Week 3 Challenge
Aim : To model the given I RCC girder bridge in Staad Pro and analyse it for IRS railway live loads.
Introduction : The given bridge is of RCC I girder type with length of bridge as 25m. The distance between piers along the bridge deck width is 26m.
Height of pier given is 10m.
The given bridge has 8 RCC I girders having flange of 0.7x0.2m and web of 0.2x1.8m. The centre to centre distance between girders is 3.714m.
The bridge will be analysed for IRS railway live load.
Procedure:
Step 1 - Modelling of the bridge in STaad pro with given details.
Open Staad pro and click on geometry tab in left, insert node details in the dialog box that pops up. X,Y,Z indicates Longitudinal,Vertical and Transverse axis respectively. Create 1st node at 0,0,0 and 2nd node at 0,10,0 since pier height is 10m.
Now click on support tab in the left menu bar and create fixed support then assign it to the bottom node of pier.
Click on property tab in the left and create circle property of concrete with diameter 2.5m and assign it to the pier.
Select the given pier and copy paste it to the distance of 26m in Z direction.
Click on geometry tab and select add beam from point to point and connect top nodes of pier.
Create the property of rectangle 2mx3m and assign it to the top beam. This is the pier cap.
Select the pier cap, right click and select insert nodes at 7 equal locations. Now we have points for 8 RCC I girders.
Now copy the entire frame and paste it at a distance of 25m as span length is 25m.
Connect the nodes of the top beam and assign property of I girder to them.
Model is ready.
Step 2 : Apply IRS railway live load.
Click on load and definition on the left tab and select vehicle definitions.
Input values of MG loading as per IRS bridge rules
Input width of vehicle for MG 1m
MG „C. CLASS LOADING - 1929 METRE GAUGE – 1000 mm
Beam number
Node Number
Results:
Maximum Axial force in Pier
Maximum bending moment in pier
Max Shear force in pier
Maximum forces for Girder
MAximum Bending moment
Maximum Shear force for girder
Maximum Fy support reaction
Maximum Moment
Report:
1. STAAD SPACE
INPUT FILE: Challenge 3.STD
2. START JOB INFORMATION
3. ENGINEER DATE 12-JUL-22
4. END JOB INFORMATION
5. INPUT WIDTH 79
6. UNIT METER KN
7. JOINT COORDINATES
8. 1 0 0 0; 2 0 10 0; 3 0 0 26; 4 0 10 26; 5 0 10 3.71429; 6 0 10 7.42857
9. 7 0 10 11.1429; 8 0 10 14.8571; 9 0 10 18.5714; 10 0 10 22.2857; 13 25 0 0
10. 14 25 10 0; 15 25 0 26; 16 25 10 26; 17 25 10 3.71429; 18 25 10 7.42857
11. 19 25 10 11.1429; 20 25 10 14.8571; 21 25 10 18.5714; 22 25 10 22.2857
12. MEMBER INCIDENCES
13. 1 1 2; 2 3 4; 3 2 5; 4 5 6; 5 6 7; 6 7 8; 7 8 9; 8 9 10; 9 10 4; 13 2 14
14. 15 4 16; 16 5 17; 17 6 18; 18 7 19; 19 8 20; 20 9 21; 21 10 22; 24 13 14
15. 25 15 16; 26 14 17; 27 17 18; 28 18 19; 29 19 20; 30 20 21; 31 21 22; 32 22 16
16. DEFINE MATERIAL START
17. ISOTROPIC CONCRETE
18. E 2.17185E+007
19. POISSON 0.17
20. DENSITY 23.5616
21. ALPHA 1E-005
22. DAMP 0.05
23. ISOTROPIC STEEL
24. E 2.05E+008
25. POISSON 0.3
26. DENSITY 76.8195
27. ALPHA 1.2E-005
28. DAMP 0.03
29. END DEFINE MATERIAL
30. MEMBER PROPERTY AMERICAN
31. 1 2 24 25 PRIS YD 2.5
32. 13 15 TO 21 TAPERED 2 0.2 2 0.7 0.2 0.7 0.2
33. 3 TO 9 26 TO 32 PRIS YD 2 ZD 3
34. CONSTANTS
35. MATERIAL CONCRETE ALL
36. SUPPORTS
37. 1 3 13 15 FIXED
38. DEFINE MOVING LOAD
39. TYPE 1 LOAD 44.6 44.6 44.6 44.6 44.6 44.6
40. DIST 0.914 0.914 3.048 0.914 0.914 WID 1
STAAD SPACE -- PAGE NO. 2
41. LOAD 1 LOADTYPE LIVE TITLE IRS MG LOADING
42. LOAD GENERATION 35 ADD LOAD 1
43. TYPE 1 -6.704 10 4.214 XINC 1
44. PERFORM ANALYSIS PRINT STATICS CHECK
P R O B L E M S T A T I S T I C S
-----------------------------------
NUMBER OF JOINTS/MEMBER+ELEMENTS/SUPPORTS = 20/ 26/ 4
SOLVER USED IS THE IN-CORE ADVANCED SOLVER
TOTAL PRIMARY LOAD CASES = 36, TOTAL DEGREES OF FREEDOM = 96
STAAD SPACE -- PAGE NO. 3
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 1
LOADTYPE LIVE TITLE IRS MG LOADING
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 1 )
SUMMATION FORCE-X = 0.0000000E+00
SUMMATION FORCE-Y = 0.0000000E+00
SUMMATION FORCE-Z = 0.0000000E+00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 0.0000000E+00 MY= 0.0000000E+00 MZ= 0.0000000E+00
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 1 )
SUMMATION FORCE-X = 0.0000000E+00
SUMMATION FORCE-Y = 0.0000000E+00
SUMMATION FORCE-Z = 0.0000000E+00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 0.0000000E+00 MY= 0.0000000E+00 MZ= 0.0000000E+00
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 1)
MAXIMUMS AT NODE
X = 0.00000E+00 0
Y = 0.00000E+00 0
Z = 0.00000E+00 0
RX= 0.00000E+00 0
RY= 0.00000E+00 0
RZ= 0.00000E+00 0
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 2
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.000000000E+00
Y = 0.100000003E+02
Z = 0.371408750E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 2 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -89.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 331.29 MY= 0.00 MZ= 0.00
STAAD SPACE -- PAGE NO. 4
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 2 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 89.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -331.29 MY= 0.00 MZ= 0.00
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 2)
MAXIMUMS AT NODE
X = -5.67179E-04 2
Y = -1.06269E-02 6
Z = 3.57125E-03 2
RX= 1.44995E-05 2
RY= 8.38801E-08 7
RZ= 2.03758E-06 19
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 3
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.588427922E-01
Y = 0.100000003E+02
Z = 0.371400009E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 3 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -178.40
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 662.58 MY= 0.00 MZ= -96.87
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 3 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 178.40
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -662.58 MY= 0.00 MZ= 96.87
STAAD SPACE -- PAGE NO. 5
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 3)
MAXIMUMS AT NODE
X = 7.80938E-04 2
Y = -2.08283E-02 6
Z = 6.67229E-03 2
RX= 2.81864E-05 5
RY= -6.44841E-07 2
RZ= -6.28670E-06 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 4
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.198454270E+00
Y = 0.100000003E+02
Z = 0.371400006E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 4 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -267.60
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 993.87 MY= 0.00 MZ= -290.61
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 4 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 267.60
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -993.87 MY= 0.00 MZ= 290.61
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 4)
MAXIMUMS AT NODE
X = 3.61633E-03 2
Y = -3.07044E-02 6
Z = 9.90625E-03 2
RX= 4.15459E-05 5
RY= -2.00433E-06 2
RZ= -2.21993E-05 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 5
STAAD SPACE -- PAGE NO. 6
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.548799884E+00
Y = 0.100000003E+02
Z = 0.371400009E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 5 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -267.60
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 993.87 MY= 0.00 MZ= -558.21
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 5 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 267.60
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -993.87 MY= 0.00 MZ= 558.21
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 5)
MAXIMUMS AT NODE
X = 7.63045E-03 2
Y = -2.96811E-02 6
Z = 9.69152E-03 2
RX= 4.01524E-05 5
RY= -3.75680E-06 2
RZ= -4.38850E-05 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 6
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.109909446E+01
Y = 0.100000003E+02
Z = 0.371400010E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 6 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -267.60
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 993.87 MY= 0.00 MZ= -825.81
STAAD SPACE -- PAGE NO. 7
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 6 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 267.60
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -993.87 MY= 0.00 MZ= 825.81
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 6)
MAXIMUMS AT NODE
X = 1.05950E-02 2
Y = -2.85885E-02 6
Z = 9.41984E-03 2
RX= 3.86681E-05 5
RY= -5.16897E-06 2
RZ= -6.16095E-05 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 7
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.137306305E+01
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 7 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -356.80
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1325.16 MY= 0.00 MZ= -1104.47
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 7 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 356.80
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1325.16 MY= 0.00 MZ= 1104.47
STAAD SPACE -- PAGE NO. 8
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 7)
MAXIMUMS AT NODE
X = 1.22781E-02 2
Y = -3.79798E-02 6
Z = 1.24543E-02 2
RX= 5.13757E-05 5
RY= -6.29312E-06 2
RZ= -7.51796E-05 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 8
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.166410286E+01
Y = 0.100000003E+02
Z = 0.371400007E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 8 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -446.00
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1656.44 MY= 0.00 MZ= -1480.01
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 8 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 446.00
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1656.44 MY= 0.00 MZ= 1480.01
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 8)
MAXIMUMS AT NODE
X = 1.49587E-02 2
Y = -4.69716E-02 6
Z = 1.53870E-02 2
RX= 6.35405E-05 5
RY= -7.89039E-06 2
RZ= -9.46918E-05 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 9
STAAD SPACE -- PAGE NO. 9
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.199402822E+01
Y = 0.100000003E+02
Z = 0.371400010E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 9 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -1952.41
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 9 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 1952.41
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 9)
MAXIMUMS AT NODE
X = 1.83144E-02 2
Y = -5.55426E-02 6
Z = 1.82008E-02 2
RX= 7.51350E-05 5
RY= -9.85244E-06 2
RZ= -1.18876E-04 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 10
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.276116397E+01
Y = 0.100000003E+02
Z = 0.371400007E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 10 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -2487.61
STAAD SPACE -- PAGE NO. 10
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 10 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 2487.61
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 10)
MAXIMUMS AT NODE
X = 2.19086E-02 2
Y = -5.32070E-02 6
Z = 1.75339E-02 2
RX= 7.19691E-05 5
RY= -1.18601E-05 2
RZ= -1.44684E-04 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 11
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.367905834E+01
Y = 0.100000003E+02
Z = 0.371400010E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 11 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -3022.81
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 11 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 3022.81
STAAD SPACE -- PAGE NO. 11
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 11)
MAXIMUMS AT NODE
X = 2.38899E-02 2
Y = -5.07668E-02 6
Z = 1.67812E-02 2
RX= 6.86660E-05 5
RY= -1.33142E-05 2
RZ= -1.63977E-04 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 12
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.472851141E+01
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 12 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -3558.01
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 12 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 3558.01
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 12)
MAXIMUMS AT NODE
X = 2.44482E-02 2
Y = -4.82353E-02 6
Z = 1.59536E-02 2
RX= 6.52432E-05 5
RY= -1.42642E-05 2
RZ= -1.77306E-04 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 13
STAAD SPACE -- PAGE NO. 12
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.589032161E+01
Y = 0.100000003E+02
Z = 0.371400006E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 13 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -4093.21
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 13 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 4093.21
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 13)
MAXIMUMS AT NODE
X = 2.37733E-02 2
Y = -4.56259E-02 6
Z = 1.50620E-02 2
RX= 6.17183E-05 5
RY= -1.47596E-05 2
RZ= -1.85220E-04 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 14
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.714529107E+01
Y = 0.100000003E+02
Z = 0.371400009E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 14 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -4628.41
STAAD SPACE -- PAGE NO. 13
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 14 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 4628.41
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 14)
MAXIMUMS AT NODE
X = 2.20552E-02 2
Y = -4.29520E-02 6
Z = 1.41173E-02 2
RX= 5.81087E-05 5
RY= -1.48502E-05 2
RZ= -1.88269E-04 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 15
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.847421932E+01
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 15 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -5163.61
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 15 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 5163.61
STAAD SPACE -- PAGE NO. 14
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 15)
MAXIMUMS AT NODE
X = 1.94836E-02 2
Y = -4.02267E-02 6
Z = 1.31305E-02 2
RX= 5.44317E-05 5
RY= -1.45853E-05 2
RZ= -1.87002E-04 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 16
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.985790598E+01
Y = 0.100000003E+02
Z = 0.371400010E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 16 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -5698.81
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 16 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 5698.81
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 16)
MAXIMUMS AT NODE
X = 1.62484E-02 2
Y = -3.74634E-02 6
Z = 1.21125E-02 2
RX= 5.07050E-05 5
RY= -1.40145E-05 2
RZ= -1.81970E-04 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 17
STAAD SPACE -- PAGE NO. 15
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.112771512E+02
Y = 0.100000003E+02
Z = 0.371400010E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 17 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -6234.01
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 17 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 6234.01
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 17)
MAXIMUMS AT NODE
X = 1.25394E-02 2
Y = -3.46755E-02 6
Z = 1.10742E-02 2
RX= 4.69460E-05 5
RY= -1.31875E-05 2
RZ= -1.73722E-04 5
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 18
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.127127532E+02
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 18 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -6769.21
STAAD SPACE -- PAGE NO. 16
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 18 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 6769.21
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 18)
MAXIMUMS AT NODE
X = -9.74678E-03 14
Y = -3.27052E-02 18
Z = 1.03371E-02 14
RX= 4.42896E-05 17
RY= 1.24783E-05 14
RZ= 1.66283E-04 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 19
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.141455149E+02
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 19 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -7304.41
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 19 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 7304.41
STAAD SPACE -- PAGE NO. 17
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 19)
MAXIMUMS AT NODE
X = -1.36754E-02 14
Y = -3.55025E-02 18
Z = 1.13830E-02 14
RX= 4.80610E-05 17
RY= 1.34561E-05 14
RZ= 1.76466E-04 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 20
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.155562355E+02
Y = 0.100000003E+02
Z = 0.371400010E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 20 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -7839.61
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 20 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 7839.61
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 20)
MAXIMUMS AT NODE
X = -1.72639E-02 14
Y = -3.82845E-02 18
Z = 1.24164E-02 14
RX= 5.18123E-05 17
RY= 1.42124E-05 14
RZ= 1.83820E-04 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 21
STAAD SPACE -- PAGE NO. 18
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.169257130E+02
Y = 0.100000003E+02
Z = 0.371400009E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 21 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -8374.81
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 21 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 8374.81
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 21)
MAXIMUMS AT NODE
X = -2.03225E-02 14
Y = -4.10379E-02 18
Z = 1.34263E-02 14
RX= 5.55261E-05 17
RY= 1.46978E-05 14
RZ= 1.87794E-04 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 22
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.182347502E+02
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 22 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -8910.01
STAAD SPACE -- PAGE NO. 19
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 22 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 8910.01
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 22)
MAXIMUMS AT NODE
X = -2.26612E-02 14
Y = -4.37494E-02 18
Z = 1.44018E-02 14
RX= 5.91849E-05 17
RY= 1.48626E-05 14
RZ= 1.87841E-04 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 23
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.194641451E+02
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 23 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -9445.21
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 23 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 9445.21
STAAD SPACE -- PAGE NO. 20
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 23)
MAXIMUMS AT NODE
X = -2.40903E-02 14
Y = -4.64057E-02 18
Z = 1.53319E-02 14
RX= 6.27713E-05 17
RY= 1.46574E-05 14
RZ= 1.83409E-04 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 24
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.205946968E+02
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 24 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -9980.41
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 24 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 9980.41
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 24)
MAXIMUMS AT NODE
X = -2.44199E-02 14
Y = -4.89933E-02 18
Z = 1.62057E-02 14
RX= 6.62678E-05 17
RY= 1.40326E-05 14
RZ= 1.73950E-04 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 25
STAAD SPACE -- PAGE NO. 21
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.216072105E+02
Y = 0.100000003E+02
Z = 0.371400007E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 25 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -10515.61
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 25 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 10515.61
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 25)
MAXIMUMS AT NODE
X = -2.34602E-02 14
Y = -5.14992E-02 18
Z = 1.70123E-02 14
RX= 6.96569E-05 17
RY= 1.29385E-05 14
RZ= 1.58913E-04 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 26
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.224824795E+02
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 26 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -11050.81
STAAD SPACE -- PAGE NO. 22
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 26 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 11050.81
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 26)
MAXIMUMS AT NODE
X = -2.10213E-02 14
Y = -5.39098E-02 18
Z = 1.77407E-02 14
RX= 7.29213E-05 17
RY= 1.13258E-05 14
RZ= 1.37748E-04 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 27
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.232013082E+02
Y = 0.100000003E+02
Z = 0.371401465E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 27 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1987.73 MY= 0.00 MZ= -11586.01
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 27 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 535.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1987.73 MY= 0.00 MZ= 11586.01
STAAD SPACE -- PAGE NO. 23
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 27)
MAXIMUMS AT NODE
X = -1.69112E-02 14
Y = -5.62546E-02 18
Z = 1.85888E-02 14
RX= 7.61031E-05 17
RY= 9.14185E-06 14
RZ= 1.09902E-04 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 28
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.231477663E+02
Y = 0.100000003E+02
Z = 0.371400010E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 28 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -356.80
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 1325.16 MY= 0.00 MZ= -7564.34
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 28 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 356.80
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -1325.16 MY= 0.00 MZ= 7564.34
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 28)
MAXIMUMS AT NODE
X = -1.44065E-02 14
Y = -3.69118E-02 18
Z = 1.21645E-02 14
RX= 4.99267E-05 17
RY= 7.39427E-06 14
RZ= 8.91768E-05 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 29
STAAD SPACE -- PAGE NO. 24
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.234039469E+02
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 29 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -267.60
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 993.87 MY= 0.00 MZ= -5675.80
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 29 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 267.60
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -993.87 MY= 0.00 MZ= 5675.80
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 29)
MAXIMUMS AT NODE
X = -1.21037E-02 14
Y = -2.77813E-02 18
Z = 9.19739E-03 14
RX= 3.75732E-05 17
RY= 5.97242E-06 14
RZ= 7.18601E-05 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 30
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.240834887E+02
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 30 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -267.60
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 993.87 MY= 0.00 MZ= -5943.40
STAAD SPACE -- PAGE NO. 25
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 30 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 267.60
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -993.87 MY= 0.00 MZ= 5943.40
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 30)
MAXIMUMS AT NODE
X = -9.82122E-03 14
Y = -2.89187E-02 18
Z = 9.50587E-03 14
RX= 3.91164E-05 17
RY= 4.78495E-06 14
RZ= 5.67595E-05 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 31
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.245765994E+02
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 31 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -267.60
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 993.87 MY= 0.00 MZ= -6211.00
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 31 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 267.60
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -993.87 MY= 0.00 MZ= 6211.00
STAAD SPACE -- PAGE NO. 26
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 31)
MAXIMUMS AT NODE
X = -6.55590E-03 14
Y = -2.99915E-02 18
Z = 9.76126E-03 14
RX= 4.05748E-05 17
RY= 3.27463E-06 14
RZ= 3.78911E-05 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 32
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.247970417E+02
Y = 0.100000003E+02
Z = 0.371400008E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 32 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -178.40
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 662.58 MY= 0.00 MZ= -4237.53
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 32 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 178.40
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -662.58 MY= 0.00 MZ= 4237.53
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 32)
MAXIMUMS AT NODE
X = -3.02264E-03 14
Y = -2.03717E-02 18
Z = 6.59097E-03 14
RX= 2.75634E-05 17
RY= 1.58222E-06 14
RZ= 1.77994E-05 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 33
STAAD SPACE -- PAGE NO. 27
CENTER OF FORCE BASED ON Y FORCES ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS WILL INVALIDATE RESULTS)
X = 0.249416418E+02
Y = 0.100000003E+02
Z = 0.371400009E+01
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 33 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = -89.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 331.29 MY= 0.00 MZ= -2167.20
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 33 )
SUMMATION FORCE-X = 0.00
SUMMATION FORCE-Y = 89.20
SUMMATION FORCE-Z = 0.00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= -331.29 MY= 0.00 MZ= 2167.20
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 33)
MAXIMUMS AT NODE
X = -7.04929E-04 14
Y = -1.03658E-02 18
Z = 3.33002E-03 14
RX= 1.40270E-05 17
RY= 4.48055E-07 14
RZ= 4.67364E-06 17
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 34
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 34 )
SUMMATION FORCE-X = 0.0000000E+00
SUMMATION FORCE-Y = 0.0000000E+00
SUMMATION FORCE-Z = 0.0000000E+00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 0.0000000E+00 MY= 0.0000000E+00 MZ= 0.0000000E+00
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 34 )
SUMMATION FORCE-X = 0.0000000E+00
SUMMATION FORCE-Y = 0.0000000E+00
SUMMATION FORCE-Z = 0.0000000E+00
STAAD SPACE -- PAGE NO. 28
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 0.0000000E+00 MY= 0.0000000E+00 MZ= 0.0000000E+00
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 34)
MAXIMUMS AT NODE
X = 0.00000E+00 0
Y = 0.00000E+00 0
Z = 0.00000E+00 0
RX= 0.00000E+00 0
RY= 0.00000E+00 0
RZ= 0.00000E+00 0
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 35
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 35 )
SUMMATION FORCE-X = 0.0000000E+00
SUMMATION FORCE-Y = 0.0000000E+00
SUMMATION FORCE-Z = 0.0000000E+00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 0.0000000E+00 MY= 0.0000000E+00 MZ= 0.0000000E+00
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 35 )
SUMMATION FORCE-X = 0.0000000E+00
SUMMATION FORCE-Y = 0.0000000E+00
SUMMATION FORCE-Z = 0.0000000E+00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 0.0000000E+00 MY= 0.0000000E+00 MZ= 0.0000000E+00
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 35)
MAXIMUMS AT NODE
X = 0.00000E+00 0
Y = 0.00000E+00 0
Z = 0.00000E+00 0
RX= 0.00000E+00 0
RY= 0.00000E+00 0
RZ= 0.00000E+00 0
STATIC LOAD/REACTION/EQUILIBRIUM SUMMARY FOR CASE NO. 36
***TOTAL APPLIED LOAD ( KN METE ) SUMMARY (LOADING 36 )
SUMMATION FORCE-X = 0.0000000E+00
SUMMATION FORCE-Y = 0.0000000E+00
SUMMATION FORCE-Z = 0.0000000E+00
STAAD SPACE -- PAGE NO. 29
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 0.0000000E+00 MY= 0.0000000E+00 MZ= 0.0000000E+00
***TOTAL REACTION LOAD( KN METE ) SUMMARY (LOADING 36 )
SUMMATION FORCE-X = 0.0000000E+00
SUMMATION FORCE-Y = 0.0000000E+00
SUMMATION FORCE-Z = 0.0000000E+00
SUMMATION OF MOMENTS AROUND THE ORIGIN-
MX= 0.0000000E+00 MY= 0.0000000E+00 MZ= 0.0000000E+00
MAXIMUM DISPLACEMENTS ( CM /RADIANS) (LOADING 36)
MAXIMUMS AT NODE
X = 0.00000E+00 0
Y = 0.00000E+00 0
Z = 0.00000E+00 0
RX= 0.00000E+00 0
RY= 0.00000E+00 0
RZ= 0.00000E+00 0
45. FINISH