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Section 2
2-53
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1. STAAD PLANE VERIFICATION PROBLEM FOR AASHTO CODE
2. *
3. * THIS DESIGN EXAMPLE IS VERIFIED BY HAND CALCULATION
4. * FOLLOWING AASHTO ASD 97 CODE.
5. *
6. UNIT FEET KIP
7. JOINT COORD
8. 1 0 0 ; 2 25 0 ; 3 0 10 ; 4 25 11
9. 5 0 15 ; 6 25 15 ; 7 5 15 ; 8 21 15
11. MEMB INCI
12. 1 1 3 ; 2 3 5 ; 3 2 4 ; 4 4 6
13. 5 5 7 ; 6 7 8 ; 7 8 6 ; 8 3 7 ; 9 4 8
15. MEMB PROP AMERICAN
16. 1 2 TA ST W12X26 ; 3 4 TA ST W14X43
17. 5 6 7 TA ST W16X36 ; 8 TA ST L40404 ; 9 TA ST L50506
19. MEMB TRUSS ; 8 9
21. CONSTANT
22. E 4176E3 ALL
23. POISSON STEEL ALL
24. SUPPORT ; 1 2 PINNED
26. LOADING 1 DL + LL
27. MEMB LOAD ; 5 6 7 UNI Y -2.0
29. LOADING 2 WIND FROM LEFT
30. JOINT LOAD ; 5 FX 15.
31. LOAD COMB 3 ; 1 0.75 2 0.75
33. PERFORM ANALYSIS
P R O B L E M S T A T I S T I C S
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NUMBER OF JOINTS/MEMBER+ELEMENTS/SUPPORTS = 8/ 9/ 2
ORIGINAL/FINAL BAND-WIDTH= 4/ 4/ 15 DOF
TOTAL PRIMARY LOAD CASES = 2, TOTAL DEGREES OF FREEDOM = 20
SIZE OF STIFFNESS MATRIX = 1 DOUBLE KILO-WORDS
REQRD/AVAIL. DISK SPACE = 12.0/ 19214.5 MB
34. LOAD LIST 1 3