 110 25 50; 111 50 27; 112 27 51; 113 51 29

    50. 114 29 52; 115 52 31; 116 31 53; 117 53 33; 118 33 55; 119 37 57; 120 38 59

    51. 121 39 61; 122 40 63; 123 41 65; 124 42 67; 125 43 69; 126 44 70; 127 45 71

    52. 128 46 72; 129 47 73; 130 48 75; 131 49 77; 132 50 79; 133 51 81; 134 52 83

    53. 135 53 85; 136 54 86; 137 35 36; 138 56 37; 139 37 58; 140 58 38; 141 38 60

    54. 142 60 39; 143 39 62; 144 62 40; 145 40 64; 146 64 41; 147 41 66; 148 66 42

    55. 149 42 68; 150 68 43; 151 43 70; 152 70 45; 153 45 72; 154 72 47; 155 47 74

    56. 156 74 48; 157 48 76; 158 76 49; 159 49 78; 160 78 50; 161 50 80; 162 80 51

    57. 163 51 82; 164 82 52; 165 52 84; 166 84 53; 167 53 86; 168 4 6; 169 55 54

    58. 170 44 45; 171 45 46

    59. UNIT MMS KG

    60. DEFINE MATERIAL START

    61. ISOTROPIC STEEL

    62. E 20904.2

    63. POISSON 0.3

    64. DENSITY 7.83341E-006

    65. ALPHA 6.5E-006

    66. DAMP 0.03

    67. END DEFINE MATERIAL

    68. CONSTANTS

    69. MATERIAL STEEL MEMB 1 TO 3 5 TO 171

    70. START USER TABLE

    71. TABLE 1

    72. UNIT METER KG

    73. PRISMATIC

    74. L0-L1

    75. 0.042 0.00300535 0.003635 5.227E-006 0 0 0.75 0.65

    76. L3-L5

    77. 0.0466 0.002876 0.004157 3.101E-006 0 0 0.75 0.65

    78. L5-L7

    79. 0.0544 0.00315055 0.00484085 4.362E-006 0 0 0.75 0.65

    80. L7-L9

    81. 0.0568 0.003456 0.004977 5.06161E-006 0 0 0.75 0.65

    82. U1-U3

    83. 0.03956 0.00273966 0.00291664 3.75952E-006 0 0 0.7 0.65

    84. U3-U5

    85. 0.030416 0.00212652 0.00224754 1.73941E-006 0 0 0.7 0.65

    86. U5-U7

    87. 0.037088 0.00255131 0.00283797 2.97484E-006 0 0 0.7 0.65

    88. U7-U9

    89. 0.03956 0.00273966 0.00291664 3.75952E-006 0 0 0.7 0.65

    90. M0-L0

    91. 0.0702 0.00390456 0.00557558 8.78136E-006 0 0 0.7 0.65

    92. M0-U1

    93. 0.027912 0.0019362 0.00216577 1.26135E-006 0 0 0.7 0.65

    94. VERT

    95. 0.0113 2.60942E-005 0.000720414 3.54516E-007 0 0 0.25 0.65

    96. DIL0-L3

    97. 0.0224 0.000524766 0.00183019 1.79125E-006 0 0 0.4 0.65

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 3

    98. DIL3-L5

    99. 0.0168 0.000399066 0.00139836 7.57914E-007 0 0 0.4 0.65

    100. DIL5-L8

    101. 0.014 0.000334867 0.00117612 4.38745E-007 0 0 0.4 0.65

    102. LINK

    103. 0.07616 0.0029347 0.0067379 8.56867E-006 0 0 0.68 0.65

    104. END

    105. UNIT MMS KG

    106. MEMBER PROPERTY AMERICAN

    107. 1 TO 3 14 TO 19 30 TO 32 UPTABLE 1 L0-L1

    108. 5 12 13 20 21 28 29 168 UPTABLE 1 L3-L5

    109. MEMBER PROPERTY AMERICAN

    110. 6 7 10 11 22 23 26 27 UPTABLE 1 L5-L7

    111. 8 9 24 25 UPTABLE 1 L7-L9

    112. 56 57 68 69 72 73 84 85 UPTABLE 1 U1-U3

    113. 58 59 66 67 74 75 82 83 UPTABLE 1 U3-U5

    114. 60 61 64 65 76 77 80 81 UPTABLE 1 U5-U7

    115. 62 63 78 79 UPTABLE 1 U7-U9

    116. 33 43 53 UPTABLE 1 M0-L0

    117. 55 86 152 153 UPTABLE 1 M0-U1

    118. 34 TO 42 44 TO 52 54 119 TO 126 128 TO 137 169 TO 171 UPTABLE 1 VERT

    119. 87 TO 89 100 TO 105 116 TO 118 138 139 150 151 154 155 166 -

    120. 167 UPTABLE 1 DIL0-L3

    121. 90 91 98 99 106 107 114 115 140 141 148 149 156 157 164 165 UPTABLE 1 DIL3-L5

    122. 92 TO 97 108 TO 113 142 TO 147 158 TO 163 UPTABLE 1 DIL5-L8

    123. 70 71 127 UPTABLE 1 LINK

    124. SUPPORTS

    125. 1 PINNED

    126. 18 FIXED BUT FX MX MY MZ

    127. UNIT METER KG

    128. MEMBER TRUSS

    129. 1 TO 3 5 TO 171

    130. UNIT MMS KG

    131. LOAD 1 LOAD 1 DEAD LOAD

    132. SELFWEIGHT Y -1

    133. LOAD 2 LOAD 2 ERECTION

    134. JOINT LOAD

    135. 1 18 FY -6320

    136. 2 TO 4 6 TO 17 FY -12640

    137. 19 TO 28 FY -12340

    138. 29 FY -14570

    139. 30 FY -21800

    140. 31 FY -21110

    141. 32 FY -11120

    142. 33 FY -9620

    143. 34 FY -4410

    144. UNIT METER KG

    145. LOAD COMB 3 LOAD COMBINATION

    146. 1 1.0 2 1.0

    147. UNIT MMS KG

    148. PERFORM ANALYSIS

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 4

    P R O B L E M S T A T I S T I C S

    -----------------------------------

    NUMBER OF JOINTS/MEMBER+ELEMENTS/SUPPORTS = 85/ 170/ 2

    ORIGINAL/FINAL BAND-WIDTH= 34/ 4/ 30 DOF

    TOTAL PRIMARY LOAD CASES = 2, TOTAL DEGREES OF FREEDOM = 505

    SIZE OF STIFFNESS MATRIX = 16 DOUBLE KILO-WORDS

    REQRD/AVAIL. DISK SPACE = 12.4/ 25300.5 MB, EXMEM = 520.2 MB

    ZERO STIFFNESS IN DIRECTION 4 AT JOINT 1 EQN.NO. 1

    LOADS APPLIED OR DISTRIBUTED HERE FROM ELEMENTS WILL BE IGNORED.

    THIS MAY BE DUE TO ALL MEMBERS AT THIS JOINT BEING RELEASED OR

    EFFECTIVELY RELEASED IN THIS DIRECTION.

    ZERO STIFFNESS IN DIRECTION 5 AT JOINT 1 EQN.NO. 2

    ZERO STIFFNESS IN DIRECTION 6 AT JOINT 1 EQN.NO. 3

    ZERO STIFFNESS IN DIRECTION 3 AT JOINT 2 EQN.NO. 6

    ZERO STIFFNESS IN DIRECTION 4 AT JOINT 2 EQN.NO. 7

    ZERO STIFFNESS IN DIRECTION 5 AT JOINT 2 EQN.NO. 8

    ZERO STIFFNESS IN DIRECTION 6 AT JOINT 2 EQN.NO. 9

    ZERO STIFFNESS IN DIRECTION 3 AT JOINT 35 EQN.NO. 12

    ZERO STIFFNESS IN DIRECTION 4 AT JOINT 35 EQN.NO. 13

    ZERO STIFFNESS IN DIRECTION 5 AT JOINT 35 EQN.NO. 14

    ZERO STIFFNESS IN DIRECTION 6 AT JOINT 35 EQN.NO. 15

    ZERO STIFFNESS IN DIRECTION 3 AT JOINT 3 EQN.NO. 18

    **WARNING - THERE WERE MORE THAN 12 DOF WITH ZERO STIFFNESS.

    THE FIRST 12 ARE LISTED ABOVE.

    TOTAL # TRANSLATIONAL= 83 TOTAL # ROTATIONAL= 255

    149. PRINT ANALYSIS RESULTS

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 5

    JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = SPACE

    ------------------

    JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN

    1 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000

    2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000

    3 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000

    2 1 0.0000 0.2373 0.0000 0.0000 0.0000 0.0000

    2 0.0000 0.4570 0.0000 0.0000 0.0000 0.0000

    3 0.0000 0.6944 0.0000 0.0000 0.0000 0.0000

    3 1 -0.0060 0.4833 0.0000 0.0000 0.0000 0.0000

    2 -0.0142 0.9161 0.0000 0.0000 0.0000 0.0000

    3 -0.0202 1.3994 0.0000 0.0000 0.0000 0.0000

    4 1 -0.0120 0.7428 0.0000 0.0000 0.0000 0.0000

    2 -0.0284 1.4176 0.0000 0.0000 0.0000 0.0000

    3 -0.0403 2.1604 0.0000 0.0000 0.0000 0.0000

    6 1 -0.0308 1.0129 0.0000 0.0000 0.0000 0.0000

    2 -0.0663 1.9287 0.0000 0.0000 0.0000 0.0000

    3 -0.0971 2.9416 0.0000 0.0000 0.0000 0.0000

    7 1 -0.0496 1.2741 0.0000 0.0000 0.0000 0.0000

    2 -0.1043 2.4347 0.0000 0.0000 0.0000 0.0000

    3 -0.1539 3.7088 0.0000 0.0000 0.0000 0.0000

    8 1 -0.0831 1.5422 0.0000 0.0000 0.0000 0.0000

    2 -0.1697 2.9445 0.0000 0.0000 0.0000 0.0000

    3 -0.2528 4.4867 0.0000 0.0000 0.0000 0.0000

    9 1 -0.1165 1.7806 0.0000 0.0000 0.0000 0.0000

    2 -0.2351 3.4034 0.0000 0.0000 0.0000 0.0000

    3 -0.3516 5.1840 0.0000 0.0000 0.0000 0.0000

    10 1 -0.1710 2.0061 0.0000 0.0000 0.0000 0.0000

    2 -0.3409 3.8351 0.0000 0.0000 0.0000 0.0000

    3 -0.5119 5.8412 0.0000 0.0000 0.0000 0.0000

    11 1 -0.2255 2.1635 0.0000 0.0000 0.0000 0.0000

    2 -0.4468 4.1363 0.0000 0.0000 0.0000 0.0000

    3 -0.6723 6.2998 0.0000 0.0000 0.0000 0.0000

    12 1 -0.3120 2.2988 0.0000 0.0000 0.0000 0.0000

    2 -0.6137 4.3949 0.0000 0.0000 0.0000 0.0000

    3 -0.9257 6.6936 0.0000 0.0000 0.0000 0.0000

    13 1 -0.3985 2.3067 0.0000 0.0000 0.0000 0.0000

    2 -0.7806 4.4158 0.0000 0.0000 0.0000 0.0000

    3 -1.1791 6.7225 0.0000 0.0000 0.0000 0.0000

    14 1 -0.5413 2.2341 0.0000 0.0000 0.0000 0.0000

    2 -1.0555 4.2713 0.0000 0.0000 0.0000 0.0000

    3 -1.5968 6.5055 0.0000 0.0000 0.0000 0.0000

    15 1 -0.6840 1.9247 0.0000 0.0000 0.0000 0.0000

    2 -1.3305 3.6857 0.0000 0.0000 0.0000 0.0000

    3 -2.0145 5.6104 0.0000 0.0000 0.0000 0.0000

    16 1 -0.8962 1.4772 0.0000 0.0000 0.0000 0.0000

    2 -1.7391 2.8276 0.0000 0.0000 0.0000 0.0000

    3 -2.6353 4.3049 0.0000 0.0000 0.0000 0.0000

    17 1 -1.1085 0.6638 0.0000 0.0000 0.0000 0.0000

    2 -2.1476 1.2863 0.0000 0.0000 0.0000 0.0000

    3 -3.2561 1.9502 0.0000 0.0000 0.0000 0.0000

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 6

    JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = SPACE

    ------------------

    JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN

    18 1 -1.3765 0.0000 0.0000 0.0000 0.0000 0.0000

    2 -2.6603 0.0000 0.0000 0.0000 0.0000 0.0000

    3 -4.0368 0.0000 0.0000 0.0000 0.0000 0.0000

    19 1 -1.6445 -1.6374 0.0000 0.0000 0.0000 0.0000

    2 -3.1730 -3.1190 0.0000 0.0000 0.0000 0.0000

    3 -4.8175 -4.7564 0.0000 0.0000 0.0000 0.0000

    20 1 -1.8567 -3.1252 0.0000 0.0000 0.0000 0.0000

    2 -3.5800 -5.9820 0.0000 0.0000 0.0000 0.0000

    3 -5.4367 -9.1071 0.0000 0.0000 0.0000 0.0000

    21 1 -2.0689 -4.9789 0.0000 0.0000 0.0000 0.0000

    2 -3.9870 -9.5248 0.0000 0.0000 0.0000 0.0000

    3 -6.0559 -14.5037 0.0000 0.0000 0.0000 0.0000

    22 1 -2.2117 -6.9707 0.0000 0.0000 0.0000 0.0000

    2 -4.2592 -13.3475 0.0000 0.0000 0.0000 0.0000

    3 -6.4709 -20.3182 0.0000 0.0000 0.0000 0.0000

    23 1 -2.3544 -9.1993 0.0000 0.0000 0.0000 0.0000

    2 -4.5315 -17.6107 0.0000 0.0000 0.0000 0.0000

    3 -6.8859 -26.8100 0.0000 0.0000 0.0000 0.0000

    24 1 -2.4409 -11.5084 0.0000 0.0000 0.0000 0.0000

    2 -4.6942 -22.0259 0.0000 0.0000 0.0000 0.0000

    3 -7.1352 -33.5343 0.0000 0.0000 0.0000 0.0000

    25 1 -2.5274 -13.9449 0.0000 0.0000 0.0000 0.0000

    2 -4.8569 -26.6694 0.0000 0.0000 0.0000 0.0000

    3 -7.3844 -40.6143 0.0000 0.0000 0.0000 0.0000

    26 1 -2.5819 -16.4035 0.0000 0.0000 0.0000 0.0000

    2 -4.9572 -31.3741 0.0000 0.0000 0.0000 0.0000

    3 -7.5391 -47.7776 0.0000 0.0000 0.0000 0.0000

    27 1 -2.6364 -18.9302 0.0000 0.0000 0.0000 0.0000

    2 -5.0574 -36.2038 0.0000 0.0000 0.0000 0.0000

    3 -7.6939 -55.1340 0.0000 0.0000 0.0000 0.0000

    28 1 -2.6699 -21.4698 0.0000 0.0000 0.0000 0.0000

    2 -5.1146 -41.0309 0.0000 0.0000 0.0000 0.0000

    3 -7.7844 -62.5007 0.0000 0.0000 0.0000 0.0000

    29 1 -2.7033 -24.0391 0.0000 0.0000 0.0000 0.0000

    2 -5.1717 -45.8920 0.0000 0.0000 0.0000 0.0000

    3 -7.8750 -69.9311 0.0000 0.0000 0.0000 0.0000

    30 1 -2.7221 -26.6015 0.0000 0.0000 0.0000 0.0000

    2 -5.1987 -50.7971 0.0000 0.0000 0.0000 0.0000

    3 -7.9208 -77.3986 0.0000 0.0000 0.0000 0.0000

    31 1 -2.7409 -29.1728 0.0000 0.0000 0.0000 0.0000

    2 -5.2256 -55.6300 0.0000 0.0000 0.0000 0.0000

    3 -7.9666 -84.8028 0.0000 0.0000 0.0000 0.0000

    32 1 -2.7469 -31.7335 0.0000 0.0000 0.0000 0.0000

    2 -5.2347 -60.3931 0.0000 0.0000 0.0000 0.0000

    3 -7.9816 -92.1266 0.0000 0.0000 0.0000 0.0000

    33 1 -2.7529 -34.2807 0.0000 0.0000 0.0000 0.0000

    2 -5.2438 -65.1344 0.0000 0.0000 0.0000 0.0000

    3 -7.9967 -99.4151 0.0000 0.0000 0.0000 0.0000

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 8

    JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = SPACE

    ------------------

    JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN

    50 1 -0.0387 -16.3960 0.0000 0.0000 0.0000 0.0000

    2 -0.1059 -31.3415 0.0000 0.0000 0.0000 0.0000

    3 -0.1445 -47.7374 0.0000 0.0000 0.0000 0.0000

    51 1 -0.0207 -21.4626 0.0000 0.0000 0.0000 0.0000

    2 -0.1079 -40.9982 0.0000 0.0000 0.0000 0.0000

    3 -0.1286 -62.4608 0.0000 0.0000 0.0000 0.0000

    52 1 -0.0072 -26.5952 0.0000 0.0000 0.0000 0.0000

    2 -0.0450 -50.7394 0.0000 0.0000 0.0000 0.0000

    3 -0.0522 -77.3346 0.0000 0.0000 0.0000 0.0000

    53 1 -0.0028 -31.7278 0.0000 0.0000 0.0000 0.0000

    2 -0.1050 -60.3637 0.0000 0.0000 0.0000 0.0000

    3 -0.1077 -92.0915 0.0000 0.0000 0.0000 0.0000

    54 1 -0.0064 -34.2806 0.0000 0.0000 0.0000 0.0000

    2 -0.0788 -65.1370 0.0000 0.0000 0.0000 0.0000

    3 -0.0852 -99.4176 0.0000 0.0000 0.0000 0.0000

    55 1 -0.0064 -36.8181 0.0000 0.0000 0.0000 0.0000

    2 -0.0788 -69.8935 0.0000 0.0000 0.0000 0.0000

    3 -0.0852 -106.7116 0.0000 0.0000 0.0000 0.0000

    56 1 -0.4952 0.2396 0.0000 0.0000 0.0000 0.0000

    2 -0.9530 0.4750 0.0000 0.0000 0.0000 0.0000

    3 -1.4482 0.7146 0.0000 0.0000 0.0000 0.0000

    57 1 -0.4888 0.4836 0.0000 0.0000 0.0000 0.0000

    2 -0.9417 0.9495 0.0000 0.0000 0.0000 0.0000

    3 -1.4305 1.4331 0.0000 0.0000 0.0000 0.0000

    58 1 -0.4824 0.7397 0.0000 0.0000 0.0000 0.0000

    2 -0.9303 1.4438 0.0000 0.0000 0.0000 0.0000

    3 -1.4128 2.1835 0.0000 0.0000 0.0000 0.0000

    59 1 -0.4540 1.0148 0.0000 0.0000 0.0000 0.0000

    2 -0.8778 1.9622 0.0000 0.0000 0.0000 0.0000

    3 -1.3318 2.9770 0.0000 0.0000 0.0000 0.0000

    60 1 -0.4255 1.2635 0.0000 0.0000 0.0000 0.0000

    2 -0.8253 2.4425 0.0000 0.0000 0.0000 0.0000

    3 -1.2508 3.7060 0.0000 0.0000 0.0000 0.0000

    61 1 -0.3767 1.5443 0.0000 0.0000 0.0000 0.0000

    2 -0.7334 2.9779 0.0000 0.0000 0.0000 0.0000

    3 -1.1100 4.5222 0.0000 0.0000 0.0000 0.0000

    62 1 -0.3278 1.7662 0.0000 0.0000 0.0000 0.0000

    2 -0.6414 3.4092 0.0000 0.0000 0.0000 0.0000

    3 -0.9693 5.1754 0.0000 0.0000 0.0000 0.0000

    63 1 -0.2499 2.0082 0.0000 0.0000 0.0000 0.0000

    2 -0.4938 3.8686 0.0000 0.0000 0.0000 0.0000

    3 -0.7437 5.8767 0.0000 0.0000 0.0000 0.0000

    64 1 -0.1720 2.1398 0.0000 0.0000 0.0000 0.0000

    2 -0.3462 4.1267 0.0000 0.0000 0.0000 0.0000

    3 -0.5182 6.2665 0.0000 0.0000 0.0000 0.0000

    65 1 -0.0453 2.3008 0.0000 0.0000 0.0000 0.0000

    2 -0.1054 4.4283 0.0000 0.0000 0.0000 0.0000

    3 -0.1507 6.7291 0.0000 0.0000 0.0000 0.0000

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 9

    JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = SPACE

    ------------------

    JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN

    66 1 0.0814 2.2597 0.0000 0.0000 0.0000 0.0000

    2 0.1355 4.3519 0.0000 0.0000 0.0000 0.0000

    3 0.2169 6.6116 0.0000 0.0000 0.0000 0.0000

    67 1 0.2997 2.2361 0.0000 0.0000 0.0000 0.0000

    2 0.5510 4.3048 0.0000 0.0000 0.0000 0.0000

    3 0.8508 6.5409 0.0000 0.0000 0.0000 0.0000

    68 1 0.5181 1.8366 0.0000 0.0000 0.0000 0.0000

    2 0.9666 3.5517 0.0000 0.0000 0.0000 0.0000

    3 1.4847 5.3883 0.0000 0.0000 0.0000 0.0000

    69 1 0.7434 1.4775 0.0000 0.0000 0.0000 0.0000

    2 1.3967 2.8611 0.0000 0.0000 0.0000 0.0000

    3 2.1401 4.3386 0.0000 0.0000 0.0000 0.0000

    70 1 0.9688 0.7276 0.0000 0.0000 0.0000 0.0000

    2 1.8267 1.4199 0.0000 0.0000 0.0000 0.0000

    3 2.7955 2.1475 0.0000 0.0000 0.0000 0.0000

    71 1 1.1248 -0.1008 0.0000 0.0000 0.0000 0.0000

    2 2.1240 -0.1746 0.0000 0.0000 0.0000 0.0000

    3 3.2488 -0.2754 0.0000 0.0000 0.0000 0.0000

    72 1 1.2809 -1.5736 0.0000 0.0000 0.0000 0.0000

    2 2.4212 -2.9843 0.0000 0.0000 0.0000 0.0000

    3 3.7021 -4.5579 0.0000 0.0000 0.0000 0.0000

    73 1 1.5063 -3.1249 0.0000 0.0000 0.0000 0.0000

    2 2.8500 -5.9493 0.0000 0.0000 0.0000 0.0000

    3 4.3563 -9.0742 0.0000 0.0000 0.0000 0.0000

    74 1 1.7316 -5.0670 0.0000 0.0000 0.0000 0.0000

    2 3.2789 -9.6657 0.0000 0.0000 0.0000 0.0000

    3 5.0105 -14.7326 0.0000 0.0000 0.0000 0.0000

    75 1 1.9499 -6.9687 0.0000 0.0000 0.0000 0.0000

    2 3.6900 -13.3149 0.0000 0.0000 0.0000 0.0000

    3 5.6399 -20.2836 0.0000 0.0000 0.0000 0.0000

    76 1 2.1683 -9.2463 0.0000 0.0000 0.0000 0.0000

    2 4.1010 -17.6605 0.0000 0.0000 0.0000 0.0000

    3 6.2693 -26.9068 0.0000 0.0000 0.0000 0.0000

    77 1 2.2950 -11.5064 0.0000 0.0000 0.0000 0.0000

    2 4.3362 -21.9932 0.0000 0.0000 0.0000 0.0000

    3 6.6312 -33.4996 0.0000 0.0000 0.0000 0.0000

    78 1 2.4216 -13.9686 0.0000 0.0000 0.0000 0.0000

    2 4.5714 -26.6984 0.0000 0.0000 0.0000 0.0000

    3 6.9931 -40.6670 0.0000 0.0000 0.0000 0.0000

    79 1 2.4996 -16.4014 0.0000 0.0000 0.0000 0.0000

    2 4.7107 -31.3415 0.0000 0.0000 0.0000 0.0000

    3 7.2103 -47.7429 0.0000 0.0000 0.0000 0.0000

    80 1 2.5775 -18.9447 0.0000 0.0000 0.0000 0.0000

    2 4.8500 -36.1689 0.0000 0.0000 0.0000 0.0000

    3 7.4276 -55.1136 0.0000 0.0000 0.0000 0.0000

    81 1 2.6264 -21.4677 0.0000 0.0000 0.0000 0.0000

    2 4.9304 -40.9982 0.0000 0.0000 0.0000 0.0000

    3 7.5567 -62.4660 0.0000 0.0000 0.0000 0.0000

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 10

    JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = SPACE

    ------------------

    JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN

    82 1 2.6752 -24.0497 0.0000 0.0000 0.0000 0.0000

    2 5.0107 -45.9151 0.0000 0.0000 0.0000 0.0000

    3 7.6859 -69.9648 0.0000 0.0000 0.0000 0.0000

    83 1 2.7036 -26.5996 0.0000 0.0000 0.0000 0.0000

    2 5.0441 -50.7394 0.0000 0.0000 0.0000 0.0000

    3 7.7478 -77.3390 0.0000 0.0000 0.0000 0.0000

    84 1 2.7321 -29.1759 0.0000 0.0000 0.0000 0.0000

    2 5.0776 -55.5342 0.0000 0.0000 0.0000 0.0000

    3 7.8097 -84.7101 0.0000 0.0000 0.0000 0.0000

    85 1 2.7385 -31.7332 0.0000 0.0000 0.0000 0.0000

    2 5.0797 -60.3637 0.0000 0.0000 0.0000 0.0000

    3 7.8182 -92.0969 0.0000 0.0000 0.0000 0.0000

    86 1 2.7449 -34.2784 0.0000 0.0000 0.0000 0.0000

    2 5.0819 -65.1397 0.0000 0.0000 0.0000 0.0000

    3 7.8268 -99.4181 0.0000 0.0000 0.0000 0.0000

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 11

    SUPPORT REACTIONS -UNIT KG MMS STRUCTURE TYPE = SPACE

    -----------------

    JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM Z

    1 1 0.00 0.00 0.00 0.00 0.00 0.00

    2 0.00 -7976.24 0.00 0.00 0.00 0.00

    3 0.00 -7976.23 0.00 0.00 0.00 0.00

    18 1 0.00 235354.48 0.00 0.00 0.00 0.00

    2 0.00 416246.25 0.00 0.00 0.00 0.00

    3 0.00 651600.75 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 12

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    1 1 1 0.00 945.88 0.00 0.00 0.00 0.00

    2 0.00 945.88 0.00 0.00 0.00 0.00

    2 1 0.00 0.00 0.00 0.00 0.00 0.00

    2 0.00 0.00 0.00 0.00 0.00 0.00

    3 1 0.00 945.88 0.00 0.00 0.00 0.00

    2 0.00 945.88 0.00 0.00 0.00 0.00

    2 1 2 9154.41 945.88 0.00 0.00 0.00 0.00

    3 -9154.41 945.88 0.00 0.00 0.00 0.00

    2 2 21648.42 0.00 0.00 0.00 0.00 0.00

    3 -21648.42 0.00 0.00 0.00 0.00 0.00

    3 2 30802.83 945.88 0.00 0.00 0.00 0.00

    3 -30802.83 945.88 0.00 0.00 0.00 0.00

    3 1 3 9154.41 945.88 0.00 0.00 0.00 0.00

    4 -9154.41 945.88 0.00 0.00 0.00 0.00

    2 3 21648.42 0.00 0.00 0.00 0.00 0.00

    4 -21648.42 0.00 0.00 0.00 0.00 0.00

    3 3 30802.83 945.88 0.00 0.00 0.00 0.00

    4 -30802.83 945.88 0.00 0.00 0.00 0.00

    5 1 6 31884.02 1049.48 0.00 0.00 0.00 0.00

    7 -31884.02 1049.48 0.00 0.00 0.00 0.00

    2 6 64324.40 0.00 0.00 0.00 0.00 0.00

    7 -64324.40 0.00 0.00 0.00 0.00 0.00

    3 6 96208.42 1049.48 0.00 0.00 0.00 0.00

    7 -96208.42 1049.48 0.00 0.00 0.00 0.00

    6 1 7 66126.52 1225.15 0.00 0.00 0.00 0.00

    8 -66126.52 1225.15 0.00 0.00 0.00 0.00

    2 7 129355.09 0.00 0.00 0.00 0.00 0.00

    8-129355.09 0.00 0.00 0.00 0.00 0.00

    3 7 195481.62 1225.15 0.00 0.00 0.00 0.00

    8-195481.62 1225.15 0.00 0.00 0.00 0.00

    7 1 8 66126.52 1225.15 0.00 0.00 0.00 0.00

    9 -66126.52 1225.15 0.00 0.00 0.00 0.00

    2 8 129355.09 0.00 0.00 0.00 0.00 0.00

    9-129355.09 0.00 0.00 0.00 0.00 0.00

    3 8 195481.62 1225.15 0.00 0.00 0.00 0.00

    9-195481.62 1225.15 0.00 0.00 0.00 0.00

    8 1 9 112523.38 1279.20 0.00 0.00 0.00 0.00

    10-112523.38 1279.20 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 13

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 9 218546.28 0.00 0.00 0.00 0.00 0.00

    10-218546.28 0.00 0.00 0.00 0.00 0.00

    3 9 331069.66 1279.20 0.00 0.00 0.00 0.00

    10-331069.66 1279.20 0.00 0.00 0.00 0.00

    9 1 10 112523.38 1279.20 0.00 0.00 0.00 0.00

    11-112523.38 1279.20 0.00 0.00 0.00 0.00

    2 10 218546.28 0.00 0.00 0.00 0.00 0.00

    11-218546.28 0.00 0.00 0.00 0.00 0.00

    3 10 331069.66 1279.20 0.00 0.00 0.00 0.00

    11-331069.66 1279.20 0.00 0.00 0.00 0.00

    10 1 11 171099.38 1225.15 0.00 0.00 0.00 0.00

    12-171099.38 1225.15 0.00 0.00 0.00 0.00

    2 11 330092.19 0.00 0.00 0.00 0.00 0.00

    12-330092.19 0.00 0.00 0.00 0.00 0.00

    3 11 501191.56 1225.15 0.00 0.00 0.00 0.00

    12-501191.56 1225.15 0.00 0.00 0.00 0.00

    11 1 12 171099.38 1225.15 0.00 0.00 0.00 0.00

    13-171099.38 1225.15 0.00 0.00 0.00 0.00

    2 12 330092.19 0.00 0.00 0.00 0.00 0.00

    13-330092.19 0.00 0.00 0.00 0.00 0.00

    3 12 501191.56 1225.15 0.00 0.00 0.00 0.00

    13-501191.56 1225.15 0.00 0.00 0.00 0.00

    12 1 13 241829.72 1049.48 0.00 0.00 0.00 0.00

    14-241829.72 1049.48 0.00 0.00 0.00 0.00

    2 13 465798.56 0.00 0.00 0.00 0.00 0.00

    14-465798.56 0.00 0.00 0.00 0.00 0.00

    3 13 707628.25 1049.48 0.00 0.00 0.00 0.00

    14-707628.25 1049.48 0.00 0.00 0.00 0.00

    13 1 14 241829.72 1049.48 0.00 0.00 0.00 0.00

    15-241829.72 1049.48 0.00 0.00 0.00 0.00

    2 14 465798.56 0.00 0.00 0.00 0.00 0.00

    15-465798.56 0.00 0.00 0.00 0.00 0.00

    3 14 707628.25 1049.48 0.00 0.00 0.00 0.00

    15-707628.25 1049.48 0.00 0.00 0.00 0.00

    14 1 15 324072.97 945.88 0.00 0.00 0.00 0.00

    16-324072.97 945.88 0.00 0.00 0.00 0.00

    2 15 623859.62 0.00 0.00 0.00 0.00 0.00

    16-623859.62 0.00 0.00 0.00 0.00 0.00

    3 15 947932.56 945.88 0.00 0.00 0.00 0.00

    16-947932.56 945.88 0.00 0.00 0.00 0.00

    15 1 16 324072.97 945.89 0.00 0.00 0.00 0.00

    17-324072.97 945.89 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 14

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 16 623859.62 0.00 0.00 0.00 0.00 0.00

    17-623859.62 0.00 0.00 0.00 0.00 0.00

    3 16 947932.56 945.89 0.00 0.00 0.00 0.00

    17-947932.56 945.89 0.00 0.00 0.00 0.00

    16 1 17 409191.94 945.88 0.00 0.00 0.00 0.00

    18-409191.94 945.88 0.00 0.00 0.00 0.00

    2 17 782857.31 0.00 0.00 0.00 0.00 0.00

    18-782857.31 0.00 0.00 0.00 0.00 0.00

    3 171192049.12 945.88 0.00 0.00 0.00 0.00

    18********** 945.88 0.00 0.00 0.00 0.00

    17 1 18 409191.94 945.88 0.00 0.00 0.00 0.00

    19-409191.94 945.88 0.00 0.00 0.00 0.00

    2 18 782857.31 0.00 0.00 0.00 0.00 0.00

    19-782857.31 0.00 0.00 0.00 0.00 0.00

    3 181192049.12 945.88 0.00 0.00 0.00 0.00

    19********** 945.88 0.00 0.00 0.00 0.00

    18 1 19 324073.00 945.88 0.00 0.00 0.00 0.00

    20-324073.00 945.88 0.00 0.00 0.00 0.00

    2 19 621417.44 0.00 0.00 0.00 0.00 0.00

    20-621417.44 0.00 0.00 0.00 0.00 0.00

    3 19 945490.50 945.88 0.00 0.00 0.00 0.00

    20-945490.50 945.88 0.00 0.00 0.00 0.00

    19 1 20 324073.00 945.88 0.00 0.00 0.00 0.00

    21-324073.00 945.88 0.00 0.00 0.00 0.00

    2 20 621417.44 0.00 0.00 0.00 0.00 0.00

    21-621417.44 0.00 0.00 0.00 0.00 0.00

    3 20 945490.50 945.88 0.00 0.00 0.00 0.00

    21-945490.50 945.88 0.00 0.00 0.00 0.00

    20 1 21 241829.77 1049.48 0.00 0.00 0.00 0.00

    22-241829.77 1049.48 0.00 0.00 0.00 0.00

    2 21 461247.75 0.00 0.00 0.00 0.00 0.00

    22-461247.75 0.00 0.00 0.00 0.00 0.00

    3 21 703077.50 1049.48 0.00 0.00 0.00 0.00

    22-703077.50 1049.48 0.00 0.00 0.00 0.00

    21 1 22 241829.77 1049.48 0.00 0.00 0.00 0.00

    23-241829.77 1049.48 0.00 0.00 0.00 0.00

    2 22 461247.75 0.00 0.00 0.00 0.00 0.00

    23-461247.75 0.00 0.00 0.00 0.00 0.00

    3 22 703077.50 1049.48 0.00 0.00 0.00 0.00

    23-703077.50 1049.48 0.00 0.00 0.00 0.00

    22 1 23 171099.41 1225.15 0.00 0.00 0.00 0.00

    24-171099.41 1225.15 0.00 0.00 0.00 0.00

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    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 23 321791.84 0.00 0.00 0.00 0.00 0.00

    24-321791.84 0.00 0.00 0.00 0.00 0.00

    3 23 492891.25 1225.15 0.00 0.00 0.00 0.00

    24-492891.25 1225.15 0.00 0.00 0.00 0.00

    23 1 24 171099.41 1225.15 0.00 0.00 0.00 0.00

    25-171099.41 1225.15 0.00 0.00 0.00 0.00

    2 24 321791.84 0.00 0.00 0.00 0.00 0.00

    25-321791.84 0.00 0.00 0.00 0.00 0.00

    3 24 492891.25 1225.15 0.00 0.00 0.00 0.00

    25-492891.25 1225.15 0.00 0.00 0.00 0.00

    24 1 25 112523.41 1279.20 0.00 0.00 0.00 0.00

    26-112523.41 1279.20 0.00 0.00 0.00 0.00

    2 25 207033.36 0.00 0.00 0.00 0.00 0.00

    26-207033.36 0.00 0.00 0.00 0.00 0.00

    3 25 319556.78 1279.20 0.00 0.00 0.00 0.00

    26-319556.78 1279.20 0.00 0.00 0.00 0.00

    25 1 26 112523.41 1279.20 0.00 0.00 0.00 0.00

    27-112523.41 1279.20 0.00 0.00 0.00 0.00

    2 26 207033.36 0.00 0.00 0.00 0.00 0.00

    27-207033.36 0.00 0.00 0.00 0.00 0.00

    3 26 319556.78 1279.20 0.00 0.00 0.00 0.00

    27-319556.78 1279.20 0.00 0.00 0.00 0.00

    26 1 27 66126.55 1225.15 0.00 0.00 0.00 0.00

    28 -66126.55 1225.15 0.00 0.00 0.00 0.00

    2 27 112988.66 0.00 0.00 0.00 0.00 0.00

    28-112988.66 0.00 0.00 0.00 0.00 0.00

    3 27 179115.22 1225.15 0.00 0.00 0.00 0.00

    28-179115.22 1225.15 0.00 0.00 0.00 0.00

    27 1 28 66126.55 1225.15 0.00 0.00 0.00 0.00

    29 -66126.55 1225.15 0.00 0.00 0.00 0.00

    2 28 112988.66 0.00 0.00 0.00 0.00 0.00

    29-112988.66 0.00 0.00 0.00 0.00 0.00

    3 28 179115.22 1225.15 0.00 0.00 0.00 0.00

    29-179115.22 1225.15 0.00 0.00 0.00 0.00

    28 1 29 31884.05 1049.48 0.00 0.00 0.00 0.00

    30 -31884.05 1049.48 0.00 0.00 0.00 0.00

    2 29 45692.97 0.00 0.00 0.00 0.00 0.00

    30 -45692.97 0.00 0.00 0.00 0.00 0.00

    3 29 77577.02 1049.48 0.00 0.00 0.00 0.00

    30 -77577.02 1049.48 0.00 0.00 0.00 0.00

    29 1 30 31884.05 1049.48 0.00 0.00 0.00 0.00

    31 -31884.05 1049.48 0.00 0.00 0.00 0.00

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    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 30 45692.97 0.00 0.00 0.00 0.00 0.00

    31 -45692.97 0.00 0.00 0.00 0.00 0.00

    3 30 77577.02 1049.48 0.00 0.00 0.00 0.00

    31 -77577.02 1049.48 0.00 0.00 0.00 0.00

    30 1 31 9154.41 945.89 0.00 0.00 0.00 0.00

    32 -9154.41 945.89 0.00 0.00 0.00 0.00

    2 31 13831.06 0.00 0.00 0.00 0.00 0.00

    32 -13831.06 0.00 0.00 0.00 0.00 0.00

    3 31 22985.47 945.89 0.00 0.00 0.00 0.00

    32 -22985.47 945.89 0.00 0.00 0.00 0.00

    31 1 32 9154.41 945.88 0.00 0.00 0.00 0.00

    33 -9154.41 945.88 0.00 0.00 0.00 0.00

    2 32 13831.06 0.00 0.00 0.00 0.00 0.00

    33 -13831.06 0.00 0.00 0.00 0.00 0.00

    3 32 22985.47 945.88 0.00 0.00 0.00 0.00

    33 -22985.47 945.88 0.00 0.00 0.00 0.00

    32 1 33 0.00 945.88 0.00 0.00 0.00 0.00

    34 0.00 945.88 0.00 0.00 0.00 0.00

    2 33 0.00 0.00 0.00 0.00 0.00 0.00

    34 0.00 0.00 0.00 0.00 0.00 0.00

    3 33 0.00 945.88 0.00 0.00 0.00 0.00

    34 0.00 945.88 0.00 0.00 0.00 0.00

    33 1 1 -945.88 0.00 0.00 0.00 0.00 0.00

    35 4382.79 0.00 0.00 0.00 0.00 0.00

    2 1 -14296.24 0.00 0.00 0.00 0.00 0.00

    35 14296.24 0.00 0.00 0.00 0.00 0.00

    3 1 -15242.12 0.00 0.00 0.00 0.00 0.00

    35 18679.03 0.00 0.00 0.00 0.00 0.00

    34 1 2 257.67 0.00 0.00 0.00 0.00 0.00

    36 295.56 0.00 0.00 0.00 0.00 0.00

    2 2 -3405.34 0.00 0.00 0.00 0.00 0.00

    36 3405.34 0.00 0.00 0.00 0.00 0.00

    3 2 -3147.67 0.00 0.00 0.00 0.00 0.00

    36 3700.91 0.00 0.00 0.00 0.00 0.00

    35 1 3 -1891.77 0.00 0.00 0.00 0.00 0.00

    37 2445.00 0.00 0.00 0.00 0.00 0.00

    2 3 -12640.00 0.00 0.00 0.00 0.00 0.00

    37 12640.00 0.00 0.00 0.00 0.00 0.00

    3 3 -14531.77 0.00 0.00 0.00 0.00 0.00

    37 15085.00 0.00 0.00 0.00 0.00 0.00

    36 1 6 -2098.96 0.00 0.00 0.00 0.00 0.00

    38 2652.20 0.00 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 17

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 6 -12640.00 0.00 0.00 0.00 0.00 0.00

    38 12640.00 0.00 0.00 0.00 0.00 0.00

    3 6 -14738.96 0.00 0.00 0.00 0.00 0.00

    38 15292.20 0.00 0.00 0.00 0.00 0.00

    37 1 8 -2450.29 0.00 0.00 0.00 0.00 0.00

    39 3003.53 0.00 0.00 0.00 0.00 0.00

    2 8 -12640.00 0.00 0.00 0.00 0.00 0.00

    39 12640.00 0.00 0.00 0.00 0.00 0.00

    3 8 -15090.29 0.00 0.00 0.00 0.00 0.00

    39 15643.52 0.00 0.00 0.00 0.00 0.00

    38 1 10 -2558.39 0.00 0.00 0.00 0.00 0.00

    40 3111.63 0.00 0.00 0.00 0.00 0.00

    2 10 -12640.00 0.00 0.00 0.00 0.00 0.00

    40 12640.00 0.00 0.00 0.00 0.00 0.00

    3 10 -15198.39 0.00 0.00 0.00 0.00 0.00

    40 15751.63 0.00 0.00 0.00 0.00 0.00

    39 1 12 -2450.29 0.00 0.00 0.00 0.00 0.00

    41 3003.53 0.00 0.00 0.00 0.00 0.00

    2 12 -12640.00 0.00 0.00 0.00 0.00 0.00

    41 12640.00 0.00 0.00 0.00 0.00 0.00

    3 12 -15090.29 0.00 0.00 0.00 0.00 0.00

    41 15643.52 0.00 0.00 0.00 0.00 0.00

    40 1 14 -2098.96 0.00 0.00 0.00 0.00 0.00

    42 2652.20 0.00 0.00 0.00 0.00 0.00

    2 14 -12640.00 0.00 0.00 0.00 0.00 0.00

    42 12640.00 0.00 0.00 0.00 0.00 0.00

    3 14 -14738.96 0.00 0.00 0.00 0.00 0.00

    42 15292.20 0.00 0.00 0.00 0.00 0.00

    41 1 16 -1891.77 0.00 0.00 0.00 0.00 0.00

    43 2445.00 0.00 0.00 0.00 0.00 0.00

    2 16 -12640.00 0.00 0.00 0.00 0.00 0.00

    43 12640.00 0.00 0.00 0.00 0.00 0.00

    3 16 -14531.77 0.00 0.00 0.00 0.00 0.00

    43 15085.00 0.00 0.00 0.00 0.00 0.00

    42 1 17 -11372.23 0.00 0.00 0.00 0.00 0.00

    44 11925.46 0.00 0.00 0.00 0.00 0.00

    2 17 -25243.48 0.00 0.00 0.00 0.00 0.00

    44 25243.48 0.00 0.00 0.00 0.00 0.00

    3 17 -36615.71 0.00 0.00 0.00 0.00 0.00

    44 37168.94 0.00 0.00 0.00 0.00 0.00

    43 1 18 233462.70 0.00 0.00 0.00 0.00 0.00

    45-230025.80 0.00 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 18

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 18 409926.25 0.00 0.00 0.00 0.00 0.00

    45-409926.25 0.00 0.00 0.00 0.00 0.00

    3 18 643388.94 0.00 0.00 0.00 0.00 0.00

    45-639952.06 0.00 0.00 0.00 0.00 0.00

    44 1 19 -11372.23 0.00 0.00 0.00 0.00 0.00

    46 11925.46 0.00 0.00 0.00 0.00 0.00

    2 19 -25464.38 0.00 0.00 0.00 0.00 0.00

    46 25464.38 0.00 0.00 0.00 0.00 0.00

    3 19 -36836.61 0.00 0.00 0.00 0.00 0.00

    46 37389.84 0.00 0.00 0.00 0.00 0.00

    45 1 20 -1891.77 0.00 0.00 0.00 0.00 0.00

    47 2445.00 0.00 0.00 0.00 0.00 0.00

    2 20 -12340.00 0.00 0.00 0.00 0.00 0.00

    47 12340.00 0.00 0.00 0.00 0.00 0.00

    3 20 -14231.77 0.00 0.00 0.00 0.00 0.00

    47 14785.00 0.00 0.00 0.00 0.00 0.00

    46 1 22 -2098.96 0.00 0.00 0.00 0.00 0.00

    48 2652.20 0.00 0.00 0.00 0.00 0.00

    2 22 -12340.00 0.00 0.00 0.00 0.00 0.00

    48 12340.00 0.00 0.00 0.00 0.00 0.00

    3 22 -14438.96 0.00 0.00 0.00 0.00 0.00

    48 14992.20 0.00 0.00 0.00 0.00 0.00

    47 1 24 -2450.29 0.00 0.00 0.00 0.00 0.00

    49 3003.53 0.00 0.00 0.00 0.00 0.00

    2 24 -12340.00 0.00 0.00 0.00 0.00 0.00

    49 12340.00 0.00 0.00 0.00 0.00 0.00

    3 24 -14790.29 0.00 0.00 0.00 0.00 0.00

    49 15343.53 0.00 0.00 0.00 0.00 0.00

    48 1 26 -2558.39 0.00 0.00 0.00 0.00 0.00

    50 3111.63 0.00 0.00 0.00 0.00 0.00

    2 26 -12340.00 0.00 0.00 0.00 0.00 0.00

    50 12340.00 0.00 0.00 0.00 0.00 0.00

    3 26 -14898.39 0.00 0.00 0.00 0.00 0.00

    50 15451.63 0.00 0.00 0.00 0.00 0.00

    49 1 28 -2450.29 0.00 0.00 0.00 0.00 0.00

    51 3003.53 0.00 0.00 0.00 0.00 0.00

    2 28 -12340.00 0.00 0.00 0.00 0.00 0.00

    51 12340.00 0.00 0.00 0.00 0.00 0.00

    3 28 -14790.29 0.00 0.00 0.00 0.00 0.00

    51 15343.53 0.00 0.00 0.00 0.00 0.00

    50 1 30 -2098.96 0.00 0.00 0.00 0.00 0.00

    52 2652.20 0.00 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 19

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 30 -21800.00 0.00 0.00 0.00 0.00 0.00

    52 21800.00 0.00 0.00 0.00 0.00 0.00

    3 30 -23898.96 0.00 0.00 0.00 0.00 0.00

    52 24452.20 0.00 0.00 0.00 0.00 0.00

    51 1 32 -1891.77 0.00 0.00 0.00 0.00 0.00

    53 2445.00 0.00 0.00 0.00 0.00 0.00

    2 32 -11120.00 0.00 0.00 0.00 0.00 0.00

    53 11120.00 0.00 0.00 0.00 0.00 0.00

    3 32 -13011.77 0.00 0.00 0.00 0.00 0.00

    53 13565.00 0.00 0.00 0.00 0.00 0.00

    52 1 33 257.67 0.00 0.00 0.00 0.00 0.00

    54 295.56 0.00 0.00 0.00 0.00 0.00

    2 33 1003.76 0.00 0.00 0.00 0.00 0.00

    54 -1003.76 0.00 0.00 0.00 0.00 0.00

    3 33 1261.43 0.00 0.00 0.00 0.00 0.00

    54 -708.20 0.00 0.00 0.00 0.00 0.00

    53 1 34 -945.88 0.00 0.00 0.00 0.00 0.00

    55 4382.79 0.00 0.00 0.00 0.00 0.00

    2 34 -4410.00 0.00 0.00 0.00 0.00 0.00

    55 4410.00 0.00 0.00 0.00 0.00 0.00

    3 34 -5355.88 0.00 0.00 0.00 0.00 0.00

    55 8792.79 0.00 0.00 0.00 0.00 0.00

    54 1 36 -550.05 0.00 0.00 0.00 0.00 0.00

    56 1103.29 0.00 0.00 0.00 0.00 0.00

    2 36 -3405.34 0.00 0.00 0.00 0.00 0.00

    56 3405.34 0.00 0.00 0.00 0.00 0.00

    3 36 -3955.40 0.00 0.00 0.00 0.00 0.00

    56 4508.63 0.00 0.00 0.00 0.00 0.00

    55 1 35 -3604.37 628.61 0.00 0.00 0.00 0.00

    56 4970.91 628.61 0.00 0.00 0.00 0.00

    2 35 -9713.03 0.00 0.00 0.00 0.00 0.00

    56 9713.03 0.00 0.00 0.00 0.00 0.00

    3 35 -13317.40 628.61 0.00 0.00 0.00 0.00

    56 14683.94 628.61 0.00 0.00 0.00 0.00

    56 1 56 -9180.29 890.93 0.00 0.00 0.00 0.00

    57 9180.29 890.93 0.00 0.00 0.00 0.00

    2 56 -16285.45 0.00 0.00 0.00 0.00 0.00

    57 16285.45 0.00 0.00 0.00 0.00 0.00

    3 56 -25465.74 890.93 0.00 0.00 0.00 0.00

    57 25465.74 890.93 0.00 0.00 0.00 0.00

    57 1 57 -9180.29 890.93 0.00 0.00 0.00 0.00

    58 9180.29 890.93 0.00 0.00 0.00 0.00

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    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 57 -16285.45 0.00 0.00 0.00 0.00 0.00

    58 16285.45 0.00 0.00 0.00 0.00 0.00

    3 57 -25465.74 890.93 0.00 0.00 0.00 0.00

    58 25465.74 890.93 0.00 0.00 0.00 0.00

    58 1 58 -31472.27 685.00 0.00 0.00 0.00 0.00

    59 31472.27 685.00 0.00 0.00 0.00 0.00

    2 58 -58058.57 0.00 0.00 0.00 0.00 0.00

    59 58058.57 0.00 0.00 0.00 0.00 0.00

    3 58 -89530.83 685.00 0.00 0.00 0.00 0.00

    59 89530.83 685.00 0.00 0.00 0.00 0.00

    59 1 59 -31472.27 685.00 0.00 0.00 0.00 0.00

    60 31472.27 685.00 0.00 0.00 0.00 0.00

    2 59 -58058.57 0.00 0.00 0.00 0.00 0.00

    60 58058.57 0.00 0.00 0.00 0.00 0.00

    3 59 -89530.83 685.00 0.00 0.00 0.00 0.00

    60 89530.83 685.00 0.00 0.00 0.00 0.00

    60 1 60 -65844.26 835.26 0.00 0.00 0.00 0.00

    61 65844.26 835.26 0.00 0.00 0.00 0.00

    2 60-123992.12 0.00 0.00 0.00 0.00 0.00

    61 123992.12 0.00 0.00 0.00 0.00 0.00

    3 60-189836.39 835.26 0.00 0.00 0.00 0.00

    61 189836.39 835.26 0.00 0.00 0.00 0.00

    61 1 61 -65844.26 835.26 0.00 0.00 0.00 0.00

    62 65844.26 835.26 0.00 0.00 0.00 0.00

    2 61-123992.12 0.00 0.00 0.00 0.00 0.00

    62 123992.12 0.00 0.00 0.00 0.00 0.00

    3 61-189836.39 835.26 0.00 0.00 0.00 0.00

    62 189836.39 835.26 0.00 0.00 0.00 0.00

    62 1 62-112089.74 890.93 0.00 0.00 0.00 0.00

    63 112089.74 890.93 0.00 0.00 0.00 0.00

    2 62-212280.45 0.00 0.00 0.00 0.00 0.00

    63 212280.45 0.00 0.00 0.00 0.00 0.00

    3 62-324370.22 890.93 0.00 0.00 0.00 0.00

    63 324370.22 890.93 0.00 0.00 0.00 0.00

    63 1 63-112089.74 890.93 0.00 0.00 0.00 0.00

    64 112089.74 890.93 0.00 0.00 0.00 0.00

    2 63-212280.45 0.00 0.00 0.00 0.00 0.00

    64 212280.45 0.00 0.00 0.00 0.00 0.00

    3 63-324370.22 890.93 0.00 0.00 0.00 0.00

    64 324370.22 890.93 0.00 0.00 0.00 0.00

    64 1 64-170817.12 835.26 0.00 0.00 0.00 0.00

    65 170817.12 835.26 0.00 0.00 0.00 0.00

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    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 64-324729.22 0.00 0.00 0.00 0.00 0.00

    65 324729.22 0.00 0.00 0.00 0.00 0.00

    3 64-495546.34 835.26 0.00 0.00 0.00 0.00

    65 495546.34 835.26 0.00 0.00 0.00 0.00

    65 1 65-170817.12 835.26 0.00 0.00 0.00 0.00

    66 170817.12 835.26 0.00 0.00 0.00 0.00

    2 65-324729.22 0.00 0.00 0.00 0.00 0.00

    66 324729.22 0.00 0.00 0.00 0.00 0.00

    3 65-495546.34 835.26 0.00 0.00 0.00 0.00

    66 495546.34 835.26 0.00 0.00 0.00 0.00

    66 1 66-241417.95 685.00 0.00 0.00 0.00 0.00

    67 241417.95 685.00 0.00 0.00 0.00 0.00

    2 66-459532.72 0.00 0.00 0.00 0.00 0.00

    67 459532.72 0.00 0.00 0.00 0.00 0.00

    3 66-700950.69 685.00 0.00 0.00 0.00 0.00

    67 700950.69 685.00 0.00 0.00 0.00 0.00

    67 1 67-241417.95 685.00 0.00 0.00 0.00 0.00

    68 241417.95 685.00 0.00 0.00 0.00 0.00

    2 67-459532.72 0.00 0.00 0.00 0.00 0.00

    68 459532.72 0.00 0.00 0.00 0.00 0.00

    3 67-700950.69 685.00 0.00 0.00 0.00 0.00

    68 700950.69 685.00 0.00 0.00 0.00 0.00

    68 1 68-324098.84 890.93 0.00 0.00 0.00 0.00

    69 324098.84 890.93 0.00 0.00 0.00 0.00

    2 68-618496.69 0.00 0.00 0.00 0.00 0.00

    69 618496.69 0.00 0.00 0.00 0.00 0.00

    3 68-942595.50 890.93 0.00 0.00 0.00 0.00

    69 942595.50 890.93 0.00 0.00 0.00 0.00

    69 1 69-324098.84 890.93 0.00 0.00 0.00 0.00

    70 324098.84 890.93 0.00 0.00 0.00 0.00

    2 69-618496.69 0.00 0.00 0.00 0.00 0.00

    70 618496.69 0.00 0.00 0.00 0.00 0.00

    3 69-942595.50 890.93 0.00 0.00 0.00 0.00

    70 942595.50 890.93 0.00 0.00 0.00 0.00

    70 1 70-432168.94 1715.20 0.00 0.00 0.00 0.00

    71 432168.94 1715.20 0.00 0.00 0.00 0.00

    2 70-823039.44 0.00 0.00 0.00 0.00 0.00

    71 823039.44 0.00 0.00 0.00 0.00 0.00

    3 70********** 1715.20 0.00 0.00 0.00 0.00

    711255208.38 1715.20 0.00 0.00 0.00 0.00

    71 1 71-432168.94 1715.20 0.00 0.00 0.00 0.00

    72 432168.94 1715.20 0.00 0.00 0.00 0.00

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    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 71-823039.44 0.00 0.00 0.00 0.00 0.00

    72 823039.44 0.00 0.00 0.00 0.00 0.00

    3 71********** 1715.20 0.00 0.00 0.00 0.00

    721255208.38 1715.20 0.00 0.00 0.00 0.00

    72 1 72-324098.88 890.93 0.00 0.00 0.00 0.00

    73 324098.88 890.93 0.00 0.00 0.00 0.00

    2 72-616736.94 0.00 0.00 0.00 0.00 0.00

    73 616736.94 0.00 0.00 0.00 0.00 0.00

    3 72-940835.88 890.93 0.00 0.00 0.00 0.00

    73 940835.88 890.93 0.00 0.00 0.00 0.00

    73 1 73-324098.88 890.93 0.00 0.00 0.00 0.00

    74 324098.88 890.93 0.00 0.00 0.00 0.00

    2 73-616736.94 0.00 0.00 0.00 0.00 0.00

    74 616736.94 0.00 0.00 0.00 0.00 0.00

    3 73-940835.88 890.93 0.00 0.00 0.00 0.00

    74 940835.88 890.93 0.00 0.00 0.00 0.00

    74 1 74-241418.02 685.00 0.00 0.00 0.00 0.00

    75 241418.02 685.00 0.00 0.00 0.00 0.00

    2 74-454575.44 0.00 0.00 0.00 0.00 0.00

    75 454575.44 0.00 0.00 0.00 0.00 0.00

    3 74-695993.44 685.00 0.00 0.00 0.00 0.00

    75 695993.44 685.00 0.00 0.00 0.00 0.00

    75 1 75-241418.02 685.00 0.00 0.00 0.00 0.00

    76 241418.02 685.00 0.00 0.00 0.00 0.00

    2 75-454575.44 0.00 0.00 0.00 0.00 0.00

    76 454575.44 0.00 0.00 0.00 0.00 0.00

    3 75-695993.44 685.00 0.00 0.00 0.00 0.00

    76 695993.44 685.00 0.00 0.00 0.00 0.00

    76 1 76-170817.14 835.26 0.00 0.00 0.00 0.00

    77 170817.14 835.26 0.00 0.00 0.00 0.00

    2 76-317111.34 0.00 0.00 0.00 0.00 0.00

    77 317111.34 0.00 0.00 0.00 0.00 0.00

    3 76-487928.53 835.26 0.00 0.00 0.00 0.00

    77 487928.53 835.26 0.00 0.00 0.00 0.00

    77 1 77-170817.14 835.26 0.00 0.00 0.00 0.00

    78 170817.14 835.26 0.00 0.00 0.00 0.00

    2 77-317111.34 0.00 0.00 0.00 0.00 0.00

    78 317111.34 0.00 0.00 0.00 0.00 0.00

    3 77-487928.53 835.26 0.00 0.00 0.00 0.00

    78 487928.53 835.26 0.00 0.00 0.00 0.00

    78 1 78-112089.77 890.93 0.00 0.00 0.00 0.00

    79 112089.77 890.93 0.00 0.00 0.00 0.00

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    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 78-200361.06 0.00 0.00 0.00 0.00 0.00

    79 200361.06 0.00 0.00 0.00 0.00 0.00

    3 78-312450.84 890.93 0.00 0.00 0.00 0.00

    79 312450.84 890.93 0.00 0.00 0.00 0.00

    79 1 79-112089.77 890.93 0.00 0.00 0.00 0.00

    80 112089.77 890.93 0.00 0.00 0.00 0.00

    2 79-200361.06 0.00 0.00 0.00 0.00 0.00

    80 200361.06 0.00 0.00 0.00 0.00 0.00

    3 79-312450.84 890.93 0.00 0.00 0.00 0.00

    80 312450.84 890.93 0.00 0.00 0.00 0.00

    80 1 80 -65844.30 835.26 0.00 0.00 0.00 0.00

    81 65844.30 835.26 0.00 0.00 0.00 0.00

    2 80-108308.16 0.00 0.00 0.00 0.00 0.00

    81 108308.16 0.00 0.00 0.00 0.00 0.00

    3 80-174152.45 835.26 0.00 0.00 0.00 0.00

    81 174152.45 835.26 0.00 0.00 0.00 0.00

    81 1 81 -65844.30 835.26 0.00 0.00 0.00 0.00

    82 65844.30 835.26 0.00 0.00 0.00 0.00

    2 81-108308.16 0.00 0.00 0.00 0.00 0.00

    82 108308.16 0.00 0.00 0.00 0.00 0.00

    3 81-174152.45 835.26 0.00 0.00 0.00 0.00

    82 174152.45 835.26 0.00 0.00 0.00 0.00

    82 1 82 -31472.29 685.00 0.00 0.00 0.00 0.00

    83 31472.29 685.00 0.00 0.00 0.00 0.00

    2 82 -36969.07 0.00 0.00 0.00 0.00 0.00

    83 36969.07 0.00 0.00 0.00 0.00 0.00

    3 82 -68441.36 685.00 0.00 0.00 0.00 0.00

    83 68441.36 685.00 0.00 0.00 0.00 0.00

    83 1 83 -31472.29 685.00 0.00 0.00 0.00 0.00

    84 31472.29 685.00 0.00 0.00 0.00 0.00

    2 83 -36969.07 0.00 0.00 0.00 0.00 0.00

    84 36969.07 0.00 0.00 0.00 0.00 0.00

    3 83 -68441.36 685.00 0.00 0.00 0.00 0.00

    84 68441.36 685.00 0.00 0.00 0.00 0.00

    84 1 84 -9180.29 890.93 0.00 0.00 0.00 0.00

    85 9180.29 890.93 0.00 0.00 0.00 0.00

    2 84 -3133.74 0.00 0.00 0.00 0.00 0.00

    85 3133.74 0.00 0.00 0.00 0.00 0.00

    3 84 -12314.03 890.93 0.00 0.00 0.00 0.00

    85 12314.03 890.93 0.00 0.00 0.00 0.00

    85 1 85 -9180.29 890.93 0.00 0.00 0.00 0.00

    86 9180.29 890.93 0.00 0.00 0.00 0.00

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    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 85 -3133.74 0.00 0.00 0.00 0.00 0.00

    86 3133.74 0.00 0.00 0.00 0.00 0.00

    3 85 -12314.03 890.93 0.00 0.00 0.00 0.00

    86 12314.03 890.93 0.00 0.00 0.00 0.00

    86 1 86 -4970.91 628.61 0.00 0.00 0.00 0.00

    55 3604.37 628.61 0.00 0.00 0.00 0.00

    2 86 -2996.20 0.00 0.00 0.00 0.00 0.00

    55 2996.20 0.00 0.00 0.00 0.00 0.00

    3 86 -7967.12 628.61 0.00 0.00 0.00 0.00

    55 6600.58 628.61 0.00 0.00 0.00 0.00

    87 1 35 3739.30 504.47 0.00 0.00 0.00 0.00

    2 -4835.98 504.47 0.00 0.00 0.00 0.00

    2 35 9713.03 0.00 0.00 0.00 0.00 0.00

    2 -9713.03 0.00 0.00 0.00 0.00 0.00

    3 35 13452.33 504.47 0.00 0.00 0.00 0.00

    2 -14549.01 504.47 0.00 0.00 0.00 0.00

    88 1 2 -8684.92 504.47 0.00 0.00 0.00 0.00

    37 9781.59 504.47 0.00 0.00 0.00 0.00

    2 2 -22261.29 0.00 0.00 0.00 0.00 0.00

    37 22261.29 0.00 0.00 0.00 0.00 0.00

    3 2 -30946.21 504.47 0.00 0.00 0.00 0.00

    37 32042.88 504.47 0.00 0.00 0.00 0.00

    89 1 37 13995.70 504.47 0.00 0.00 0.00 0.00

    4 -15092.38 504.47 0.00 0.00 0.00 0.00

    2 37 22928.05 0.00 0.00 0.00 0.00 0.00

    4 -22928.05 0.00 0.00 0.00 0.00 0.00

    3 37 36923.75 504.47 0.00 0.00 0.00 0.00

    4 -38020.42 504.47 0.00 0.00 0.00 0.00

    90 1 4 -18615.92 378.35 0.00 0.00 0.00 0.00

    38 19438.43 378.35 0.00 0.00 0.00 0.00

    2 4 -40103.57 0.00 0.00 0.00 0.00 0.00

    38 40103.57 0.00 0.00 0.00 0.00 0.00

    3 4 -58719.50 378.35 0.00 0.00 0.00 0.00

    38 59542.01 378.35 0.00 0.00 0.00 0.00

    91 1 38 22635.05 378.35 0.00 0.00 0.00 0.00

    7 -23457.56 378.35 0.00 0.00 0.00 0.00

    2 38 39436.81 0.00 0.00 0.00 0.00 0.00

    7 -39436.81 0.00 0.00 0.00 0.00 0.00

    3 38 62071.86 378.35 0.00 0.00 0.00 0.00

    7 -62894.38 378.35 0.00 0.00 0.00 0.00

    92 1 7 -27186.53 315.29 0.00 0.00 0.00 0.00

    39 27871.95 315.29 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 25

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 7 -56612.34 0.00 0.00 0.00 0.00 0.00

    39 56612.34 0.00 0.00 0.00 0.00 0.00

    3 7 -83798.87 315.29 0.00 0.00 0.00 0.00

    39 84484.29 315.29 0.00 0.00 0.00 0.00

    93 1 39 31586.67 315.29 0.00 0.00 0.00 0.00

    9 -32272.10 315.29 0.00 0.00 0.00 0.00

    2 39 57279.09 0.00 0.00 0.00 0.00 0.00

    9 -57279.09 0.00 0.00 0.00 0.00 0.00

    3 39 88865.77 315.29 0.00 0.00 0.00 0.00

    9 -89551.19 315.29 0.00 0.00 0.00 0.00

    94 1 9 -36255.20 315.29 0.00 0.00 0.00 0.00

    40 36940.62 315.29 0.00 0.00 0.00 0.00

    2 9 -74454.63 0.00 0.00 0.00 0.00 0.00

    40 74454.63 0.00 0.00 0.00 0.00 0.00

    3 9-110709.83 315.29 0.00 0.00 0.00 0.00

    40 111395.26 315.29 0.00 0.00 0.00 0.00

    95 1 40 40580.86 315.29 0.00 0.00 0.00 0.00

    11 -41266.29 315.29 0.00 0.00 0.00 0.00

    2 40 73787.86 0.00 0.00 0.00 0.00 0.00

    11 -73787.86 0.00 0.00 0.00 0.00 0.00

    3 40 114368.72 315.29 0.00 0.00 0.00 0.00

    11-115054.15 315.29 0.00 0.00 0.00 0.00

    96 1 11 -45249.38 315.29 0.00 0.00 0.00 0.00

    41 45934.81 315.29 0.00 0.00 0.00 0.00

    2 11 -90963.38 0.00 0.00 0.00 0.00 0.00

    41 90963.38 0.00 0.00 0.00 0.00 0.00

    3 11-136212.77 315.29 0.00 0.00 0.00 0.00

    41 136898.19 315.29 0.00 0.00 0.00 0.00

    97 1 41 49649.53 315.29 0.00 0.00 0.00 0.00

    13 -50334.96 315.29 0.00 0.00 0.00 0.00

    2 41 91630.15 0.00 0.00 0.00 0.00 0.00

    13 -91630.15 0.00 0.00 0.00 0.00 0.00

    3 41 141279.69 315.29 0.00 0.00 0.00 0.00

    13-141965.09 315.29 0.00 0.00 0.00 0.00

    98 1 13 -54063.93 378.35 0.00 0.00 0.00 0.00

    42 54886.43 378.35 0.00 0.00 0.00 0.00

    2 13-108805.66 0.00 0.00 0.00 0.00 0.00

    42 108805.66 0.00 0.00 0.00 0.00 0.00

    3 13-162869.59 378.35 0.00 0.00 0.00 0.00

    42 163692.09 378.35 0.00 0.00 0.00 0.00

    99 1 42 58083.05 378.35 0.00 0.00 0.00 0.00

    15 -58905.55 378.35 0.00 0.00 0.00 0.00

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    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 21 109899.91 0.00 0.00 0.00 0.00 0.00

    48-109899.91 0.00 0.00 0.00 0.00 0.00

    3 21 168805.47 378.35 0.00 0.00 0.00 0.00

    48-167982.97 378.35 0.00 0.00 0.00 0.00

    107 1 48 -54886.44 378.35 0.00 0.00 0.00 0.00

    23 54063.93 378.35 0.00 0.00 0.00 0.00

    2 48-111370.84 0.00 0.00 0.00 0.00 0.00

    23 111370.84 0.00 0.00 0.00 0.00 0.00

    3 48-166257.28 378.35 0.00 0.00 0.00 0.00

    23 165434.77 378.35 0.00 0.00 0.00 0.00

    108 1 23 50334.96 315.29 0.00 0.00 0.00 0.00

    49 -49649.54 315.29 0.00 0.00 0.00 0.00

    2 23 94602.95 0.00 0.00 0.00 0.00 0.00

    49 -94602.95 0.00 0.00 0.00 0.00 0.00

    3 23 144937.91 315.29 0.00 0.00 0.00 0.00

    49-144252.50 315.29 0.00 0.00 0.00 0.00

    109 1 49 -45934.81 315.29 0.00 0.00 0.00 0.00

    25 45249.39 315.29 0.00 0.00 0.00 0.00

    2 49 -93132.03 0.00 0.00 0.00 0.00 0.00

    25 93132.03 0.00 0.00 0.00 0.00 0.00

    3 49-139066.84 315.29 0.00 0.00 0.00 0.00

    25 138381.42 315.29 0.00 0.00 0.00 0.00

    110 1 25 41266.29 315.29 0.00 0.00 0.00 0.00

    50 -40580.87 315.29 0.00 0.00 0.00 0.00

    2 25 76364.16 0.00 0.00 0.00 0.00 0.00

    50 -76364.16 0.00 0.00 0.00 0.00 0.00

    3 25 117630.45 315.29 0.00 0.00 0.00 0.00

    50-116945.02 315.29 0.00 0.00 0.00 0.00

    111 1 50 -36940.62 315.29 0.00 0.00 0.00 0.00

    27 36255.20 315.29 0.00 0.00 0.00 0.00

    2 50 -77835.09 0.00 0.00 0.00 0.00 0.00

    27 77835.09 0.00 0.00 0.00 0.00 0.00

    3 50-114775.71 315.29 0.00 0.00 0.00 0.00

    27 114090.29 315.29 0.00 0.00 0.00 0.00

    112 1 27 32272.11 315.29 0.00 0.00 0.00 0.00

    51 -31586.68 315.29 0.00 0.00 0.00 0.00

    2 27 61067.21 0.00 0.00 0.00 0.00 0.00

    51 -61067.21 0.00 0.00 0.00 0.00 0.00

    3 27 93339.31 315.29 0.00 0.00 0.00 0.00

    51 -92653.88 315.29 0.00 0.00 0.00 0.00

    113 1 51 -27871.96 315.29 0.00 0.00 0.00 0.00

    29 27186.53 315.29 0.00 0.00 0.00 0.00

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    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 51 -59596.29 0.00 0.00 0.00 0.00 0.00

    29 59596.29 0.00 0.00 0.00 0.00 0.00

    3 51 -87468.24 315.29 0.00 0.00 0.00 0.00

    29 86782.82 315.29 0.00 0.00 0.00 0.00

    114 1 29 23457.56 378.35 0.00 0.00 0.00 0.00

    52 -22635.05 378.35 0.00 0.00 0.00 0.00

    2 29 39798.23 0.00 0.00 0.00 0.00 0.00

    52 -39798.23 0.00 0.00 0.00 0.00 0.00

    3 29 63255.79 378.35 0.00 0.00 0.00 0.00

    52 -62433.29 378.35 0.00 0.00 0.00 0.00

    115 1 52 -19438.44 378.35 0.00 0.00 0.00 0.00

    31 18615.93 378.35 0.00 0.00 0.00 0.00

    2 52 -37872.09 0.00 0.00 0.00 0.00 0.00

    31 37872.09 0.00 0.00 0.00 0.00 0.00

    3 52 -57310.54 378.35 0.00 0.00 0.00 0.00

    31 56488.02 378.35 0.00 0.00 0.00 0.00

    116 1 31 15092.39 504.47 0.00 0.00 0.00 0.00

    53 -13995.72 504.47 0.00 0.00 0.00 0.00

    2 31 9187.35 0.00 0.00 0.00 0.00 0.00

    53 -9187.35 0.00 0.00 0.00 0.00 0.00

    3 31 24279.74 504.47 0.00 0.00 0.00 0.00

    53 -23183.06 504.47 0.00 0.00 0.00 0.00

    117 1 53 -9781.59 504.47 0.00 0.00 0.00 0.00

    33 8684.92 504.47 0.00 0.00 0.00 0.00

    2 53 -17432.02 0.00 0.00 0.00 0.00 0.00

    33 17432.02 0.00 0.00 0.00 0.00 0.00

    3 53 -27213.61 504.47 0.00 0.00 0.00 0.00

    33 26116.93 504.47 0.00 0.00 0.00 0.00

    118 1 33 4835.98 504.47 0.00 0.00 0.00 0.00

    55 -3739.30 504.47 0.00 0.00 0.00 0.00

    2 33 2996.20 0.00 0.00 0.00 0.00 0.00

    55 -2996.20 0.00 0.00 0.00 0.00 0.00

    3 33 7832.19 504.47 0.00 0.00 0.00 0.00

    55 -6735.51 504.47 0.00 0.00 0.00 0.00

    119 1 37 2335.10 0.00 0.00 0.00 0.00 0.00

    57 -1781.87 0.00 0.00 0.00 0.00 0.00

    2 37 0.00 0.00 0.00 0.00 0.00 0.00

    57 0.00 0.00 0.00 0.00 0.00 0.00

    3 37 2335.10 0.00 0.00 0.00 0.00 0.00

    57 -1781.87 0.00 0.00 0.00 0.00 0.00

    120 1 38 1923.24 0.00 0.00 0.00 0.00 0.00

    59 -1370.00 0.00 0.00 0.00 0.00 0.00

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    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 45 0.00 0.00 0.00 0.00 0.00 0.00

    71 0.00 0.00 0.00 0.00 0.00 0.00

    3 45 7159.11 0.00 0.00 0.00 0.00 0.00

    71 -3430.41 0.00 0.00 0.00 0.00 0.00

    128 1 46 -12179.95 0.00 0.00 0.00 0.00 0.00

    72 12733.18 0.00 0.00 0.00 0.00 0.00

    2 46 -25464.38 0.00 0.00 0.00 0.00 0.00

    72 25464.38 0.00 0.00 0.00 0.00 0.00

    3 46 -37644.33 0.00 0.00 0.00 0.00 0.00

    72 38197.56 0.00 0.00 0.00 0.00 0.00

    129 1 47 2335.10 0.00 0.00 0.00 0.00 0.00

    73 -1781.87 0.00 0.00 0.00 0.00 0.00

    2 47 0.00 0.00 0.00 0.00 0.00 0.00

    73 0.00 0.00 0.00 0.00 0.00 0.00

    3 47 2335.10 0.00 0.00 0.00 0.00 0.00

    73 -1781.87 0.00 0.00 0.00 0.00 0.00

    130 1 48 1923.24 0.00 0.00 0.00 0.00 0.00

    75 -1370.00 0.00 0.00 0.00 0.00 0.00

    2 48 0.00 0.00 0.00 0.00 0.00 0.00

    75 0.00 0.00 0.00 0.00 0.00 0.00

    3 48 1923.24 0.00 0.00 0.00 0.00 0.00

    75 -1370.00 0.00 0.00 0.00 0.00 0.00

    131 1 49 2223.76 0.00 0.00 0.00 0.00 0.00

    77 -1670.52 0.00 0.00 0.00 0.00 0.00

    2 49 0.00 0.00 0.00 0.00 0.00 0.00

    77 0.00 0.00 0.00 0.00 0.00 0.00

    3 49 2223.76 0.00 0.00 0.00 0.00 0.00

    77 -1670.52 0.00 0.00 0.00 0.00 0.00

    132 1 50 2335.10 0.00 0.00 0.00 0.00 0.00

    79 -1781.87 0.00 0.00 0.00 0.00 0.00

    2 50 0.00 0.00 0.00 0.00 0.00 0.00

    79 0.00 0.00 0.00 0.00 0.00 0.00

    3 50 2335.10 0.00 0.00 0.00 0.00 0.00

    79 -1781.87 0.00 0.00 0.00 0.00 0.00

    133 1 51 2223.76 0.00 0.00 0.00 0.00 0.00

    81 -1670.52 0.00 0.00 0.00 0.00 0.00

    2 51 0.00 0.00 0.00 0.00 0.00 0.00

    81 0.00 0.00 0.00 0.00 0.00 0.00

    3 51 2223.76 0.00 0.00 0.00 0.00 0.00

    81 -1670.52 0.00 0.00 0.00 0.00 0.00

    134 1 52 1923.24 0.00 0.00 0.00 0.00 0.00

    83 -1370.00 0.00 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 31

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 52 0.00 0.00 0.00 0.00 0.00 0.00

    83 0.00 0.00 0.00 0.00 0.00 0.00

    3 52 1923.24 0.00 0.00 0.00 0.00 0.00

    83 -1370.00 0.00 0.00 0.00 0.00 0.00

    135 1 53 2335.10 0.00 0.00 0.00 0.00 0.00

    85 -1781.87 0.00 0.00 0.00 0.00 0.00

    2 53 0.00 0.00 0.00 0.00 0.00 0.00

    85 0.00 0.00 0.00 0.00 0.00 0.00

    3 53 2335.10 0.00 0.00 0.00 0.00 0.00

    85 -1781.87 0.00 0.00 0.00 0.00 0.00

    136 1 54 -550.05 0.00 0.00 0.00 0.00 0.00

    86 1103.29 0.00 0.00 0.00 0.00 0.00

    2 54 1003.76 0.00 0.00 0.00 0.00 0.00

    86 -1003.76 0.00 0.00 0.00 0.00 0.00

    3 54 453.71 0.00 0.00 0.00 0.00 0.00

    86 99.52 0.00 0.00 0.00 0.00 0.00

    137 1 35 0.00 254.49 0.00 0.00 0.00 0.00

    36 0.00 254.49 0.00 0.00 0.00 0.00

    2 35 0.00 0.00 0.00 0.00 0.00 0.00

    36 0.00 0.00 0.00 0.00 0.00 0.00

    3 35 0.00 254.49 0.00 0.00 0.00 0.00

    36 0.00 254.49 0.00 0.00 0.00 0.00

    138 1 56 8723.14 504.47 0.00 0.00 0.00 0.00

    37 -9819.81 504.47 0.00 0.00 0.00 0.00

    2 56 14340.29 0.00 0.00 0.00 0.00 0.00

    37 -14340.29 0.00 0.00 0.00 0.00 0.00

    3 56 23063.42 504.47 0.00 0.00 0.00 0.00

    37 -24160.10 504.47 0.00 0.00 0.00 0.00

    139 1 37 -13957.48 504.47 0.00 0.00 0.00 0.00

    58 15054.15 504.47 0.00 0.00 0.00 0.00

    2 37 -30849.05 0.00 0.00 0.00 0.00 0.00

    58 30849.05 0.00 0.00 0.00 0.00 0.00

    3 37 -44806.53 504.47 0.00 0.00 0.00 0.00

    58 45903.21 504.47 0.00 0.00 0.00 0.00

    140 1 58 18007.77 378.35 0.00 0.00 0.00 0.00

    38 -18830.28 378.35 0.00 0.00 0.00 0.00

    2 58 30849.06 0.00 0.00 0.00 0.00 0.00

    38 -30849.06 0.00 0.00 0.00 0.00 0.00

    3 58 48856.82 378.35 0.00 0.00 0.00 0.00

    38 -49679.34 378.35 0.00 0.00 0.00 0.00

    141 1 38 -23243.20 378.35 0.00 0.00 0.00 0.00

    60 24065.71 378.35 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 32

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 38 -48691.34 0.00 0.00 0.00 0.00 0.00

    60 48691.34 0.00 0.00 0.00 0.00 0.00

    3 38 -71934.53 378.35 0.00 0.00 0.00 0.00

    60 72757.05 378.35 0.00 0.00 0.00 0.00

    142 1 60 26769.63 315.29 0.00 0.00 0.00 0.00

    39 -27455.06 315.29 0.00 0.00 0.00 0.00

    2 60 48691.34 0.00 0.00 0.00 0.00 0.00

    39 -48691.34 0.00 0.00 0.00 0.00 0.00

    3 60 75460.96 315.29 0.00 0.00 0.00 0.00

    39 -76146.39 315.29 0.00 0.00 0.00 0.00

    143 1 39 -32003.57 315.29 0.00 0.00 0.00 0.00

    62 32688.99 315.29 0.00 0.00 0.00 0.00

    2 39 -65200.10 0.00 0.00 0.00 0.00 0.00

    62 65200.10 0.00 0.00 0.00 0.00 0.00

    3 39 -97203.66 315.29 0.00 0.00 0.00 0.00

    62 97889.09 315.29 0.00 0.00 0.00 0.00

    144 1 62 35614.73 315.29 0.00 0.00 0.00 0.00

    40 -36300.16 315.29 0.00 0.00 0.00 0.00

    2 62 65200.11 0.00 0.00 0.00 0.00 0.00

    40 -65200.11 0.00 0.00 0.00 0.00 0.00

    3 62 100814.84 315.29 0.00 0.00 0.00 0.00

    40-101500.27 315.29 0.00 0.00 0.00 0.00

    145 1 40 -41221.33 315.29 0.00 0.00 0.00 0.00

    64 41906.75 315.29 0.00 0.00 0.00 0.00

    2 40 -83042.38 0.00 0.00 0.00 0.00 0.00

    64 83042.38 0.00 0.00 0.00 0.00 0.00

    3 40-124263.71 315.29 0.00 0.00 0.00 0.00

    64 124949.14 315.29 0.00 0.00 0.00 0.00

    146 1 64 44832.49 315.29 0.00 0.00 0.00 0.00

    41 -45517.91 315.29 0.00 0.00 0.00 0.00

    2 64 83042.38 0.00 0.00 0.00 0.00 0.00

    41 -83042.38 0.00 0.00 0.00 0.00 0.00

    3 64 127874.88 315.29 0.00 0.00 0.00 0.00

    41-128560.30 315.29 0.00 0.00 0.00 0.00

    147 1 41 -50066.43 315.29 0.00 0.00 0.00 0.00

    66 50751.85 315.29 0.00 0.00 0.00 0.00

    2 41 -99551.15 0.00 0.00 0.00 0.00 0.00

    66 99551.15 0.00 0.00 0.00 0.00 0.00

    3 41-149617.58 315.29 0.00 0.00 0.00 0.00

    66 150303.00 315.29 0.00 0.00 0.00 0.00

    148 1 66 53455.77 378.35 0.00 0.00 0.00 0.00

    42 -54278.28 378.35 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 33

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 66 99551.15 0.00 0.00 0.00 0.00 0.00

    42 -99551.15 0.00 0.00 0.00 0.00 0.00

    3 66 153006.92 378.35 0.00 0.00 0.00 0.00

    42-153829.42 378.35 0.00 0.00 0.00 0.00

    149 1 42 -58691.20 378.35 0.00 0.00 0.00 0.00

    68 59513.71 378.35 0.00 0.00 0.00 0.00

    2 42-117393.42 0.00 0.00 0.00 0.00 0.00

    68 117393.42 0.00 0.00 0.00 0.00 0.00

    3 42-176084.62 378.35 0.00 0.00 0.00 0.00

    68 176907.14 378.35 0.00 0.00 0.00 0.00

    150 1 68 62467.32 504.47 0.00 0.00 0.00 0.00

    43 -63564.01 504.47 0.00 0.00 0.00 0.00

    2 68 117393.42 0.00 0.00 0.00 0.00 0.00

    43-117393.42 0.00 0.00 0.00 0.00 0.00

    3 68 179860.75 504.47 0.00 0.00 0.00 0.00

    43-180957.44 504.47 0.00 0.00 0.00 0.00

    151 1 43 -67701.70 504.47 0.00 0.00 0.00 0.00

    70 68798.38 504.47 0.00 0.00 0.00 0.00

    2 43-133902.25 0.00 0.00 0.00 0.00 0.00

    70 133902.25 0.00 0.00 0.00 0.00 0.00

    3 43-201603.95 504.47 0.00 0.00 0.00 0.00

    70 202700.61 504.47 0.00 0.00 0.00 0.00

    152 1 70 90684.20 628.61 0.00 0.00 0.00 0.00

    45 -92050.73 628.61 0.00 0.00 0.00 0.00

    2 70 168203.61 0.00 0.00 0.00 0.00 0.00

    45-168203.61 0.00 0.00 0.00 0.00 0.00

    3 70 258887.80 628.61 0.00 0.00 0.00 0.00

    45-260254.33 628.61 0.00 0.00 0.00 0.00

    153 1 45 92050.74 628.61 0.00 0.00 0.00 0.00

    72 -90684.20 628.61 0.00 0.00 0.00 0.00

    2 45 169653.31 0.00 0.00 0.00 0.00 0.00

    72-169653.31 0.00 0.00 0.00 0.00 0.00

    3 45 261704.06 628.61 0.00 0.00 0.00 0.00

    72-260337.50 628.61 0.00 0.00 0.00 0.00

    154 1 72 -68798.35 504.47 0.00 0.00 0.00 0.00

    47 67701.67 504.47 0.00 0.00 0.00 0.00

    2 72-135051.73 0.00 0.00 0.00 0.00 0.00

    47 135051.73 0.00 0.00 0.00 0.00 0.00

    3 72-203850.08 504.47 0.00 0.00 0.00 0.00

    47 202753.41 504.47 0.00 0.00 0.00 0.00

    155 1 47 63564.01 504.47 0.00 0.00 0.00 0.00

    74 -62467.33 504.47 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 34

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 47 119754.77 0.00 0.00 0.00 0.00 0.00

    74-119754.77 0.00 0.00 0.00 0.00 0.00

    3 47 183318.78 504.47 0.00 0.00 0.00 0.00

    74-182222.09 504.47 0.00 0.00 0.00 0.00

    156 1 74 -59513.72 378.35 0.00 0.00 0.00 0.00

    48 58691.21 378.35 0.00 0.00 0.00 0.00

    2 74-119754.77 0.00 0.00 0.00 0.00 0.00

    48 119754.77 0.00 0.00 0.00 0.00 0.00

    3 74-179268.48 378.35 0.00 0.00 0.00 0.00

    48 178445.98 378.35 0.00 0.00 0.00 0.00

    157 1 48 54278.29 378.35 0.00 0.00 0.00 0.00

    76 -53455.77 378.35 0.00 0.00 0.00 0.00

    2 48 101515.98 0.00 0.00 0.00 0.00 0.00

    76-101515.98 0.00 0.00 0.00 0.00 0.00

    3 48 155794.25 378.35 0.00 0.00 0.00 0.00

    76-154971.75 378.35 0.00 0.00 0.00 0.00

    158 1 76 -50751.85 315.29 0.00 0.00 0.00 0.00

    49 50066.43 315.29 0.00 0.00 0.00 0.00

    2 76-101515.98 0.00 0.00 0.00 0.00 0.00

    49 101515.98 0.00 0.00 0.00 0.00 0.00

    3 76-152267.83 315.29 0.00 0.00 0.00 0.00

    49 151582.41 315.29 0.00 0.00 0.00 0.00

    159 1 49 45517.92 315.29 0.00 0.00 0.00 0.00

    78 -44832.50 315.29 0.00 0.00 0.00 0.00

    2 49 86219.02 0.00 0.00 0.00 0.00 0.00

    78 -86219.02 0.00 0.00 0.00 0.00 0.00

    3 49 131736.94 315.29 0.00 0.00 0.00 0.00

    78-131051.52 315.29 0.00 0.00 0.00 0.00

    160 1 78 -41906.76 315.29 0.00 0.00 0.00 0.00

    50 41221.34 315.29 0.00 0.00 0.00 0.00

    2 78 -86219.02 0.00 0.00 0.00 0.00 0.00

    50 86219.02 0.00 0.00 0.00 0.00 0.00

    3 78-128125.78 315.29 0.00 0.00 0.00 0.00

    50 127440.35 315.29 0.00 0.00 0.00 0.00

    161 1 50 36300.16 315.29 0.00 0.00 0.00 0.00

    80 -35614.73 315.29 0.00 0.00 0.00 0.00

    2 50 67980.22 0.00 0.00 0.00 0.00 0.00

    80 -67980.22 0.00 0.00 0.00 0.00 0.00

    3 50 104280.38 315.29 0.00 0.00 0.00 0.00

    80-103594.95 315.29 0.00 0.00 0.00 0.00

    162 1 80 -32689.00 315.29 0.00 0.00 0.00 0.00

    51 32003.57 315.29 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 35

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 80 -67980.22 0.00 0.00 0.00 0.00 0.00

    51 67980.22 0.00 0.00 0.00 0.00 0.00

    3 80-100669.21 315.29 0.00 0.00 0.00 0.00

    51 99983.80 315.29 0.00 0.00 0.00 0.00

    163 1 51 27455.06 315.29 0.00 0.00 0.00 0.00

    82 -26769.64 315.29 0.00 0.00 0.00 0.00

    2 51 52683.27 0.00 0.00 0.00 0.00 0.00

    82 -52683.27 0.00 0.00 0.00 0.00 0.00

    3 51 80138.33 315.29 0.00 0.00 0.00 0.00

    82 -79452.91 315.29 0.00 0.00 0.00 0.00

    164 1 82 -24065.72 378.35 0.00 0.00 0.00 0.00

    52 23243.21 378.35 0.00 0.00 0.00 0.00

    2 82 -52683.27 0.00 0.00 0.00 0.00 0.00

    52 52683.27 0.00 0.00 0.00 0.00 0.00

    3 82 -76748.98 378.35 0.00 0.00 0.00 0.00

    52 75926.48 378.35 0.00 0.00 0.00 0.00

    165 1 52 18830.28 378.35 0.00 0.00 0.00 0.00

    84 -18007.78 378.35 0.00 0.00 0.00 0.00

    2 52 24987.06 0.00 0.00 0.00 0.00 0.00

    84 -24987.06 0.00 0.00 0.00 0.00 0.00

    3 52 43817.34 378.35 0.00 0.00 0.00 0.00

    84 -42994.84 378.35 0.00 0.00 0.00 0.00

    166 1 84 -15054.17 504.47 0.00 0.00 0.00 0.00

    53 13957.50 504.47 0.00 0.00 0.00 0.00

    2 84 -24987.08 0.00 0.00 0.00 0.00 0.00

    53 24987.08 0.00 0.00 0.00 0.00 0.00

    3 84 -40041.26 504.47 0.00 0.00 0.00 0.00

    53 38944.58 504.47 0.00 0.00 0.00 0.00

    167 1 53 9819.81 504.47 0.00 0.00 0.00 0.00

    86 -8723.13 504.47 0.00 0.00 0.00 0.00

    2 53 1632.27 0.00 0.00 0.00 0.00 0.00

    86 -1632.27 0.00 0.00 0.00 0.00 0.00

    3 53 11452.08 504.47 0.00 0.00 0.00 0.00

    86 -10355.40 504.47 0.00 0.00 0.00 0.00

    168 1 4 31884.02 1049.48 0.00 0.00 0.00 0.00

    6 -31884.02 1049.48 0.00 0.00 0.00 0.00

    2 4 64324.40 0.00 0.00 0.00 0.00 0.00

    6 -64324.40 0.00 0.00 0.00 0.00 0.00

    3 4 96208.42 1049.48 0.00 0.00 0.00 0.00

    6 -96208.42 1049.48 0.00 0.00 0.00 0.00

    169 1 55 0.00 254.49 0.00 0.00 0.00 0.00

    54 0.00 254.49 0.00 0.00 0.00 0.00

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    DXF IMPORT OF ACAD-89 SPAN.DXF -- PAGE NO. 36

    MEMBER END FORCES STRUCTURE TYPE = SPACE

    -----------------

    ALL UNITS ARE -- KG MMS

    MEMBER LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z

    2 55 0.00 0.00 0.00 0.00 0.00 0.00

    54 0.00 0.00 0.00 0.00 0.00 0.00

    3 55 0.00 254.49 0.00 0.00 0.00 0.00

    54 0.00 254.49 0.00 0.00 0.00 0.00

    170 1 44 0.00 254.49 0.00 0.00 0.00 0.00

    45 0.00 254.49 0.00 0.00 0.00 0.00

    2 44 0.00 0.00 0.00 0.00 0.00 0.00

    45 0.00 0.00 0.00 0.00 0.00 0.00

    3 44 0.00 254.49 0.00 0.00 0.00 0.00

    45 0.00 254.49 0.00 0.00 0.00 0.00

    171 1 45 0.00 254.49 0.00 0.00 0.00 0.00

    46 0.00 254.49 0.00 0.00 0.00 0.00

    2 45 0.00 0.00 0.00 0.00 0.00 0.00

    46 0.00 0.00 0.00 0.00 0.00 0.00

    3 45 0.00 254.49 0.00 0.00 0.00 0.00

    46 0.00 254.49 0.00 0.00 0.00 0.00

    ************** END OF LATEST ANALYSIS RESULT **************

    150. FINISH

    *********** END OF THE STAAD.Pro RUN ***********

    **** DATE= FEB 1,2008 TIME= 17:31:20 ****

    *********************************************************

    * For questions on STAAD.Pro, please contact : *

    * By Email - North America : [email protected] *

    * By Email - International : [email protected] *

    * Tel. (USA) : 714-974-2500 ; Fax (USA) : 714-974-4771 *

    *********************************************************

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    Software licensed to (

    Job Title

    Client

    Cantilever Erection Span 92m

    RVNL

    Print Time/Date: 02/02/2008 10:26 STAAD.Pro for Windows Release 2003

    56 656463626160595857 66

    49484746

    67 77 7876

    45

    7574737271706968

    44

    13 222120193181716151412 2311109876432 24

    434241403938373635

    1 25

    X

    Y

    Z

    Whole Structure

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    BOTTOM CHORD L0-L3

    Section element Rotationangle

    Mirror Material E (kg/mm^2)

    Sheet 20 x 750 Steel 20897.044Sheet 20 x 750 Steel 20897.044Sheet 150 x 20 Steel 20897.044Sheet 150 x 20 Steel 20897.044

    Sheet 150 x 20 Steel 20897.044Sheet 150 x 20 Steel 20897.044

    The overall dimentions of the section are 650.0 x 750.0 mm

    Basic geometry of the sectionParameter Value

    A Sectional area 42000.0 mm2

    Angle of principal inertia axes -90.0 deg

    Iy Inertia moment about centroidal Y1-axis parallel with Y-axis 3005350000.04

    Iz Inertia moment about centroidal Z1-axis parallel with Z-axis 3635050000.04

    It Torsional moment of inertia (St. Venant) 5226666.667 mm4

    iy Radius of inertia about Y1-axis 267.499 mm

    iz Radius of inertia about Z1-axis 294.192 mm

    Wu+ Maximum resisting moment about U-axis11184769.231

    3

    Wu- Minimum resisting moment about U-axis 11184769.2313

    Wv+ Maximum resisting moment about V-axis 8014266.667 mm3

    Wv- Minimum resisting moment about V-axis 8014266.667 mm3

    Wpl,u Plastic resisting moment about U-axis 12210000.0 mm3

    Wpl,v Plastic resisting moment about V-axis 10003539.6 mm3

    Iu Maximum inertia moment 3635050000.04

    Iv Minimum inertia moment 3005350000.04

    iu Maximum radius of inertia 294.192 mm

    iv Minimum radius of inertia 267.499 mm

    au+ Middle point along positive direction of Y(U)-axis 190.816 mm

    au- Middle point along negative direction of Y(U)-axis 190.816 mm

    av+ Middle point along positive direction of Z(V)-axis 266.304 mm

    av- Middle point along negative direction of Z(V)-axis 266.304 mm

    yM Coordinate of the center of gravity along Y-axis325.0

    mm

    zM Coordinate of the center of gravity along Z-axis -375.0 mm

    File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L0-L1.sec

    U

    V

    Z

    Y

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    BOTTOM CHORD L5-L7

    Section element Rotationangle

    Mirror Material E (kg/mm^2)

    Sheet 16 x 750 Steel 20897.044Sheet 16 x 750 Steel 20897.044Sheet 150 x 16 Steel 20897.044Sheet 150 x 16 Steel 20897.044

    Sheet 150 x 16 Steel 20897.044Sheet 150 x 16 Steel 20897.044Sheet 16 x 650 Steel 20897.044Sheet 16 x 650 Steel 20897.044

    The overall dimentions of the section are 650.0 x 750.0 mm

    Basic geometry of the sectionParameter Value

    A Sectional area 54400.0 mm2

    Angle of principal inertia axes -90.0 deg

    Iy Inertia moment about centroidal Y1-axis parallel with Y-axis 3150552533.333 04

    Iz Inertia moment about centroidal Z1-axis parallel with Z-axis 4840850133.333 04

    It Torsional moment of inertia (St. Venant) 4362226.554 mm4

    iy Radius of inertia about Y1-axis240.654

    mm

    iz Radius of inertia about Z1-axis 298.306 mm

    Wu+ Maximum resisting moment about U-axis 14894923.4873

    Wu- Minimum resisting moment about U-axis 14894923.4873

    Wv+ Maximum resisting moment about V-axis 8401473.422 mm3

    Wv- Minimum resisting moment about V-axis 8401473.422 mm3

    Wpl,u Plastic resisting moment about U-axis 16116163.2 mm3

    Wpl,v Plastic resisting moment about V-axis 11404105.92 mm3

    Iu Maximum inertia moment 4840850133.333 04

    Iv Minimum inertia moment 3150552533.333 04

    iu Maximum radius of inertia 298.306 mm

    iv Minimum radius of inertia 240.654 mm

    au+ Middle point along positive direction of Y(U)-axis 154.439 mm

    au- Middle point along negative direction of Y(U)-axis 154.439 mm

    av+ Middle point along positive direction of Z(V)-axis273.804

    mm

    av- Middle point along negative direction of Z(V)-axis 273.804 mm

    yM Coordinate of the center of gravity along Y-axis 325.0 mm

    zM Coordinate of the center of gravity along Z-axis -375.0 mm

    File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L5-L7.sec

    U

    V

    Z

    Y

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    BOTTOM CHORD L7-L9

    Section element Rotationangle

    Mirror Material E (kg/mm^2)

    Sheet 16 x 750 Steel 20897.044Sheet 16 x 750 Steel 20897.044Sheet 150 x 20 Steel 20897.044Sheet 150 x 20 Steel 20897.044

    Sheet 150 x 20 Steel 20897.044Sheet 150 x 20 Steel 20897.044Sheet 16 x 650 Steel 20897.044Sheet 16 x 650 Steel 20897.044

    The overall dimentions of the section are 650.0 x 750.0 mm

    Basic geometry of the sectionParameter Value

    A Sectional area 56800.0 mm2

    Angle of principal inertia axes -90.0 deg

    Iy Inertia moment about centroidal Y1-axis parallel with Y-axis 3456433333.333 04

    Iz Inertia moment about centroidal Z1-axis parallel with Z-axis 4976764533.333 04

    It Torsional moment of inertia (St. Venant) 5061605.754 mm4

    iy Radius of inertia about Y1-axis246.683

    mm

    iz Radius of inertia about Z1-axis 296.005 mm

    Wu+ Maximum resisting moment about U-axis 15313121.6413

    Wu- Minimum resisting moment about U-axis 15313121.6413

    Wv+ Maximum resisting moment about V-axis 9217155.556 mm3

    Wv- Minimum resisting moment about V-axis 9217155.556 mm3

    Wpl,u Plastic resisting moment about U-axis 16677763.2 mm3

    Wpl,v Plastic resisting moment about V-axis 12260620.32 mm3

    Iu Maximum inertia moment 4976764533.333 04

    Iv Minimum inertia moment 3456433333.333 04

    iu Maximum radius of inertia 296.005 mm

    iv Minimum radius of inertia 246.683 mm

    au+ Middle point along positive direction of Y(U)-axis 162.274 mm

    au- Middle point along negative direction of Y(U)-axis 162.274 mm

    av+ Middle point along positive direction of Z(V)-axis269.597

    mm

    av- Middle point along negative direction of Z(V)-axis 269.597 mm

    yM Coordinate of the center of gravity along Y-axis 325.0 mm

    zM Coordinate of the center of gravity along Z-axis -375.0 mm

    File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\L7-L9.sec

    U

    V

    Z

    Y

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    UPPER CHORD U1-U3

    Section element Rotationangle

    Mirror Material E (kg/mm^2)

    Sheet 650 x 20 Steel 20897.044Sheet 16 x 680 Steel 20897.044Sheet 16 x 680 Steel 20897.044Sheet 150 x 16 Steel 20897.044

    Sheet 150 x 16 Steel 20897.044

    The overall dimentions of the section are 650.0 x 700.0 mm

    Basic geometry of the sectionParameter Value

    A Sectional area 39560.0 mm2

    Angle of principal inertia axes -90.0 deg

    Iy Inertia moment about centroidal Y1-axis parallel with Y-axis 2739658426.424 04

    Iz Inertia moment about centroidal Z1-axis parallel with Z-axis 2916641986.667 04

    It Torsional moment of inertia (St. Venant) 3759516.755 mm4

    iy Radius of inertia about Y1-axis 263.16 mm

    iz Radius of inertia about Z1-axis271.527

    mm

    Wu+ Maximum resisting moment about U-axis 8974283.036 mm3

    Wu- Minimum resisting moment about U-axis 8974283.036 mm3

    Wv+ Maximum resisting moment about V-axis 6605851.68 mm3

    Wv- Minimum resisting moment about V-axis 9603807.407 mm3

    Wpl,u Plastic resisting moment about U-axis 10133620.0 mm3

    Wpl,v Plastic resisting moment about V-axis 9407411.743 mm3

    Iu Maximum inertia moment 2916641986.667 04

    Iv Minimum inertia moment 2739658426.424 04

    iu Maximum radius of inertia 271.527 mm

    iv Minimum radius of inertia 263.16 mm

    au+ Middle point along positive direction of Y(U)-axis 166.983 mm

    au- Middle point along negative direction of Y(U)-axis 242.766 mm

    av+ Middle point along positive direction of Z(V)-axis 226.852 mm

    av- Middle point along negative direction of Z(V)-axis226.852

    mm

    yM Coordinate of the center of gravity along Y-axis 325.0 mm

    zM Coordinate of the center of gravity along Z-axis -414.732 mm

    File: C:\My Data\India Project\01Roadbed Works\Design\Cantilever Erection\U1-U3.sec

    V

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    Y

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    UPPER CHORD U3-U5

    Section element Rotationangle

    Mirror Material E (kg/mm^2)

    Sheet 650 x 16 Steel 20897.044Sheet 12 x 684 Steel 20897.044Sheet 12 x 684 Steel 20897.044Sheet 150 x 12 Steel 20897.044

    Sheet 150 x 12 Steel 208