****************************************************
* *
* STAAD.Pro V8i SELECTseries6 *
* Version 20.07.11.33 *
* Proprietary Program of *
* Bentley Systems, Inc. *
* Date= MAR 1, 2024 *
* Time= 5:29:31 *
* *
* USER ID: *
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1. STAAD SPACE
INPUT FILE: C:\Users\natha\OneDrive\Desktop\CAPSTONE\BASIS STRUCTURAL\AV B F OFFSET D6.STD
2. START JOB INFORMATION
3. ENGINEER DATE 08-FEB-24
4. END JOB INFORMATION
5. INPUT WIDTH 79
6. UNIT METER KN
7. JOINT COORDINATES
8. 1 0 4.9 -1; 2 0 0 0; 3 0 0.9 0; 4 0 4.9 0; 5 0 0 5; 6 0 0.9 5; 7 0 4.9 5
9. 8 0 7.15 5; 9 0 0 10; 10 0 0.9 10; 11 0 4.9 10; 12 0 4.9 11; 13 4.5 0 0
10. 14 4.5 0.9 0; 15 4.5 4.9 0; 16 4.5 0.9 5; 17 4.5 4.9 5; 18 4.5 0 10
11. 19 4.5 0.9 10; 20 4.5 4.9 10; 21 9 0 0; 22 9 0.9 0; 23 9 4.9 0; 24 9 0.9 5
12. 25 9 4.9 5; 26 9 0 10; 27 9 0.9 10; 28 9 4.9 10; 29 13.5 0 0; 30 13.5 0.9 0
13. 31 13.5 4.9 0; 32 13.5 0.9 5; 33 13.5 4.9 5; 34 13.5 0 10; 35 13.5 0.9 10
14. 36 13.5 4.9 10; 37 18 4.9 -1; 38 18 0 0; 39 18 0.9 0; 40 18 4.9 0; 41 18 0 5
15. 42 18 0.9 5; 43 18 4.9 5; 44 18 7.15 5; 45 18 0 10; 46 18 0.9 10; 47 18 4.9 10
16. 48 18 4.9 11; 49 1.125 0.9 0; 50 2.25 0.9 0; 51 3.375 0.9 0; 52 5.625 0.9 0
17. 53 6.75 0.9 0; 54 7.875 0.9 0; 55 10.125 0.9 0; 56 11.25 0.9 0
18. 57 12.375 0.9 0; 58 14.625 0.9 0; 59 15.75 0.9 0; 60 16.875 0.9 0
19. 61 1.125 0.9 5; 62 2.25 0.9 5; 63 3.375 0.9 5; 64 5.625 0.9 5; 65 6.75 0.9 5
20. 66 7.875 0.9 5; 67 10.125 0.9 5; 68 11.25 0.9 5; 69 12.375 0.9 5
21. 70 14.625 0.9 5; 71 15.75 0.9 5; 72 16.875 0.9 5; 73 1.125 0.9 10
22. 74 2.25 0.9 10; 75 3.375 0.9 10; 76 5.625 0.9 10; 77 6.75 0.9 10
23. 78 7.875 0.9 10; 79 10.125 0.9 10; 80 11.25 0.9 10; 81 12.375 0.9 10
24. 82 14.625 0.9 10; 83 15.75 0.9 10; 84 16.875 0.9 10; 85 0 0.9 1; 86 0 0.9 2
25. 87 0 0.9 3; 88 0 0.9 4; 89 4.5 0.9 1; 90 4.5 0.9 2; 91 4.5 0.9 3; 92 4.5 0.9 4
26. 93 9 0.9 1; 94 9 0.9 2; 95 9 0.9 3; 96 9 0.9 4; 97 13.5 0.9 1; 98 13.5 0.9 2
27. 99 13.5 0.9 3; 100 13.5 0.9 4; 101 18 0.9 1; 102 18 0.9 2; 103 18 0.9 3
28. 104 18 0.9 4; 105 0 0.9 6; 106 0 0.9 7; 107 0 0.9 8; 108 0 0.9 9
29. 109 4.5 0.9 6; 110 4.5 0.9 7; 111 4.5 0.9 8; 112 4.5 0.9 9; 113 9 0.9 6
30. 114 9 0.9 7; 115 9 0.9 8; 116 9 0.9 9; 117 13.5 0.9 6; 118 13.5 0.9 7
31. 119 13.5 0.9 8; 120 13.5 0.9 9; 121 18 0.9 6; 122 18 0.9 7; 123 18 0.9 8
32. 124 18 0.9 9
33. MEMBER INCIDENCES
34. 1 3 49; 2 14 52; 3 22 55; 4 30 58; 5 2 3; 6 13 14; 7 21 22; 8 29 30; 9 38 39
35. 10 6 61; 11 16 64; 12 24 67; 13 32 70; 14 5 6; 18 41 42; 19 10 73; 20 19 76
36. 21 27 79; 22 35 82; 23 9 10; 24 18 19; 25 26 27; 26 34 35; 27 45 46; 28 3 85
37. 29 14 89; 30 22 93; 31 30 97; 32 39 101; 33 6 105; 34 16 109; 35 24 113
38. 36 32 117; 37 42 121; 38 3 4; 39 14 15; 40 22 23; 41 30 31; 42 39 40; 43 6 7
STAAD SPACE -- PAGE NO. 2
39. 47 42 43; 48 10 11; 49 19 20; 50 27 28; 51 35 36; 52 46 47; 53 4 15; 54 15 23
40. 55 23 31; 56 31 40; 57 7 17; 58 17 25; 59 25 33; 60 33 43; 61 11 20; 62 20 28
41. 63 28 36; 64 36 47; 65 4 7; 66 15 17; 67 23 25; 68 31 33; 69 40 43; 70 7 11
42. 71 17 20; 72 25 28; 73 33 36; 74 43 47; 83 7 8; 84 11 12; 85 4 1; 86 40 37
43. 87 47 48; 88 43 44; 89 44 48; 90 44 37; 91 8 12; 92 8 1; 93 49 50; 94 50 51
44. 95 51 14; 96 52 53; 97 53 54; 98 54 22; 99 55 56; 100 56 57; 101 57 30
45. 102 58 59; 103 59 60; 104 60 39; 105 61 62; 106 62 63; 107 63 16; 108 64 65
46. 109 65 66; 110 66 24; 111 67 68; 112 68 69; 113 69 32; 114 70 71; 115 71 72
47. 116 72 42; 117 73 74; 118 74 75; 119 75 19; 120 76 77; 121 77 78; 122 78 27
48. 123 79 80; 124 80 81; 125 81 35; 126 82 83; 127 83 84; 128 84 46; 129 85 86
49. 130 86 87; 131 87 88; 132 88 6; 133 89 90; 134 90 91; 135 91 92; 136 92 16
50. 137 93 94; 138 94 95; 139 95 96; 140 96 24; 141 97 98; 142 98 99; 143 99 100
51. 144 100 32; 145 101 102; 146 102 103; 147 103 104; 148 104 42; 149 105 106
52. 150 106 107; 151 107 108; 152 108 10; 153 109 110; 154 110 111; 155 111 112
53. 156 112 19; 157 113 114; 158 114 115; 159 115 116; 160 116 27; 161 117 118
54. 162 118 119; 163 119 120; 164 120 35; 165 121 122; 166 122 123; 167 123 124
55. 168 124 46
56. ELEMENT INCIDENCES SHELL
57. 75 14 16 6 3; 76 22 24 16 14; 77 30 32 24 22; 78 39 42 32 30; 79 42 46 35 32
58. 80 32 35 27 24; 81 24 27 19 16; 82 16 19 10 6
59. START GROUP DEFINITION
60. FLOOR
61. _1STFLOOR 1 TO 4 10 TO 13 19 TO 22 28 TO 37 93 TO 168
62. _CEILING 53 TO 74
63. _ROOM 1 TO 4 10 TO 13 19 TO 22 28 TO 37 93 TO 168
64. MEMBER
65. _W1 1 TO 4 19 TO 22 28 32 33 37 93 TO 104 117 TO 132 145 TO 152 165 TO 168
66. _W2 65 69 70 74 84 TO 87
67. _R1 89 TO 92
68. _TC1 90 92
69. _TC2 89 91
70. JOINT
71. _1 4 15 23 31 40
72. _9 11 20 28 36 47
73. END GROUP DEFINITION
74. ELEMENT PROPERTY
75. 75 TO 82 THICKNESS 0.1
76. DEFINE MATERIAL START
77. ISOTROPIC CONCRETE
78. E 2.17185E+007
79. POISSON 0.17
80. DENSITY 23.5616
81. ALPHA 1E-005
82. DAMP 0.05
83. TYPE CONCRETE
84. STRENGTH FCU 27579
85. ISOTROPIC 21MPA
86. E 2.1538E+007
87. POISSON 0.17
88. DENSITY 24
89. ALPHA 1E-005
90. DAMP 0.05
91. G 9.28139E+006
92. TYPE CONCRETE
93. STRENGTH FCU 21000
94. END DEFINE MATERIAL
STAAD SPACE -- PAGE NO. 3
95. MEMBER PROPERTY AMERICAN
96. 1 TO 4 10 TO 13 19 TO 22 28 TO 37 53 TO 74 84 TO 87 93 TO 167 -
97. 168 PRIS YD 0.4 ZD 0.25
98. MEMBER PROPERTY AMERICAN
99. 5 TO 9 14 18 23 TO 27 38 TO 43 47 TO 52 83 88 PRIS YD 0.35 ZD 0.35
100. MEMBER PROPERTY AMERICAN
101. 89 TO 92 PRIS YD 0.3 ZD 0.25
102. CONSTANTS
103. MATERIAL 21MPA ALL
104. SUPPORTS
105. 3 6 10 14 16 19 22 24 27 30 32 35 39 42 46 49 TO 123 -
106. 124 FIXED BUT MX MY MZ KFX 2400 KFY 2400 KFZ 2400
107. 2 5 9 13 18 21 26 29 34 38 41 45 FIXED
108. MEMBER RELEASE
109. 57 START MZ
110. 60 END MZ
111. MEMBER OFFSET
112. 65 START 0 0 -0.2
113. 70 TO 74 END 0 0 0.2
114. 28 START 0 0 -0.175
115. 1 93 START -0.175 0 0
116. MEMBER CRACKED
117. 5 TO 9 14 18 23 TO 27 38 TO 43 47 TO 52 83 -
118. 88 REDUCTION RIY 0.700000 RIZ 0.700000
119. 1 TO 4 10 TO 13 19 TO 22 28 TO 37 53 TO 74 84 TO 87 89 TO 167 -
120. 168 REDUCTION RIY 0.350000 RIZ 0.350000
121. DEFINE REFERENCE LOADS
122. LOAD R1 LOADTYPE MASS TITLE DL
123. SELFWEIGHT Y 1 LIST 1 TO 14 18 TO 43 47 TO 82
124. FLOOR LOAD
125. _1STFLOOR FLOAD 2.4 GY
126. _CEILING FLOAD 0.5 GY
127. MEMBER LOAD
128. 1 TO 4 19 TO 22 28 32 33 37 93 TO 104 117 TO 132 145 TO 152 165 TO 167 -
129. 168 UNI GY 11.7
130. _W2 UNI GY 6
131. _R1 UNI GY 2.3
132. JOINT LOAD
133. _1 FX 0 FY 32.238 FZ 68.763 MX 0 MY 0 MZ 0
134. _9 FX 0 FY 32.238 FZ -68.763 MX 0 MY 0 MZ 0
135. MEMBER LOAD
136. 1 TO 4 19 TO 22 28 32 33 37 93 TO 104 117 TO 132 145 TO 152 165 TO 167 -
137. 168 UNI GY 8.5
138. END DEFINE REFERENCE LOADS
*** NOTE: MASS MODEL FORMED WILL BE USED IN SEISMIC/RESPONSE/TIME HISTORY LOADING, IF ANY.
IF MASS MODEL IS SEPARATELY PROVIDED IN INDIVIDUAL LOADING, THE GENERATED MASS
WILL BE REPLACED BY THE MASS PROVIDED IN INDIVIDUAL LOADING.
139. FLOOR DIAPHRAGM
140. DIA 1 TYPE RIG HEI 0.9 JOINT 3 6 10 14 16 19 22 24 27 30 32 35 39 42 46 49 -
141. 50 TO 124
*** ERROR: SUPPORT OR SPRING IN SLAVE DIRECTION. JOINT= 3 DIR= 1
*********** END OF THE STAAD.Pro RUN ***********
**** DATE= MAR 1,2024 TIME= 5:29:32 ****
STAAD SPACE -- PAGE NO. 4
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* Details about additional assistance from *
* Bentley and Partners can be found at program menu *
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