Staad Output BW
Staad Output BW
Staad Output BW
PAGE NO. 1
****************************************************
* *
* STAAD.Pro V8i SELECTseries6 *
* Version 20.07.11.33 *
* Proprietary Program of *
* Bentley Systems, Inc. *
* Date= OCT 10, 2021 *
* Time= 16:28:56 *
* *
* USER ID: ITS *
****************************************************
1. STAAD SPACE
INPUT FILE: E:\Kerjaan\Project PLTU Sulut Timor\Timor\WTP Equip\BW SW\Staad\T1-PP-XXX-CVL-CAL-XXXXX_R0.. .STD
2. START JOB INFORMATION
3. ENGINEER DATE 09-SEP-21
4. END JOB INFORMATION
5. INPUT WIDTH 79
6. SET NL 1000
7. UNIT METER KG
8. JOINT COORDINATES
9. 1 -0.15 0 0; 2 -0.15 0 0.75; 3 -0.15 0 1.5; 4 -0.15 0 2.25; 5 -0.15 0 3
10. 6 0 0 0; 7 0 0 0.75; 8 0 0 1.5; 9 0 0 2.25; 10 0 0 3; 11 0.5 0 0
11. 12 0.5 0 0.75; 13 0.5 0 1.5; 14 0.5 0 2.25; 15 0.5 0 3; 16 1 0 0; 17 1 0 0.75
12. 18 1 0 1.5; 19 1 0 2.25; 20 1 0 3; 21 1.5 0 0; 22 1.5 0 0.75; 23 1.5 0 1.5
13. 24 1.5 0 2.25; 25 1.5 0 3; 26 2 0 0; 27 2 0 0.75; 28 2 0 1.5; 29 2 0 2.25
14. 30 2 0 3; 31 2.15 0 0; 32 2.15 0 0.75; 33 2.15 0 1.5; 34 2.15 0 2.25
15. 35 2.15 0 3; 36 0 0.6 1.5; 37 1 0.6 1.5; 38 2 0.6 1.5
16. MEMBER INCIDENCES
17. 1 8 36; 2 18 37; 3 28 38
18. ELEMENT INCIDENCES SHELL
19. 4 1 6 7 2; 5 2 7 8 3; 6 3 8 9 4; 7 4 9 10 5; 8 6 11 12 7; 9 7 12 13 8
20. 10 8 13 14 9; 11 9 14 15 10; 12 11 16 17 12; 13 12 17 18 13; 14 13 18 19 14
21. 15 14 19 20 15; 16 16 21 22 17; 17 17 22 23 18; 18 18 23 24 19; 19 19 24 25 20
22. 20 21 26 27 22; 21 22 27 28 23; 22 23 28 29 24; 23 24 29 30 25; 24 26 31 32 27
23. 25 27 32 33 28; 26 28 33 34 29; 27 29 34 35 30
24. ELEMENT PROPERTY
25. 4 TO 27 THICKNESS 0.2
26. DEFINE MATERIAL START
27. ISOTROPIC STEEL
28. E 2.09042E+010
29. POISSON 0.3
30. DENSITY 7833.41
31. ALPHA 1.2E-005
32. DAMP 0.03
33. TYPE STEEL
34. STRENGTH FY 2.58192E+007 FU 4.1584E+007 RY 1.5 RT 1.2
35. ISOTROPIC CONCRETE
36. E 2.21467E+009
37. POISSON 0.17
38. DENSITY 2402.62
1 0.028125
2 0.056250
3 0.056250
4 0.056250
5 0.028125
6 0.121875
7 0.243750
8 0.243750
9 0.243750
10 0.121875
11 0.187500
12 0.375000
13 0.375000
14 0.375000
15 0.187500
16 0.187500
17 0.375000
18 0.375000
19 0.375000
20 0.187500
21 0.187500
22 0.375000
23 0.375000
24 0.375000
25 0.187500
26 0.121875
27 0.243750
28 0.243750
29 0.243750
30 0.121875
31 0.028125
32 0.056250
33 0.056250
34 0.056250
35 0.028125
TOTAL 6.900000
50. DEFINE REFERENCE LOADS
51. LOAD R1 LOADTYPE DEAD TITLE SELFWEIGHT SEISMIC
52. SELFWEIGHT Y -1
53. LOAD R2 LOADTYPE NONE TITLE EQUIPMENT
54. JOINT LOAD
55. 37 FY -6315
56. 36 38 FY -3158
57. 37 FY -152.2
58. 36 38 FY -76.11
59. END DEFINE REFERENCE LOADS
60. DEFINE IBC 2003
61. SDS 0.77 SD1 0.317 S1 0.25 IE 1.5 RX 3 RZ 3 SCLASS 4 CT 0.047
62. REFERENCE LOAD Y
63. R1 1.0 R2 1.0
64. LOAD 23 VX+
65. IBC LOAD X 1
66. PERFORM ANALYSIS
P R O B L E M S T A T I S T I C S
-----------------------------------
************************************************************
* IBC 2003 SEISMIC LOAD ALONG X : *
* CT = 0.019 Cu = 1.400 *
* TIME PERIODS : *
* Ta = 0.032 T = 0.055 Tuser = 0.000 *
* TIME PERIOD USED (T) = 0.045 *
* LOAD FACTOR = 1.000 *
* DESIGN BASE SHEAR = 1.000 X 0.385 X 20143.28 *
* = 7755.16 KG *
************************************************************
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
67. CHANGE
68. LOAD 24 VX -
69. IBC LOAD X -1.
70. PERFORM ANALYSIS
************************************************************
* IBC 2003 SEISMIC LOAD ALONG X : *
* CT = 0.019 Cu = 1.400 *
* TIME PERIODS : *
* Ta = 0.032 T = 0.055 Tuser = 0.000 *
* TIME PERIOD USED (T) = 0.045 *
* LOAD FACTOR = -1.000 *
* DESIGN BASE SHEAR = -1.000 X 0.385 X 20143.28 *
* = -7755.16 KG *
************************************************************
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
71. CHANGE
72. LOAD 25 VZ+
73. IBC LOAD Z 1
************************************************************
* IBC 2003 SEISMIC LOAD ALONG Z : *
* CT = 0.019 Cu = 1.400 *
* TIME PERIODS : *
* Ta = 0.032 T = 0.049 Tuser = 0.000 *
* TIME PERIOD USED (T) = 0.045 *
* LOAD FACTOR = 1.000 *
* DESIGN BASE SHEAR = 1.000 X 0.385 X 20143.28 *
* = 7755.16 KG *
************************************************************
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
75. CHANGE
76. LOAD 26 VZ -
77. IBC LOAD Z -1.
78. PERFORM ANALYSIS
************************************************************
* IBC 2003 SEISMIC LOAD ALONG Z : *
* CT = 0.019 Cu = 1.400 *
* TIME PERIODS : *
* Ta = 0.032 T = 0.049 Tuser = 0.000 *
* TIME PERIOD USED (T) = 0.045 *
* LOAD FACTOR = -1.000 *
* DESIGN BASE SHEAR = -1.000 X 0.385 X 20143.28 *
* = -7755.16 KG *
************************************************************
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
THE ABOVE CONDITIONS COULD ALSO BE CAUSED BY VERY STIFF OR VERY WEAK
ELEMENTS AS WELL AS TRUE SINGULARITIES.
79. CHANGE
80. ***********************************************************
81. LOAD 27 LOADTYPE NONE TITLE VEX+
246. *===========*
247. * OPERATION *
248. *===========*
249. LOAD 141 1D+1E(O)+1P(O)+1TF+1TA
250. REPEAT LOAD
251. 1 1.0 5 1.0 8 1.0 10 1.0 11 1.0
252. LOAD 142 1D+1L+1E(O)+1P(O)+1TF+1TA+1I1+1SP
253. REPEAT LOAD
254. 1 1.0 2 1.0 5 1.0 8 1.0 10 1.0 11 1.0 13 1.0 17 1.0
255. LOAD 143 1D+1L+1E(O)+1P(O)+1TF+1TA+1I2+1SP
256. REPEAT LOAD
257. 1 1.0 2 1.0 5 1.0 8 1.0 10 1.0 11 1.0 14 1.0 17 1.0
258. LOAD 144 1D+1L+1E(O)+1P(O)+1TF+1TA+1I3+1SP
259. REPEAT LOAD
260. 1 1.0 2 1.0 5 1.0 8 1.0 10 1.0 11 1.0 15 1.0 17 1.0
261. LOAD 145 1D+1L+1E(O)+1P(O)+1TF+1TA+1I4+1SP
262. REPEAT LOAD
263. 1 1.0 2 1.0 5 1.0 8 1.0 10 1.0 11 1.0 16 1.0 17 1.0
264. LOAD 146 1D+1LR+1E(O)+1P(O)+1TF+1TA+1I1+1SP
265. REPEAT LOAD
266. 1 1.0 3 1.0 5 1.0 8 1.0 10 1.0 11 1.0 13 1.0 17 1.0
267. LOAD 147 1D+1LR+1E(O)+1P(O)+1TF+1TA+1I2+1SP
268. REPEAT LOAD
269. 1 1.0 3 1.0 5 1.0 8 1.0 10 1.0 11 1.0 14 1.0 17 1.0
270. LOAD 148 1D+1LR+1E(O)+1P(O)+1TF+1TA+1I3+1SP
271. REPEAT LOAD
272. 1 1.0 3 1.0 5 1.0 8 1.0 10 1.0 11 1.0 15 1.0 17 1.0
273. LOAD 149 1D+1LR+1E(O)+1P(O)+1TF+1TA+1I4+1SP
274. REPEAT LOAD
275. 1 1.0 3 1.0 5 1.0 8 1.0 10 1.0 11 1.0 16 1.0 17 1.0
276. LOAD 150 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I1+1SP
277. REPEAT LOAD
278. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 13 0.75 17 1.0
279. LOAD 151 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I2+1SP
280. REPEAT LOAD
281. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 14 0.75 17 1.0
282. LOAD 152 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I3+1SP
283. REPEAT LOAD
284. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 15 0.75 17 1.0
285. LOAD 153 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I4+1SP
286. REPEAT LOAD
287. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 16 0.75 17 1.0
288. LOAD 154 1D+1E(O)+1P(O)+1TF+1TA+1SP+1WX+
289. REPEAT LOAD
290. 1 1.0 5 1.0 8 1.0 10 1.0 11 1.0 17 1.0 19 1.0
291. LOAD 155 1D+1E(O)+1P(O)+1TF+1TA+1SP+1WX -
292. REPEAT LOAD
293. 1 1.0 5 1.0 8 1.0 10 1.0 11 1.0 17 1.0 20 1.0
294. LOAD 156 1D+1E(O)+1P(O)+1TF+1TA+1SP+1WZ+
295. REPEAT LOAD
296. 1 1.0 5 1.0 8 1.0 10 1.0 11 1.0 17 1.0 21 1.0
297. LOAD 157 1D+1E(O)+1P(O)+1TF+1TA+1SP+1WZ -
298. REPEAT LOAD
299. 1 1.0 5 1.0 8 1.0 10 1.0 11 1.0 17 1.0 22 1.0
300. LOAD 158 1.13D+1.13E(O)+1.13P(O)+1TF+1TA+1SP+0.7VX++0.21VZ++0.7VEX++0.21VEZ+
301. REPEAT LOAD
302. 1 1.13 5 1.13 8 1.13 10 1.0 11 1.0 17 1.0 23 0.7 25 0.21 27 0.7 29 0.21
303. LOAD 159 1.13D+1.13E(O)+1.13P(O)+1TF+1TA+1SP+0.7VX++0.21VZ-+0.7VEX++0.21VEZ -
304. REPEAT LOAD
305. 1 1.13 5 1.13 8 1.13 10 1.0 11 1.0 17 1.0 23 0.7 26 0.21 27 0.7 30 0.21
306. LOAD 160 1.13D+1.13E(O)+1.13P(O)+1TF+1TA+1SP+0.7VX-+0.21VZ++0.7VEX-+0.21VEZ+
307. REPEAT LOAD
308. 1 1.13 5 1.13 8 1.13 10 1.0 11 1.0 17 1.0 24 0.7 25 0.21 28 0.7 29 0.21
309. LOAD 161 1.13D+1.13E(O)+1.13P(O)+1TF+1TA+1SP+0.7VX-+0.21VZ-+0.7VEX-+0.21VEZ -
310. REPEAT LOAD
311. 1 1.13 5 1.13 8 1.13 10 1.0 11 1.0 17 1.0 24 0.7 26 0.21 28 0.7 30 0.21
312. LOAD 162 1.13D+1.13E(O)+1.13P(O)+1TF+1TA+1SP+0.21VX++0.7VZ++0.21VEX++0.7VEZ+
313. REPEAT LOAD
314. 1 1.13 5 1.13 8 1.13 10 1.0 11 1.0 17 1.0 23 0.21 25 0.7 27 0.21 29 0.7
315. LOAD 163 1.13D+1.13E(O)+1.13P(O)+1TF+1TA+1SP+0.21VX-+0.7VZ++0.21VEX-+0.7VEZ+
316. REPEAT LOAD
317. 1 1.13 5 1.13 8 1.13 10 1.0 11 1.0 17 1.0 24 0.21 25 0.7 28 0.21 29 0.7
318. LOAD 164 1.13D+1.13E(O)+1.13P(O)+1TF+1TA+1SP+0.21VX++0.7VZ-+0.21VEX++0.7VEZ -
319. REPEAT LOAD
320. 1 1.13 5 1.13 8 1.13 10 1.0 11 1.0 17 1.0 23 0.21 26 0.7 27 0.21 30 0.7
321. LOAD 165 1.13D+1.13E(O)+1.13P(O)+1TF+1TA+1SP+0.21VX-+0.7VZ-+0.21VEX-+0.7VEZ -
322. REPEAT LOAD
323. 1 1.13 5 1.13 8 1.13 10 1.0 11 1.0 17 1.0 24 0.21 26 0.7 28 0.21 30 0.7
324. LOAD 166 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I1+1SP+0.75WX+
325. REPEAT LOAD
326. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 13 0.75 17 1.0 19 0.75
327. LOAD 167 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I1+1SP+0.75WX -
328. REPEAT LOAD
329. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 13 0.75 17 1.0 20 0.75
330. LOAD 168 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I1+1SP+0.75WZ+
331. REPEAT LOAD
332. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 13 0.75 17 1.0 21 0.75
333. LOAD 169 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I1+1SP+0.75WZ -
334. REPEAT LOAD
335. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 13 0.75 17 1.0 22 0.75
336. LOAD 170 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I2+1SP+0.75WX+
337. REPEAT LOAD
338. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 14 0.75 17 1.0 19 0.75
339. LOAD 171 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I2+1SP+0.75WX -
340. REPEAT LOAD
341. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 14 0.75 17 1.0 20 0.75
342. LOAD 172 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I2+1SP+0.75WZ+
343. REPEAT LOAD
344. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 14 0.75 17 1.0 21 0.75
345. LOAD 173 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I2+1SP+0.75WZ -
346. REPEAT LOAD
347. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 14 0.75 17 1.0 22 0.75
348. LOAD 174 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I3+1SP+0.75WX+
349. REPEAT LOAD
350. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 15 0.75 17 1.0 19 0.75
351. LOAD 175 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I3+1SP+0.75WX -
352. REPEAT LOAD
353. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 15 0.75 17 1.0 20 0.75
354. LOAD 176 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I3+1SP+0.75WZ+
355. REPEAT LOAD
356. 1 1.0 2 0.75 3 0.75 5 1.0 8 1.0 10 1.0 11 1.0 15 0.75 17 1.0 21 0.75
357. LOAD 177 1D+0.75L+0.75LR+1E(O)+1P(O)+1TF+1TA+0.75I3+1SP+0.75WZ -
842. 1 0.72 5 0.72 8 0.72 10 0.9 11 0.9 17 1.6 23 0.3 26 1.0 27 0.3 30 1.0
843. LOAD 580 0.72D+0.72E(O)+0.72P(O)+0.9TF+0.9TA+1.6SP+0.3VX-+1VZ-+0.3VEX-+1VEZ -
844. REPEAT LOAD
845. 1 0.72 5 0.72 8 0.72 10 0.9 11 0.9 17 1.6 24 0.3 26 1.0 28 0.3 30 1.0
846. *===========*
847. * TEST *
848. *===========*
849. LOAD 581 1.4D+1.4E(T)+1.4P(T)+1.4WT
850. REPEAT LOAD
851. 1 1.4 6 1.4 9 1.4 18 1.4
852. LOAD 582 1.2D+1.6L+0.5LR+1.2E(T)+1.2P(T)+1.2WT
853. REPEAT LOAD
854. 1 1.2 2 1.6 3 0.5 6 1.2 9 1.2 18 1.2
855. LOAD 583 1.2D+1L+1.6LR+1.2E(T)+1.2P(T)+1.2WT
856. REPEAT LOAD
857. 1 1.2 2 1.0 3 1.6 6 1.2 9 1.2 18 1.2
858. LOAD 584 1.2D+1L+0.5LR+1.2E(T)+1.2P(T)+1.2WT+1.6WX+
859. REPEAT LOAD
860. 1 1.2 2 1.0 3 0.5 6 1.2 9 1.2 18 1.2 19 1.6
861. LOAD 585 1.2D+1L+0.5LR+1.2E(T)+1.2P(T)+1.2WT+1.6WX -
862. REPEAT LOAD
863. 1 1.2 2 1.0 3 0.5 6 1.2 9 1.2 18 1.2 20 1.6
864. LOAD 586 1.2D+1L+0.5LR+1.2E(T)+1.2P(T)+1.2WT+1.6WZ+
865. REPEAT LOAD
866. 1 1.2 2 1.0 3 0.5 6 1.2 9 1.2 18 1.2 21 1.6
867. LOAD 587 1.2D+1L+0.5LR+1.2E(T)+1.2P(T)+1.2WT+1.6WZ -
868. REPEAT LOAD
869. 1 1.2 2 1.0 3 0.5 6 1.2 9 1.2 18 1.2 22 1.6
870. LOAD 588 0.9D+0.9E(T)+0.9P(T)+0.9WT+1.6WX+
871. REPEAT LOAD
872. 1 0.9 6 0.9 9 0.9 18 0.9 19 1.6
873. LOAD 589 0.9D+0.9E(T)+0.9P(T)+0.9WT+1.6WX -
874. REPEAT LOAD
875. 1 0.9 6 0.9 9 0.9 18 0.9 20 1.6
876. LOAD 590 0.9D+0.9E(T)+0.9P(T)+0.9WT+1.6WZ+
877. REPEAT LOAD
878. 1 0.9 6 0.9 9 0.9 18 0.9 21 1.6
879. *========================*
880. * CONSTRUCTION LOAD *
881. *========================*
882. LOAD 591 0.9D+0.9E(T)+0.9P(T)+0.9WT+1.6WZ -
883. REPEAT LOAD
884. 1 0.9 6 0.9 9 0.9 18 0.9 22 1.6
885. LOAD 592 1.4D+1.4E(E)+1.4P(E)+1.6SP
886. REPEAT LOAD
887. 1 1.4 4 1.4 7 1.4 17 1.6
888. LOAD 593 1.2D+1.6L+0.5LR+1.2E(E)+1.2P(E)+1.6B+1.6I1+1.6SP
889. REPEAT LOAD
890. 1 1.2 2 1.6 3 0.5 4 1.2 7 1.2 13 1.6 17 1.6
891. LOAD 594 1.2D+1.6L+0.5LR+1.2E(E)+1.2P(E)+1.6B+1.6I2+1.6SP
892. REPEAT LOAD
893. 1 1.2 2 1.6 3 0.5 4 1.2 7 1.2 14 1.6 17 1.6
894. LOAD 595 1.2D+1.6L+0.5LR+1.2E(E)+1.2P(E)+1.6B+1.6I3+1.6SP
895. REPEAT LOAD
896. 1 1.2 2 1.6 3 0.5 4 1.2 7 1.2 15 1.6 17 1.6
897. LOAD 596 1.2D+1.6L+0.5LR+1.2E(E)+1.2P(E)+1.6B+1.6I4+1.6SP
994. PARAMETER 1
995. CODE AISC
996. LOAD LIST 501 TO 596
997. START CONCRETE DESIGN
--------------------------------------------------------
P0 Pn max P-bal. M-bal. e-bal. (MM)
23059.69 18447.76 7770.80 886.87 114.1
M0 P-tens. Des.Pn Des.Mn e/h
281.17 -2079.41 68.31 0.00 0.00000
--------------------------------------------------------
--------------------------------------------------------
P0 Pn max P-bal. M-bal. e-bal. (MM)
23059.69 18447.76 10307.06 10798.71 1047.7
M0 P-tens. Des.Pn Des.Mn e/h
2989.70 -2079.41 68.31 0.00 0.00000
--------------------------------------------------------
Pn Mn Pn Mn (@ Z )
| 17028.70 654.25 8514.35 894.46
P0 |* 15609.64 750.66 7095.29 858.15
| * 14190.58 820.69 5676.23 779.79
Pn,max|__* 12771.52 865.96 4257.17 679.03
| * 11352.46 891.70 2838.12 559.14
Pn | * 9933.41 900.24 1419.06 426.75
NOMINAL| * Pn Mn Pn Mn (@ Y )
AXIAL| * 17028.70 7244.51 8514.35 10523.55
COMPRESSION| * 15609.64 8351.39 7095.29 9981.71
Pb|-------*Mb 14190.58 9248.60 5676.23 9153.53
| * 12771.52 9954.54 4257.17 8039.01
___________|____*_______11352.46 10492.65 2838.12 6638.16
| * M0 Mn, 9933.41 10779.06 1419.06 4950.96
| * BENDING
P-tens|* MOMENT
|
--------------------------------------------------------
P0 Pn max P-bal. M-bal. e-bal. (MM)
23059.69 18447.76 7770.80 886.87 114.1
M0 P-tens. Des.Pn Des.Mn e/h
281.17 -2079.41 136.60 0.00 0.00000
--------------------------------------------------------
--------------------------------------------------------
P0 Pn max P-bal. M-bal. e-bal. (MM)
23059.69 18447.76 10307.06 10798.71 1047.7
M0 P-tens. Des.Pn Des.Mn e/h
2989.70 -2079.41 136.60 0.00 0.00000
--------------------------------------------------------
Pn Mn Pn Mn (@ Z )
| 17028.70 654.25 8514.35 894.46
P0 |* 15609.64 750.66 7095.29 858.15
| * 14190.58 820.69 5676.23 779.79
Pn,max|__* 12771.52 865.96 4257.17 679.03
| * 11352.46 891.70 2838.12 559.14
Pn | * 9933.41 900.24 1419.06 426.75
NOMINAL| * Pn Mn Pn Mn (@ Y )
AXIAL| * 17028.70 7244.51 8514.35 10523.55
COMPRESSION| * 15609.64 8351.39 7095.29 9981.71
Pb|-------*Mb 14190.58 9248.60 5676.23 9153.53
| * 12771.52 9954.54 4257.17 8039.01
___________|____*_______11352.46 10492.65 2838.12 6638.16
| * M0 Mn, 9933.41 10779.06 1419.06 4950.96
| * BENDING
P-tens|* MOMENT
|
--------------------------------------------------------
P0 Pn max P-bal. M-bal. e-bal. (MM)
23059.69 18447.76 7770.80 886.87 114.1
M0 P-tens. Des.Pn Des.Mn e/h
281.17 -2079.41 68.31 0.00 0.00000
--------------------------------------------------------
--------------------------------------------------------
P0 Pn max P-bal. M-bal. e-bal. (MM)
23059.69 18447.76 10307.06 10798.71 1047.7
M0 P-tens. Des.Pn Des.Mn e/h
2989.70 -2079.41 68.31 0.00 0.00000
--------------------------------------------------------
Pn Mn Pn Mn (@ Z )
| 17028.70 654.25 8514.35 894.46
P0 |* 15609.64 750.66 7095.29 858.15
| * 14190.58 820.69 5676.23 779.79
Pn,max|__* 12771.52 865.96 4257.17 679.03
| * 11352.46 891.70 2838.12 559.14
Pn | * 9933.41 900.24 1419.06 426.75
NOMINAL| * Pn Mn Pn Mn (@ Y )
AXIAL| * 17028.70 7244.51 8514.35 10523.55
COMPRESSION| * 15609.64 8351.39 7095.29 9981.71
Pb|-------*Mb 14190.58 9248.60 5676.23 9153.53
| * 12771.52 9954.54 4257.17 8039.01
___________|____*_______11352.46 10492.65 2838.12 6638.16
| * M0 Mn, 9933.41 10779.06 1419.06 4950.96
| * BENDING
P-tens|* MOMENT
|
1009. FINISH
************************************************************
* For technical assistance on STAAD.Pro, please visit *
* http://selectservices.bentley.com/en-US/ *
* *
* Details about additional assistance from *
* Bentley and Partners can be found at program menu *
* Help->Technical Support *
* *
* Copyright (c) 1997-2015 Bentley Systems, Inc.
* http://www.bentley.com *
************************************************************