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INDEX S.N o TOPIC Sign. Remark s 1 ANALYSE THE CONTINUOUS BEAM BY FEM 2 ANALYSE THE CONTINUOUS BEAM BY FEM ( 1 INTERNAL NODE EACH MEMBER) 3 ANALYSE THE CONTINUOUS BEAM BY FEM ( 2 INTERNAL NODES EACH MEMBER) 4 ANALYSE THE TRUSS BY FEM 5 ANALYSE THE TRUSS BY FEM( 1INTERNAL NODE EACH MEMBER) 6 ANALYSE THE TRUSS BY FEM( 2 INTERNAL NODES IN EACH MEMBER) 7 ANALYSE THE PLANE FRAME BY FEM 8 ANALYSE THE PLANE FRAME BY FEM( 1 INTERNAL NODES IN EACH MEMBER) 9 ANALYSE THE PLANE FRAME BY FEM( 2 INTERNAL NODES IN EACH MEMBER) 10 ANALYSE THE SPACE TRUSS 11 ANALYSE THE GRID STRUCTURE 12 ANALYSE THE COMMERCIAL BUILDING (G+12) SUBJECTED TO EARTHQUAKE 13 ANALYSE THE COMMERCIAL BUILDING (G+12) SUBJECTED TO WIND FORCE
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Project File- Finite Element

Dec 19, 2015

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Ankur Dubey

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Page 1: Project File- Finite Element

INDEX

S.No

TOPIC Sign. Remarks

1 ANALYSE THE CONTINUOUS BEAM BY FEM

2 ANALYSE THE CONTINUOUS BEAM BY FEM ( 1 INTERNAL NODE EACH MEMBER)

3 ANALYSE THE CONTINUOUS BEAM BY FEM ( 2 INTERNAL NODES EACH MEMBER)

4 ANALYSE THE TRUSS BY FEM

5 ANALYSE THE TRUSS BY FEM( 1INTERNAL NODE EACH MEMBER)

6 ANALYSE THE TRUSS BY FEM( 2 INTERNAL NODES IN EACH MEMBER)

7 ANALYSE THE PLANE FRAME BY FEM

8 ANALYSE THE PLANE FRAME BY FEM( 1 INTERNAL NODES IN EACH MEMBER)

9 ANALYSE THE PLANE FRAME BY FEM( 2 INTERNAL NODES IN EACH MEMBER)

10 ANALYSE THE SPACE TRUSS

11 ANALYSE THE GRID STRUCTURE

12 ANALYSE THE COMMERCIAL BUILDING (G+12) SUBJECTED TO EARTHQUAKE

13 ANALYSE THE COMMERCIAL BUILDING (G+12) SUBJECTED TO WIND FORCE

Page 2: Project File- Finite Element

EXPERIMENT-1

OBJECTIVE: ANALYSE THE CONTINUOUS BEAM BY FEM

FIG -1

The Length of beam is 6 m.

In this practical, the beam has no internal node.

Load of 30 kN/m is acting on the beam of span 6m each with element of length 6m each.

Total number of nodes = 3Total number of Elements = 2

Page 3: Project File- Finite Element

FIG -2. SHEAR FORCE DIAGRAM

FIG 3. BENDING MOMENT DIAGRAM

Page 4: Project File- Finite Element

OUTPUT :

**************************************************** * * * STAAD.Pro V8i SELECTseries5 * * Version 20.07.10.65 * * Proprietary Program of * * Bentley Systems, Inc. * * Date= APR 30, 2015 * * Time= 4: 0:22 * * * * USER ID: * ****************************************************

1. STAAD PLANEINPUT FILE: Q-1.STD 2. START JOB INFORMATION 3. ENGINEER DATE 27-APR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 2 6 0 0; 3 12 0 0 9. MEMBER INCIDENCES 10. 1 1 2; 2 2 3 11. CONSTANTS 12. E 100 ALL 14. MEMBER PROPERTY 15. 1 2 PRIS YD 1 ZD 12 16. SUPPORTS 17. 1 FIXED 18. 2 3 FIXED BUT FX MZ 19. LOAD 1 20. MEMBER LOAD 21. 1 2 UNI GY -30 22. PERFORM ANALYSIS

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

NUMBER OF JOINTS 3 NUMBER OF MEMBERS 2 NUMBER OF PLATES 0 NUMBER OF SOLIDS 0 NUMBER OF SURFACES 0 NUMBER OF SUPPORTS 3

SOLVER USED IS THE IN-CORE ADVANCED SOLVER TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 4 TOTAL LOAD COMBINATION CASES = 0 SO FAR.

23. LOAD LIST 1 24. PRINT ANALYSIS RESULTS ANALYSIS RESULTS

Page 5: Project File- Finite Element
Page 6: Project File- Finite Element

JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = PLANE ------------------

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 1 0.0000 0.0000 0.0000 0.0000 0.0000 -0.3766 3 1 0.0000 0.0000 0.0000 0.0000 0.0000 1.6190

SUPPORT REACTIONS -UNIT KN METE STRUCTURE TYPE = PLANE -----------------

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

1 1 0.00 84.27 0.00 0.00 0.00 79.08 2 1 0.00 204.65 0.00 0.00 0.00 0.00 3 1 0.00 71.09 0.00 0.00 0.00 0.00

MEMBER END FORCES STRUCTURE TYPE = PLANE ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

1 1 1 0.00 84.27 0.00 0.00 0.00 79.08 2 0.00 95.73 0.00 0.00 0.00 -113.48

2 1 2 0.00 108.91 0.00 0.00 0.00 113.48 3 0.00 71.09 0.00 0.00 0.00 0.00

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

25. FINISH

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

Page 7: Project File- Finite Element

EXPERIMENT-2

OBJECTIVE: ANALYSE THE CONTINUOUS BEAM BY FEM ( 1 INTERNAL NODE IN EACH BEAM)

FIG 4.

The beam has been provided one internal node at the midpoint.

Load of 30 kN/m is acting on the beam of span 6m each with element of length 3m each.

Total number of nodes = 5Total number of Elements = 4

Page 8: Project File- Finite Element

Fig 5. Bending Moment Diagram

Fig 6. Shear Force Diagram

Page 9: Project File- Finite Element

OUTPUT :

**************************************************** * * * STAAD.Pro V8i SELECTseries5 * * Version 20.07.10.65 * * Proprietary Program of * * Bentley Systems, Inc. * * Date= APR 30, 2015 * * Time= 4: 6:13 * * * * USER ID: * ****************************************************

1. STAAD PLANEINPUT FILE: Q-2.STD 2. START JOB INFORMATION 3. ENGINEER DATE 27-APR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 2 6 0 0; 3 12 0 0; 4 3 0 0; 5 9 0 0 9. MEMBER INCIDENCES 10. 1 1 4; 2 2 5; 3 4 2; 4 5 3 11. DEFINE MATERIAL START 12. ISOTROPIC MATERIAL1 13. E 100 14. POISSON 0.45 15. END DEFINE MATERIAL 16. CONSTANTS 17. MATERIAL MATERIAL1 ALL 18. MEMBER PROPERTY AMERICAN 19. 1 TO 4 PRIS YD 1 ZD 12 20. SUPPORTS 21. 1 FIXED 22. 2 3 FIXED BUT FX MZ 23. LOAD 1 24. MEMBER LOAD 25. 1 TO 4 UNI GY -30 26. PERFORM ANALYSIS

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

NUMBER OF JOINTS 5 NUMBER OF MEMBERS 4 NUMBER OF PLATES 0 NUMBER OF SOLIDS 0 NUMBER OF SURFACES 0 NUMBER OF SUPPORTS 3

SOLVER USED IS THE IN-CORE ADVANCED SOLVER TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 10 TOTAL LOAD COMBINATION CASES = 0 SO FAR.

Page 10: Project File- Finite Element

27. LOAD LIST 1 28. PRINT ANALYSIS RESULTS ANALYSIS RESULTS

JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = PLANE ------------------

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 1 0.0000 0.0000 0.0000 0.0000 0.0000 -0.3766 3 1 0.0000 0.0000 0.0000 0.0000 0.0000 1.6190 4 1 0.0000 -111.3842 0.0000 0.0000 0.0000 0.0697 5 1 0.0000 -289.3040 0.0000 0.0000 0.0000 -0.2299

SUPPORT REACTIONS -UNIT KN METE STRUCTURE TYPE = PLANE -----------------

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

1 1 0.00 84.27 0.00 0.00 0.00 79.08 2 1 0.00 204.65 0.00 0.00 0.00 0.00 3 1 0.00 71.09 0.00 0.00 0.00 0.00

MEMBER END FORCES STRUCTURE TYPE = PLANE ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

1 1 1 0.00 84.27 0.00 0.00 0.00 79.08 4 0.00 5.73 0.00 0.00 0.00 38.72

2 1 2 0.00 108.91 0.00 0.00 0.00 113.48 5 0.00 -18.91 0.00 0.00 0.00 78.26

3 1 4 0.00 -5.73 0.00 0.00 0.00 -38.72 2 0.00 95.73 0.00 0.00 0.00 -113.48

4 1 5 0.00 18.91 0.00 0.00 0.00 -78.26 3 0.00 71.09 0.00 0.00 0.00 0.00

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

29. FINISH

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

Page 11: Project File- Finite Element

EXPERIMENT-3

OBJECTIVE: ANALYSE THE CONTINUOUS BEAM BY FEM ( 2 INTERNAL NODE IN EACH BEAM)

Fig 7.

The beam has been provided two internal nodes at the equal intervals.

Load of 30 kN/m is acting on the beam of span 6m each with element of length 2m each.

Total number of nodes = 7Total number of Elements = 6

Page 12: Project File- Finite Element

Fig .8 Bending Moment Diagram

Fig .9 Shear Force Diagram

Page 13: Project File- Finite Element

OUTPUT :

**************************************************** * * * STAAD.Pro V8i SELECTseries5 * * Version 20.07.10.65 * * Proprietary Program of * * Bentley Systems, Inc. * * Date= APR 30, 2015 * * Time= 4:11:10 * * * * USER ID: * ****************************************************

1. STAAD PLANEINPUT FILE: Q-3.STD 2. START JOB INFORMATION 3. ENGINEER DATE 27-APR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 2 6 0 0; 3 12 0 0; 4 2 0 0; 5 4 0 0; 6 8 0 0; 7 10 0 0 9. MEMBER INCIDENCES 10. 1 1 4; 2 2 6; 3 4 5; 4 5 2; 5 6 7; 6 7 3 11. DEFINE MATERIAL START 12. ISOTROPIC MATERIAL1 13. E 100 14. POISSON 0.45 15. END DEFINE MATERIAL 16. CONSTANTS 17. MATERIAL MATERIAL1 ALL 18. MEMBER PROPERTY AMERICAN 19. 1 TO 6 PRIS YD 1 ZD 12 20. SUPPORTS 21. 1 FIXED 22. 2 3 FIXED BUT FX MZ 23. LOAD 1 24. MEMBER LOAD 25. 1 TO 6 UNI GY -30 26. PERFORM ANALYSIS P R O B L E M S T A T I S T I C S -----------------------------------

NUMBER OF JOINTS 7 NUMBER OF MEMBERS 6 NUMBER OF PLATES 0 NUMBER OF SOLIDS 0 NUMBER OF SURFACES 0 NUMBER OF SUPPORTS 3

SOLVER USED IS THE IN-CORE ADVANCED SOLVER TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 16 TOTAL LOAD COMBINATION CASES = 0 SO FAR.

27. LOAD LIST 1 28. PRINT ANALYSIS RESULTS ANALYSIS RESULTS

Page 14: Project File- Finite Element

JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = PLANE ------------------

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 1 0.0000 0.0000 0.0000 0.0000 0.0000 -0.3766 3 1 0.0000 0.0000 0.0000 0.0000 0.0000 1.6190 4 1 0.0000 -96.6534 0.0000 0.0000 0.0000 -0.2962 5 1 0.0000 -81.3629 0.0000 0.0000 0.0000 0.3783 6 1 0.0000 -221.9415 0.0000 0.0000 0.0000 -0.8680 7 1 0.0000 -272.3767 0.0000 0.0000 0.0000 0.5972

SUPPORT REACTIONS -UNIT KN METE STRUCTURE TYPE = PLANE -----------------

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

1 1 0.00 84.27 0.00 0.00 0.00 79.08 2 1 0.00 204.65 0.00 0.00 0.00 0.00 3 1 0.00 71.09 0.00 0.00 0.00 0.00

MEMBER END FORCES STRUCTURE TYPE = PLANE ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

1 1 1 0.00 84.27 0.00 0.00 0.00 79.08 4 0.00 -24.27 0.00 0.00 0.00 29.46

2 1 2 0.00 108.91 0.00 0.00 0.00 113.48 6 0.00 -48.91 0.00 0.00 0.00 44.35

3 1 4 0.00 24.27 0.00 0.00 0.00 -29.46 5 0.00 35.73 0.00 0.00 0.00 17.99

4 1 5 0.00 -35.73 0.00 0.00 0.00 -17.99 2 0.00 95.73 0.00 0.00 0.00 -113.48

5 1 6 0.00 48.91 0.00 0.00 0.00 -44.35 7 0.00 11.09 0.00 0.00 0.00 82.17

6 1 7 0.00 -11.09 0.00 0.00 0.00 -82.17 3 0.00 71.09 0.00 0.00 0.00 0.00

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

29. FINISH

Page 15: Project File- Finite Element

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

Page 16: Project File- Finite Element

EXPERIMENT-4

OBJECTIVE: ANALYSE THE TRUSS BY FEM

Fig. 10

The truss is subjected to vertical downward load of 8 kN at node 3 and horizontal force of 4 kN at node 4.In the present practical , the members have no internal node.

Total number of nodes = 4Total number of Elements = 6

Page 17: Project File- Finite Element

Fig 11. Joint displacement of truss

Page 18: Project File- Finite Element

Output :

**************************************************** * * * STAAD.Pro V8i SELECTseries5 * * Version 20.07.10.65 * * Proprietary Program of * * Bentley Systems, Inc. * * Date= APR 30, 2015 * * Time= 4:14:42 * * * * USER ID: * ****************************************************

1. STAAD TRUSSINPUT FILE: Q-4.STD 2. START JOB INFORMATION 3. ENGINEER DATE 27-APR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 2 5 0 0; 3 0 3 0; 4 5 3 0 9. MEMBER INCIDENCES 10. 1 1 2; 2 2 4; 3 1 4; 4 3 4; 5 3 1; 6 3 2 11. CONSTANTS 12. E 100 ALL 13. MEMBER PROPERTY 14. 1 TO 6 PRIS AX 1 AY 1 AZ 1 15. SUPPORTS 16. 1 2 PINNED 17. LOAD 1 18. JOINT LOAD 19. 3 FY -8 20. 4 FX 4 21. LOAD LIST 1

**WARNING: A LOAD LIST COMMAND WITHIN LOAD DATA IGNORED. **

22. PERFORM ANALYSIS

**WARNING** THE POISSON'S RATIO HAS NOT BEEN SPECIFIED FOR ONE OR MORE MEMBERS/ELEMENTS/SOLIDS. THE DEFAULT VALUE HAS BEEN SET FOR THE SAME.

** WARNING ** A SOFT MATERIAL WITH (1.0 / 2.172E+05) TIMES THE STIFFNESS OF CONCRETE ENTERED. PLEASE CHECK.

Page 19: Project File- Finite Element

STAAD TRUSS -- PAGE NO. 2

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

NUMBER OF JOINTS 4 NUMBER OF MEMBERS 6 NUMBER OF PLATES 0 NUMBER OF SOLIDS 0 NUMBER OF SURFACES 0 NUMBER OF SUPPORTS 2

SOLVER USED IS THE IN-CORE ADVANCED SOLVER TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 4 TOTAL LOAD COMBINATION CASES = 0 SO FAR.

23. PRINT ANALYSIS RESULTS ANALYSIS RESULTS

JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = TRUSS ------------------

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 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 3 1 5.3423 -20.0560 0.0000 0.0000 0.0000 0.0000 4 1 16.2980 -3.2560 0.0000 0.0000 0.0000 0.0000

SUPPORT REACTIONS -UNIT KN METE STRUCTURE TYPE = TRUSS -----------------

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

1 1 -1.81 5.60 0.00 0.00 0.00 0.00 2 1 -2.19 2.40 0.00 0.00 0.00 0.00

MEMBER END FORCES STRUCTURE TYPE = TRUSS ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

1 1 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

2 1 2 1.09 0.00 0.00 0.00 0.00 0.00 4 -1.09 0.00 0.00 0.00 0.00 0.00

Page 20: Project File- Finite Element

3 1 1 -2.11 0.00 0.00 0.00 0.00 0.00 4 2.11 0.00 0.00 0.00 0.00 0.00

4 1 3 -2.19 0.00 0.00 0.00 0.00 0.00 4 2.19 0.00 0.00 0.00 0.00 0.00

5 1 3 6.69 0.00 0.00 0.00 0.00 0.00 1 -6.69 0.00 0.00 0.00 0.00 0.00

6 1 3 2.56 0.00 0.00 0.00 0.00 0.00 2 -2.56 0.00 0.00 0.00 0.00 0.00

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

24. FINISH

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

Page 21: Project File- Finite Element

EXPERIMENT-5

OBJECTIVE: ANALYSE THE TRUSS BY FEM (1 internal node)

Fig. 12

The truss is subjected to vertical downward load of 8 kN at node 3 and horizontal force of 4 kN at node 4.In the present practical , the members have 1 internal node at the midpoint of each member.

Total number of nodes = 9Total number of Elements = 12

Page 22: Project File- Finite Element

Fig .13 Joint Displacement

Page 23: Project File- Finite Element

Output :

**************************************************** * * * STAAD.Pro V8i SELECTseries5 * * Version 20.07.10.65 * * Proprietary Program of * * Bentley Systems, Inc. * * Date= APR 30, 2015 * * Time= 4:16:19 * * * * USER ID: * ****************************************************

1. STAAD TRUSSINPUT FILE: Q-5.STD 2. START JOB INFORMATION 3. ENGINEER DATE 27-APR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 2 5 0 0; 3 0 3 0; 4 5 3 0; 5 2.5 0 0; 6 5 1.5 0; 7 2.5 1.5 0 9. 8 2.5 3 0; 9 0 1.5 0 10. MEMBER INCIDENCES 11. 1 1 5; 2 2 6; 3 1 7; 4 3 8; 5 3 9; 6 3 7; 7 5 2; 8 6 4; 9 7 4; 10 8 4; 11 9 1 12. 12 7 2 13. DEFINE MATERIAL START 14. ISOTROPIC MATERIAL1 15. E 100 16. POISSON 0.45 17. END DEFINE MATERIAL 18. CONSTANTS 19. MATERIAL MATERIAL1 ALL 20. MEMBER PROPERTY AMERICAN 21. 1 TO 12 PRIS AX 1 AY 1 AZ 1 22. SUPPORTS 23. 1 2 PINNED 24. LOAD 1 25. JOINT LOAD 26. 3 FY -8 27. 4 FX 4 28. LOAD LIST 1 29. PERFORM ANALYSIS

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

NUMBER OF JOINTS 9 NUMBER OF MEMBERS 12 NUMBER OF PLATES 0 NUMBER OF SOLIDS 0 NUMBER OF SURFACES 0 NUMBER OF SUPPORTS 2

SOLVER USED IS THE IN-CORE ADVANCED SOLVER TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 14 TOTAL LOAD COMBINATION CASES = 0 SO FAR.

30. PRINT ANALYSIS RESULTS

Page 24: Project File- Finite Element

ANALYSIS RESULTS

JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = TRUSS ------------------

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 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 3 1 5.3423 -20.0560 0.0000 0.0000 0.0000 0.0000 4 1 16.2980 -3.2560 0.0000 0.0000 0.0000 0.0000 5 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 6 1 0.0000 -1.6280 0.0000 0.0000 0.0000 0.0000 7 1 7.9301 -1.2631 0.0000 0.0000 0.0000 0.0000 8 1 10.8202 0.0000 0.0000 0.0000 0.0000 0.0000 9 1 0.0000 -10.0280 0.0000 0.0000 0.0000 0.0000

SUPPORT REACTIONS -UNIT KN METE STRUCTURE TYPE = TRUSS -----------------

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

1 1 -1.81 5.60 0.00 0.00 0.00 0.00 2 1 -2.19 2.40 0.00 0.00 0.00 0.00

MEMBER END FORCES STRUCTURE TYPE = TRUSS ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

1 1 1 0.00 0.00 0.00 0.00 0.00 0.00 5 0.00 0.00 0.00 0.00 0.00 0.00

2 1 2 1.09 0.00 0.00 0.00 0.00 0.00 6 -1.09 0.00 0.00 0.00 0.00 0.00

3 1 1 -2.11 0.00 0.00 0.00 0.00 0.00 7 2.11 0.00 0.00 0.00 0.00 0.00

4 1 3 -2.19 0.00 0.00 0.00 0.00 0.00 8 2.19 0.00 0.00 0.00 0.00 0.00

5 1 3 6.69 0.00 0.00 0.00 0.00 0.00 9 -6.69 0.00 0.00 0.00 0.00 0.00

6 1 3 2.56 0.00 0.00 0.00 0.00 0.00 7 -2.56 0.00 0.00 0.00 0.00 0.00

7 1 5 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

Page 25: Project File- Finite Element

8 1 6 1.09 0.00 0.00 0.00 0.00 0.00 4 -1.09 0.00 0.00 0.00 0.00 0.00

9 1 7 -2.11 0.00 0.00 0.00 0.00 0.00 4 2.11 0.00 0.00 0.00 0.00 0.00

10 1 8 -2.19 0.00 0.00 0.00 0.00 0.00 4 2.19 0.00 0.00 0.00 0.00 0.00

11 1 9 6.69 0.00 0.00 0.00 0.00 0.00 1 -6.69 0.00 0.00 0.00 0.00 0.00

12 1 7 2.56 0.00 0.00 0.00 0.00 0.00 2 -2.56 0.00 0.00 0.00 0.00 0.00

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

Page 26: Project File- Finite Element

EXPERIMENT-6

OBJECTIVE: ANALYSE THE TRUSS BY FEM (2 internal node)

Fig. 14

The truss is subjected to vertical downward load of 8 kN at node 3 and horizontal force of 4 kN at node 4.In the present practical , the members have 2 internal node at the equal interval of each member.

Total number of nodes = 16Total number of Elements = 18

Page 27: Project File- Finite Element

Fig. 15

Page 28: Project File- Finite Element

Output:

**************************************************** * * * STAAD.Pro V8i SELECTseries5 * * Version 20.07.10.65 * * Proprietary Program of * * Bentley Systems, Inc. * * Date= APR 30, 2015 * * Time= 4:18: 5 * * * * USER ID: * ****************************************************

1. STAAD TRUSSINPUT FILE: Q-6.STD 2. START JOB INFORMATION 3. ENGINEER DATE 27-APR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 2 5 0 0; 3 0 3 0; 4 5 3 0; 5 1.66667 0 0; 6 3.33333 0 0; 7 5 1 0 9. 8 5 2 0; 9 1.66667 1 0; 10 3.33333 2 0; 11 1.66667 3 0; 12 3.33333 3 0 10. 13 0 2 0; 14 0 1 0; 15 1.66667 2 0; 16 3.33333 1 0 11. MEMBER INCIDENCES 12. 1 1 5; 2 2 7; 3 1 9; 4 3 11; 5 3 13; 6 3 15; 7 5 6; 8 6 2; 9 7 8; 10 8 4 13. 11 9 10; 12 10 4; 13 11 12; 14 12 4; 15 13 14; 16 14 1; 17 15 16; 18 16 2 14. DEFINE MATERIAL START 15. ISOTROPIC MATERIAL1 16. E 100 17. POISSON 0.45 18. END DEFINE MATERIAL 19. CONSTANTS 20. MATERIAL MATERIAL1 ALL 21. MEMBER PROPERTY AMERICAN 22. 1 TO 18 PRIS AX 1 AY 1 AZ 1 23. SUPPORTS 24. 1 2 PINNED 25. LOAD 1 26. JOINT LOAD 27. 3 FY -8 28. 4 FX 4 29. LOAD LIST 1 30. PERFORM ANALYSIS

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

NUMBER OF JOINTS 16 NUMBER OF MEMBERS 18 NUMBER OF PLATES 0 NUMBER OF SOLIDS 0 NUMBER OF SURFACES 0 NUMBER OF SUPPORTS 2

SOLVER USED IS THE IN-CORE ADVANCED SOLVER TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 28 TOTAL LOAD COMBINATION CASES = 0 SO FAR.

31. PRINT ANALYSIS RESULTS

Page 29: Project File- Finite Element

ANALYSIS RESULTS

JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = TRUSS ------------------

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 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 3 1 5.3443 -20.0560 0.0000 0.0000 0.0000 0.0000 4 1 16.2999 -3.2560 0.0000 0.0000 0.0000 0.0000 5 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 6 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 7 1 0.0000 -1.0853 0.0000 0.0000 0.0000 0.0000 8 1 0.0000 -2.1707 0.0000 0.0000 0.0000 0.0000 9 1 -139.7666 240.9140 0.0000 0.0000 0.0000 0.0000 10 1 150.1086 -234.2402 0.0000 0.0000 0.0000 0.0000 11 1 8.9962 0.0000 0.0000 0.0000 0.0000 0.0000 12 1 12.6480 0.0000 0.0000 0.0000 0.0000 0.0000 13 1 0.0000 -13.3707 0.0000 0.0000 0.0000 0.0000 14 1 0.0000 -6.6853 0.0000 0.0000 0.0000 0.0000 15 1 175.0935 272.5131 0.0000 0.0000 0.0000 0.0000 16 1 -181.8279 -312.7003 0.0000 0.0000 0.0000 0.0000

SUPPORT REACTIONS -UNIT KN METE STRUCTURE TYPE = TRUSS -----------------

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

1 1 -1.81 5.60 0.00 0.00 0.00 0.00 2 1 -2.19 2.40 0.00 0.00 0.00 0.00

MEMBER END FORCES STRUCTURE TYPE = TRUSS ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

1 1 1 0.00 0.00 0.00 0.00 0.00 0.00 5 0.00 0.00 0.00 0.00 0.00 0.00

2 1 2 1.09 0.00 0.00 0.00 0.00 0.00 7 -1.09 0.00 0.00 0.00 0.00 0.00

3 1 1 -2.11 0.00 0.00 0.00 0.00 0.00 9 2.11 0.00 0.00 0.00 0.00 0.00

4 1 3 -2.19 0.00 0.00 0.00 0.00 0.00 11 2.19 0.00 0.00 0.00 0.00 0.00

5 1 3 6.69 0.00 0.00 0.00 0.00 0.00 13 -6.69 0.00 0.00 0.00 0.00 0.00

Page 30: Project File- Finite Element

6 1 3 2.56 0.00 0.00 0.00 0.00 0.00 15 -2.56 0.00 0.00 0.00 0.00 0.00

7 1 5 0.00 0.00 0.00 0.00 0.00 0.00 6 0.00 0.00 0.00 0.00 0.00 0.00

8 1 6 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

9 1 7 1.09 0.00 0.00 0.00 0.00 0.00 8 -1.09 0.00 0.00 0.00 0.00 0.00

10 1 8 1.09 0.00 0.00 0.00 0.00 0.00 4 -1.09 0.00 0.00 0.00 0.00 0.00

11 1 9 -2.11 0.00 0.00 0.00 0.00 0.00 10 2.11 0.00 0.00 0.00 0.00 0.00

12 1 10 -2.11 0.00 0.00 0.00 0.00 0.00 4 2.11 0.00 0.00 0.00 0.00 0.00

13 1 11 -2.19 0.00 0.00 0.00 0.00 0.00 12 2.19 0.00 0.00 0.00 0.00 0.00

14 1 12 -2.19 0.00 0.00 0.00 0.00 0.00 4 2.19 0.00 0.00 0.00 0.00 0.00

15 1 13 6.69 0.00 0.00 0.00 0.00 0.00 14 -6.69 0.00 0.00 0.00 0.00 0.00

MEMBER END FORCES STRUCTURE TYPE = TRUSS ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

16 1 14 6.69 0.00 0.00 0.00 0.00 0.00 1 -6.69 0.00 0.00 0.00 0.00 0.00

17 1 15 2.56 0.00 0.00 0.00 0.00 0.00 16 -2.56 0.00 0.00 0.00 0.00 0.00

18 1 16 2.56 0.00 0.00 0.00 0.00 0.00 2 -2.56 0.00 0.00 0.00 0.00 0.00

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

32. FINISH

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

Page 31: Project File- Finite Element

EXPERIMENT-7

OBJECTIVE: ANALYSE THE TRUSS BY PLANE FRAME

Fig . 16

The plane frame(x-y plane) is subjected to uniformly distributed load of 10 kN/m on the beam of span 8 m and an axial load at node 3 of 2.0 kN.

Total number of nodes = 4Total number of elements = 3

Column dimensions = 250x450 mmBeam dimensions = 250x600 mm

Page 32: Project File- Finite Element

Fig 17 Bending Moment Diagram

Fig 18 Bending Moment Diagram

Page 33: Project File- Finite Element

Output:

**************************************************** * * * STAAD.Pro V8i SELECTseries5 * * Version 20.07.10.65 * * Proprietary Program of * * Bentley Systems, Inc. * * Date= APR 30, 2015 * * Time= 4:28:15 * * * * USER ID: * ****************************************************

1. STAAD PLANEINPUT FILE: Q-7.STD 2. START JOB INFORMATION 3. ENGINEER DATE 27-APR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 2 8 0 0; 3 0 4 0; 4 8 4 0 9. MEMBER INCIDENCES 10. 3 3 4; 5 1 3; 7 2 4 11. DEFINE MATERIAL START 12. ISOTROPIC MATERIAL1 13. E 100 14. POISSON 0.45 15. END DEFINE MATERIAL 16. CONSTANTS 17. MATERIAL MATERIAL1 ALL 18. MEMBER PROPERTY AMERICAN 19. 3 PRIS YD 0.6 ZD 0.25 20. 5 7 PRIS YD 0.45 ZD 0.25 21. SUPPORTS 22. 1 2 FIXED 23. LOAD 1 24. MEMBER LOAD 25. 3 UNI GY -10 26. JOINT LOAD 27. 3 FX 2 28. PERFORM ANALYSIS

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

NUMBER OF JOINTS 4 NUMBER OF MEMBERS 3 NUMBER OF PLATES 0 NUMBER OF SOLIDS 0 NUMBER OF SURFACES 0 NUMBER OF SUPPORTS 2

SOLVER USED IS THE IN-CORE ADVANCED SOLVER TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 6 TOTAL LOAD COMBINATION CASES = 0 SO FAR.

Page 34: Project File- Finite Element

29. PRINT ANALYSIS RESULTS ANALYSIS RESULTS

JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = PLANE ------------------

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 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 3 1 4.346E+03-1.407E+03 0.000E+00 0.000E+00 0.000E+00-1.860E+02 4 1 3.642E+03-1.438E+03 0.000E+00 0.000E+00 0.000E+00 1.754E+02

SUPPORT REACTIONS -UNIT KN METE STRUCTURE TYPE = PLANE -----------------

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

1 1 11.21 39.56 0.00 0.00 0.00 -13.60 2 1 -13.21 40.44 0.00 0.00 0.00 18.10

MEMBER END FORCES STRUCTURE TYPE = PLANE ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

3 1 3 13.21 39.56 0.00 0.00 0.00 31.25 4 -13.21 40.44 0.00 0.00 0.00 -34.75

5 1 1 39.56 -11.21 0.00 0.00 0.00 -13.60 3 -39.56 11.21 0.00 0.00 0.00 -31.25

7 1 2 40.44 13.21 0.00 0.00 0.00 18.10 4 -40.44 -13.21 0.00 0.00 0.00 34.75

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

30. FINISH

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

Page 35: Project File- Finite Element

EXPERIMENT-8

OBJECTIVE: ANALYSE THE TRUSS BY PLANE FRAME (1 INTERNAL NODE)

Fig . 19

The plane frame(x-y plane) is subjected to uniformly distributed load of 10 kN/m on the beam of span 8 m and an axial load at node 3 of 2.0 kN.The members

Total number of nodes = 7Total number of elements = 6

Column dimensions = 250x450 mmBeam dimensions = 250x600 mm

Page 36: Project File- Finite Element

Fig 20 Bending Moment Diagram

Fig 21 Shear Force Diagram

Page 37: Project File- Finite Element

Output:

**************************************************** * * * STAAD.Pro V8i SELECTseries5 * * Version 20.07.10.65 * * Proprietary Program of * * Bentley Systems, Inc. * * Date= APR 30, 2015 * * Time= 4:35: 3 * * * * USER ID: * ****************************************************

1. STAAD PLANEINPUT FILE: Q-8.STD 2. START JOB INFORMATION 3. ENGINEER DATE 27-APR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 2 8 0 0; 3 0 4 0; 4 8 4 0; 5 0 2 0; 6 8 2 0; 7 4 4 0 9. MEMBER INCIDENCES 10. 1 1 5; 2 2 6; 3 3 7; 4 5 3; 5 6 4; 6 7 4 11. DEFINE MATERIAL START 12. ISOTROPIC MATERIAL1 13. E 100 14. POISSON 0.45 15. END DEFINE MATERIAL 16. CONSTANTS 17. MATERIAL MATERIAL1 ALL 18. MEMBER PROPERTY AMERICAN 19. 3 6 PRIS YD 0.6 ZD 0.25 20. 1 2 4 5 PRIS YD 0.45 ZD 0.25 21. SUPPORTS 22. 1 2 FIXED 23. LOAD 1 LOADTYPE NONE TITLE LOAD CASE 1 24. MEMBER LOAD 25. 3 6 UNI GY -10 26. JOINT LOAD 27. 3 FX 2 28. PERFORM ANALYSIS

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

NUMBER OF JOINTS 7 NUMBER OF MEMBERS 6 NUMBER OF PLATES 0 NUMBER OF SOLIDS 0 NUMBER OF SURFACES 0 NUMBER OF SUPPORTS 2

SOLVER USED IS THE IN-CORE ADVANCED SOLVER TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 15 TOTAL LOAD COMBINATION CASES = 0 SO FAR.

Page 38: Project File- Finite Element

29. PRINT ANALYSIS RESULTS ANALYSIS RESULTS

JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = PLANE ------------------

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 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 3 1 4.346E+03-1.407E+03 0.000E+00 0.000E+00 0.000E+00-1.860E+02 4 1 3.642E+03-1.438E+03 0.000E+00 0.000E+00 0.000E+00 1.754E+02 5 1 -7.129E+03-7.033E+02 0.000E+00 0.000E+00 0.000E+00 2.511E+01 6 1 1.059E+04-7.189E+02 0.000E+00 0.000E+00 0.000E+00-5.150E+01 7 1 3.994E+03-6.309E+04 0.000E+00 0.000E+00 0.000E+00 2.451E+00

SUPPORT REACTIONS -UNIT KN METE STRUCTURE TYPE = PLANE -----------------

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

1 1 11.21 39.56 0.00 0.00 0.00 -13.60 2 1 -13.21 40.44 0.00 0.00 0.00 18.10

MEMBER END FORCES STRUCTURE TYPE = PLANE ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

1 1 1 39.56 -11.21 0.00 0.00 0.00 -13.60 5 -39.56 11.21 0.00 0.00 0.00 -8.83

2 1 2 40.44 13.21 0.00 0.00 0.00 18.10 6 -40.44 -13.21 0.00 0.00 0.00 8.32

3 1 3 13.21 39.56 0.00 0.00 0.00 31.25 7 -13.21 0.44 0.00 0.00 0.00 47.00

4 1 5 39.56 -11.21 0.00 0.00 0.00 8.83 3 -39.56 11.21 0.00 0.00 0.00 -31.25

5 1 6 40.44 13.21 0.00 0.00 0.00 -8.32 4 -40.44 -13.21 0.00 0.00 0.00 34.75

6 1 7 13.21 -0.44 0.00 0.00 0.00 -47.00 4 -13.21 40.44 0.00 0.00 0.00 -34.75

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

30. FINISH

Page 39: Project File- Finite Element

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

EXPERIMENT-9

OBJECTIVE: ANALYSE THE TRUSS BY PLANE FRAME (2 INTERNAL NODE)

Fig . 22

The plane frame(x-y plane) is subjected to uniformly distributed load of 10 kN/m on the beam of span 8 m and an axial load at node 3 of 2.0 kN.The members

Total number of nodes = 10Total number of elements = 9

Column dimensions = 250x450 mmBeam dimensions = 250x600 mm

Page 40: Project File- Finite Element

Fig 23 Bending Moment Diagram

Fig 24 Shear Force Diagram

Page 41: Project File- Finite Element

Output:

**************************************************** * * * STAAD.Pro V8i SELECTseries5 * * Version 20.07.10.65 * * Proprietary Program of * * Bentley Systems, Inc. * * Date= APR 30, 2015 * * Time= 4:38:42 * * * * USER ID: * ****************************************************

1. STAAD PLANEINPUT FILE: Q-9.STD 2. START JOB INFORMATION 3. ENGINEER DATE 27-APR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 2 8 0 0; 3 0 4 0; 4 8 4 0; 5 0 1.33333 0; 6 0 2.66667 0 9. 7 8 1.33333 0; 8 8 2.66667 0; 9 2.66667 4 0; 10 5.33333 4 0 10. MEMBER INCIDENCES 11. 1 1 5; 2 2 7; 3 3 9; 4 5 6; 5 6 3; 6 7 8; 7 8 4; 8 9 10; 9 10 4 12. DEFINE MATERIAL START 13. ISOTROPIC MATERIAL1 14. E 100 15. POISSON 0.45 16. END DEFINE MATERIAL 17. CONSTANTS 18. MATERIAL MATERIAL1 ALL 19. MEMBER PROPERTY AMERICAN 20. 3 8 9 PRIS YD 0.6 ZD 0.25 21. 1 2 4 TO 7 PRIS YD 0.45 ZD 0.25 22. SUPPORTS 23. 1 2 FIXED 24. LOAD 1 LOADTYPE NONE TITLE LOAD CASE 1 25. MEMBER LOAD 26. 3 8 9 UNI GY -10 27. JOINT LOAD 28. 3 FX 2 29. PERFORM ANALYSIS

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

NUMBER OF JOINTS 10 NUMBER OF MEMBERS 9 NUMBER OF PLATES 0 NUMBER OF SOLIDS 0 NUMBER OF SURFACES 0 NUMBER OF SUPPORTS 2

SOLVER USED IS THE IN-CORE ADVANCED SOLVER TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 24 TOTAL LOAD COMBINATION CASES = 0 SO FAR.

Page 42: Project File- Finite Element

30. PRINT ANALYSIS RESULTS ANALYSIS RESULTS JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = PLANE ------------------

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 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 3 1 4.346E+03-1.407E+03 0.000E+00 0.000E+00 0.000E+00-1.860E+02 4 1 3.642E+03-1.438E+03 0.000E+00 0.000E+00 0.000E+00 1.754E+02 5 1 -4.486E+03-4.689E+02 0.000E+00 0.000E+00 0.000E+00 4.299E+01 6 1 -7.704E+03-9.378E+02 0.000E+00 0.000E+00 0.000E+00-1.902E+01 7 1 6.260E+03-4.793E+02 0.000E+00 0.000E+00 0.000E+00-6.526E+01 8 1 1.297E+04-9.585E+02 0.000E+00 0.000E+00 0.000E+00-6.796E+00 9 1 4.111E+03-5.420E+04 0.000E+00 0.000E+00 0.000E+00-1.289E+02 10 1 3.876E+03-5.359E+04 0.000E+00 0.000E+00 0.000E+00 1.321E+02

SUPPORT REACTIONS -UNIT KN METE STRUCTURE TYPE = PLANE -----------------

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

1 1 11.21 39.56 0.00 0.00 0.00 -13.60 2 1 -13.21 40.44 0.00 0.00 0.00 18.10

MEMBER END FORCES STRUCTURE TYPE = PLANE ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

1 1 1 39.56 -11.21 0.00 0.00 0.00 -13.60 5 -39.56 11.21 0.00 0.00 0.00 -1.35

2 1 2 40.44 13.21 0.00 0.00 0.00 18.10 7 -40.44 -13.21 0.00 0.00 0.00 -0.48

3 1 3 13.21 39.56 0.00 0.00 0.00 31.25 9 -13.21 -12.90 0.00 0.00 0.00 38.69

4 1 5 39.56 -11.21 0.00 0.00 0.00 1.35 6 -39.56 11.21 0.00 0.00 0.00 -16.30

5 1 6 39.56 -11.21 0.00 0.00 0.00 16.30 3 -39.56 11.21 0.00 0.00 0.00 -31.25

6 1 7 40.44 13.21 0.00 0.00 0.00 0.48 8 -40.44 -13.21 0.00 0.00 0.00 17.13

7 1 8 40.44 13.21 0.00 0.00 0.00 -17.13 4 -40.44 -13.21 0.00 0.00 0.00 34.75

Page 43: Project File- Finite Element

8 1 9 13.21 12.90 0.00 0.00 0.00 -38.69 10 -13.21 13.77 0.00 0.00 0.00 37.53

9 1 10 13.21 -13.77 0.00 0.00 0.00 -37.53 4 -13.21 40.44 0.00 0.00 0.00 -34.75

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

31. FINISH

Page 44: Project File- Finite Element

EXPERIMENT-10

OBJECTIVE: ANALYSE THE SPACE TRUSS

Fig . 25

The Space truss is subjected to concentrated load at joint 5 of 5 kN (downward). Each member is of length 8 m .

Total number of nodes = 10Total number of elements = 9

Page 45: Project File- Finite Element

Fig 26 Joint Displacement of Space Truss

Page 46: Project File- Finite Element

Output:

**************************************************** * * * STAAD.Pro V8i SELECTseries5 * * Version 20.07.10.65 * * Proprietary Program of * * Bentley Systems, Inc. * * Date= APR 30, 2015 * * Time= 4:42:12 * * * * USER ID: * ****************************************************

1. STAAD TRUSSINPUT FILE: Q-10.STD 2. START JOB INFORMATION 3. ENGINEER DATE 27-APR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 2 10 0 0; 3 10 0 10; 4 0 0 10; 5 5 3.74165 5 9. MEMBER INCIDENCES 10. 1 1 5; 2 5 2; 3 5 4; 4 5 3 11. DEFINE MATERIAL START 12. ISOTROPIC MATERIAL1 13. E 100 14. POISSON 0.45 15. END DEFINE MATERIAL 16. MEMBER PROPERTY 17. 1 TO 4 PRIS AX 1 AY 1 AZ 1 18. CONSTANTS 19. MATERIAL MATERIAL1 ALL 20. SUPPORTS 21. 1 TO 4 PINNED 22. LOAD 1 23. JOINT LOAD 24. 5 FY -5 25. PERFORM ANALYSIS

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

NUMBER OF JOINTS 5 NUMBER OF MEMBERS 4 NUMBER OF PLATES 0 NUMBER OF SOLIDS 0 NUMBER OF SURFACES 0 NUMBER OF SUPPORTS 4

SOLVER USED IS THE IN-CORE ADVANCED SOLVER TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 3 TOTAL LOAD COMBINATION CASES = 0 SO FAR.

26. LOAD LIST 1

Page 47: Project File- Finite Element

27. PRINT ANALYSIS RESULTS ANALYSIS RESULTS

JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = TRUSS ------------------

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 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 3 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 4 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 5 1 0.0000 -45.7144 0.0000 0.0000 0.0000 0.0000

SUPPORT REACTIONS -UNIT KN METE STRUCTURE TYPE = TRUSS -----------------

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

1 1 1.67 1.25 1.67 0.00 0.00 0.00 2 1 -1.67 1.25 1.67 0.00 0.00 0.00 3 1 -1.67 1.25 -1.67 0.00 0.00 0.00 4 1 1.67 1.25 -1.67 0.00 0.00 0.00

MEMBER END FORCES STRUCTURE TYPE = TRUSS ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

1 1 1 2.67 0.00 0.00 0.00 0.00 0.00 5 -2.67 0.00 0.00 0.00 0.00 0.00

2 1 5 2.67 0.00 0.00 0.00 0.00 0.00 2 -2.67 0.00 0.00 0.00 0.00 0.00

3 1 5 2.67 0.00 0.00 0.00 0.00 0.00 4 -2.67 0.00 0.00 0.00 0.00 0.00

4 1 5 2.67 0.00 0.00 0.00 0.00 0.00 3 -2.67 0.00 0.00 0.00 0.00 0.00

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

28. FINISH

Page 48: Project File- Finite Element

EXPERIMENT-11

OBJECTIVE: ANALYSE THE GRID

Fig 27

The grid has 4 beams each of length of dimension 4 m placed at right angles to each other in the x-z plane.

Total number of Nodes = 5Total number of elements = 4

Page 49: Project File- Finite Element

Fig 28 Bending Moment Diagram

Fig 29 Shear Force Diagram

Page 50: Project File- Finite Element

Output:

**************************************************** * * * STAAD.Pro V8i SELECTseries5 * * Version 20.07.10.65 * * Proprietary Program of * * Bentley Systems, Inc. * * Date= APR 30, 2015 * * Time= 4:45: 1 * * * * USER ID: * ****************************************************

1. STAAD SPACEINPUT FILE: Q-11.STD 2. START JOB INFORMATION 3. ENGINEER DATE 27-APR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 2 4 0 0; 3 0 0 4; 4 -4 0 0; 5 0 0 -4 9. MEMBER INCIDENCES 10. 1 1 2; 2 1 4; 3 1 5; 4 1 3 11. CONSTANTS 12. E 200000000 ALL 13. POISSON 0.25 ALL 14. G 80000000 ALL 15. MEMBER PROPERTY 16. 1 TO 4 PRIS YD 0.45 ZD 0.25 17. SUPPORTS 18. 2 TO 5 FIXED 19. LOAD 1 20. JOINT LOAD 21. 1 FY -10 22. PERFORM ANALYSIS

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

NUMBER OF JOINTS 5 NUMBER OF MEMBERS 4 NUMBER OF PLATES 0 NUMBER OF SOLIDS 0 NUMBER OF SURFACES 0 NUMBER OF SUPPORTS 4

SOLVER USED IS THE IN-CORE ADVANCED SOLVER TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 6 TOTAL LOAD COMBINATION CASES = 0 SO FAR.

23. LOAD LIST 1 24. PRINT ANALYSIS RESULTS ANALYSIS RESULTS

JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = SPACE ------------------

Page 51: Project File- Finite Element

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

1 1 0.0000 -0.0036 0.0000 0.0000 0.0000 0.0000 2 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 3 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 4 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 5 1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000

SUPPORT REACTIONS -UNIT KN METE STRUCTURE TYPE = SPACE -----------------

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

2 1 0.00 2.50 0.00 0.00 0.00 -5.00 3 1 0.00 2.50 0.00 5.00 0.00 0.00 4 1 0.00 2.50 0.00 0.00 0.00 5.00 5 1 0.00 2.50 0.00 -5.00 0.00 0.00

MEMBER END FORCES STRUCTURE TYPE = SPACE ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

1 1 1 0.00 -2.50 0.00 0.00 0.00 -5.00 2 0.00 2.50 0.00 0.00 0.00 -5.00

2 1 1 0.00 -2.50 0.00 0.00 0.00 -5.00 4 0.00 2.50 0.00 0.00 0.00 -5.00

3 1 1 0.00 -2.50 0.00 0.00 0.00 -5.00 5 0.00 2.50 0.00 0.00 0.00 -5.00

4 1 1 0.00 -2.50 0.00 0.00 0.00 -5.00 3 0.00 2.50 0.00 0.00 0.00 -5.00

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

25. FINISH

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

Page 52: Project File- Finite Element

EXPERIMENT-12

OBJECTIVE: ANALYSE THE COMMERCIAL BUILDING (G+12) SUBJECTED TO EARTHQUAKE

LOAD DATA BASIS:

1. M-25 GRADE OF CONCRETE2. FE-500 GRADE OF STEEL3. ZONE-IV COMMERCIAL BUILDING

DEAD LOAD CALCULATION:

1. Wall Load :230 mm thick brick Wall

Wall on grid 1 = 0.23*20*(3.2-0.45) =12.65 kN/m = 12.7 kN/m (say)Wall on Grid A =0.23*20*(3.2-0.6) =11.96 kN/m = 12.0 kN/m (say)

2. Slab:Lx (shorter side) =3 mLy (longer side) =6mLy/Lx =2.0

Hence, One Way Slab.

ii) One way slab(continuous)

Slab thickness assumed, D = 110 MM.

Clear cover = 25 MMEffective Slab thickness d = 80 MMSpan, Lx = 3000 MM

Grade of concrete, fck = 25 N/MM2

Grade of steel , fy = 500 N/MM2

Dead load DL = 3.60 KN

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Live load LL = 3.00 KNTotal load w = 6.60 KNMax +ve BM=wl2/12 = 4.95 KN-M

Max -ve BM=wl2/10 = 5.94 KN-M

Check for effective depth

Mud= K b fck = 51 MM OK

Calculation for area of steel

Ast (at midspan) = 266.83

Required Spacing 8 dia bars @188.28 C/C

Provide 8 bars @ 150 C/C

Ast (at Support) = 320.203125

Required Spacing 8 dia bars @ 156.90 C/CProvide 8 bars @ 150 C/C

Earthquake force is to be taken as 1.0 DEAD LOAD +0.5 LL

Effective length of Columns in each direction 0.65 Lo

Column Dimensions = 300x900 mm & 300x750 mm

Beam dimensions =230x600 mm & 230x450 mm

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PLAN

Fig 30

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Elevation

Front view

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Side View

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Output

**************************************************** * * * STAAD.Pro V8i SELECTseries5 * * Version 20.07.10.65 * * Proprietary Program of * * Bentley Systems, Inc. * * Date= APR 30, 2015 * * Time= 6:45:56 * * * * USER ID: * ****************************************************

1. STAAD SPACEINPUT FILE: Q-13.STD 2. START JOB INFORMATION 3. ENGINEER DATE 27-APR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 7 6 0 0; 28 12 0 0; 29 18 0 0; 30 24 0 0; 31 30 0 0; 32 36 0 0 9. 33 42 0 0; 34 0 0 3; 35 6 0 3; 36 12 0 3; 37 18 0 3; 38 24 0 3; 39 30 0 3 10. 40 36 0 3; 41 42 0 3; 42 0 0 6; 43 6 0 6; 44 12 0 6; 45 18 0 6; 46 24 0 6 11. 47 30 0 6; 48 36 0 6; 49 42 0 6; 50 0 0 9; 51 6 0 9; 52 12 0 9; 53 18 0 9 12. 54 24 0 9; 55 30 0 9; 56 36 0 9; 57 42 0 9; 58 0 0 12; 59 6 0 12; 60 12 0 12 13. 61 18 0 12; 62 24 0 12; 63 30 0 12; 64 36 0 12; 65 42 0 12; 66 0 1.5 0 14. 67 6 1.5 0; 68 12 1.5 0; 69 18 1.5 0; 70 24 1.5 0; 71 30 1.5 0; 72 36 1.5 0 15. 73 42 1.5 0; 74 0 1.5 3; 75 6 1.5 3; 76 12 1.5 3; 77 18 1.5 3; 78 24 1.5 3 16. 79 30 1.5 3; 80 36 1.5 3; 81 42 1.5 3; 82 0 1.5 6; 83 6 1.5 6; 84 12 1.5 6 17. 85 18 1.5 6; 86 24 1.5 6; 87 30 1.5 6; 88 36 1.5 6; 89 42 1.5 6; 90 0 1.5 9 18. 91 6 1.5 9; 92 12 1.5 9; 93 18 1.5 9; 94 24 1.5 9; 95 30 1.5 9; 96 36 1.5 9 19. 97 42 1.5 9; 98 0 1.5 12; 99 6 1.5 12; 100 12 1.5 12; 101 18 1.5 12 20. 102 24 1.5 12; 103 30 1.5 12; 104 36 1.5 12; 105 42 1.5 12; 106 0 4.3 0 21. 107 6 4.3 0; 108 12 4.3 0; 109 18 4.3 0; 110 24 4.3 0; 111 30 4.3 0 22. 112 36 4.3 0; 113 42 4.3 0; 114 0 4.3 3; 115 6 4.3 3; 116 12 4.3 3 23. 117 18 4.3 3; 118 24 4.3 3; 119 30 4.3 3; 120 36 4.3 3; 121 42 4.3 3 24. 122 0 4.3 6; 123 6 4.3 6; 124 12 4.3 6; 125 18 4.3 6; 126 24 4.3 6 25. 127 30 4.3 6; 128 36 4.3 6; 129 42 4.3 6; 130 0 4.3 9; 131 6 4.3 9 26. 132 12 4.3 9; 133 18 4.3 9; 134 24 4.3 9; 135 30 4.3 9; 136 36 4.3 9 27. 137 42 4.3 9; 138 0 4.3 12; 139 6 4.3 12; 140 12 4.3 12; 141 18 4.3 12 28. 142 24 4.3 12; 143 30 4.3 12; 144 36 4.3 12; 145 42 4.3 12; 146 0 7.5 0 29. 147 6 7.5 0; 148 12 7.5 0; 149 18 7.5 0; 150 24 7.5 0; 151 30 7.5 0 30. 152 36 7.5 0; 153 42 7.5 0; 154 0 7.5 3; 155 6 7.5 3; 156 12 7.5 3 31. 157 18 7.5 3; 158 24 7.5 3; 159 30 7.5 3; 160 36 7.5 3; 161 42 7.5 3 32. 162 0 7.5 6; 163 6 7.5 6; 164 12 7.5 6; 165 18 7.5 6; 166 24 7.5 6 33. 167 30 7.5 6; 168 36 7.5 6; 169 42 7.5 6; 170 0 7.5 9; 171 6 7.5 9 34. 172 12 7.5 9; 173 18 7.5 9; 174 24 7.5 9; 175 30 7.5 9; 176 36 7.5 9 35. 177 42 7.5 9; 178 0 7.5 12; 179 6 7.5 12; 180 12 7.5 12; 181 18 7.5 12 36. 182 24 7.5 12; 183 30 7.5 12; 184 36 7.5 12; 185 42 7.5 12; 186 0 10.7 0 37. 187 6 10.7 0; 188 12 10.7 0; 189 18 10.7 0; 190 24 10.7 0; 191 30 10.7 0 38. 192 36 10.7 0; 193 42 10.7 0; 194 0 10.7 3; 195 6 10.7 3; 196 12 10.7 3 39. 197 18 10.7 3; 198 24 10.7 3; 199 30 10.7 3; 200 36 10.7 3; 201 42 10.7 3 40. 202 0 10.7 6; 203 6 10.7 6; 204 12 10.7 6; 205 18 10.7 6; 206 24 10.7 6 41. 207 30 10.7 6; 208 36 10.7 6; 209 42 10.7 6; 210 0 10.7 9; 211 6 10.7 9 42. 212 12 10.7 9; 213 18 10.7 9; 214 24 10.7 9; 215 30 10.7 9; 216 36 10.7 9 43. 217 42 10.7 9; 218 0 10.7 12; 219 6 10.7 12; 220 12 10.7 12; 221 18 10.7 12 44. 222 24 10.7 12; 223 30 10.7 12; 224 36 10.7 12; 225 42 10.7 12; 226 0 13.9 0

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45. 227 6 13.9 0; 228 12 13.9 0; 229 18 13.9 0; 230 24 13.9 0; 231 30 13.9 0 46. 232 36 13.9 0; 233 42 13.9 0; 234 0 13.9 3; 235 6 13.9 3; 236 12 13.9 3 47. 237 18 13.9 3; 238 24 13.9 3; 239 30 13.9 3; 240 36 13.9 3; 241 42 13.9 3 48. 242 0 13.9 6; 243 6 13.9 6; 244 12 13.9 6; 245 18 13.9 6; 246 24 13.9 6 49. 247 30 13.9 6; 248 36 13.9 6; 249 42 13.9 6; 250 0 13.9 9; 251 6 13.9 9 50. 252 12 13.9 9; 253 18 13.9 9; 254 24 13.9 9; 255 30 13.9 9; 256 36 13.9 9 51. 257 42 13.9 9; 258 0 13.9 12; 259 6 13.9 12; 260 12 13.9 12; 261 18 13.9 12 52. 262 24 13.9 12; 263 30 13.9 12; 264 36 13.9 12; 265 42 13.9 12; 266 0 17.1 0 53. 267 6 17.1 0; 268 12 17.1 0; 269 18 17.1 0; 270 24 17.1 0; 271 30 17.1 0 54. 272 36 17.1 0; 273 42 17.1 0; 274 0 17.1 3; 275 6 17.1 3; 276 12 17.1 3 55. 277 18 17.1 3; 278 24 17.1 3; 279 30 17.1 3; 280 36 17.1 3; 281 42 17.1 3 56. 282 0 17.1 6; 283 6 17.1 6; 284 12 17.1 6; 285 18 17.1 6; 286 24 17.1 6 57. 287 30 17.1 6; 288 36 17.1 6; 289 42 17.1 6; 290 0 17.1 9; 291 6 17.1 9 58. 292 12 17.1 9; 293 18 17.1 9; 294 24 17.1 9; 295 30 17.1 9; 296 36 17.1 9 59. 297 42 17.1 9; 298 0 17.1 12; 299 6 17.1 12; 300 12 17.1 12; 301 18 17.1 12 60. 302 24 17.1 12; 303 30 17.1 12; 304 36 17.1 12; 305 42 17.1 12; 306 0 20.3 0 61. 307 6 20.3 0; 308 12 20.3 0; 309 18 20.3 0; 310 24 20.3 0; 311 30 20.3 0 62. 312 36 20.3 0; 313 42 20.3 0; 314 0 20.3 3; 315 6 20.3 3; 316 12 20.3 3 63. 317 18 20.3 3; 318 24 20.3 3; 319 30 20.3 3; 320 36 20.3 3; 321 42 20.3 3 64. 322 0 20.3 6; 323 6 20.3 6; 324 12 20.3 6; 325 18 20.3 6; 326 24 20.3 6 65. 327 30 20.3 6; 328 36 20.3 6; 329 42 20.3 6; 330 0 20.3 9; 331 6 20.3 9 66. 332 12 20.3 9; 333 18 20.3 9; 334 24 20.3 9; 335 30 20.3 9; 336 36 20.3 9 67. 337 42 20.3 9; 338 0 20.3 12; 339 6 20.3 12; 340 12 20.3 12; 341 18 20.3 12 68. 342 24 20.3 12; 343 30 20.3 12; 344 36 20.3 12; 345 42 20.3 12; 346 0 23.5 0 69. 347 6 23.5 0; 348 12 23.5 0; 349 18 23.5 0; 350 24 23.5 0; 351 30 23.5 0 70. 352 36 23.5 0; 353 42 23.5 0; 354 0 23.5 3; 355 6 23.5 3; 356 12 23.5 3 71. 357 18 23.5 3; 358 24 23.5 3; 359 30 23.5 3; 360 36 23.5 3; 361 42 23.5 3 72. 362 0 23.5 6; 363 6 23.5 6; 364 12 23.5 6; 365 18 23.5 6; 366 24 23.5 6 73. 367 30 23.5 6; 368 36 23.5 6; 369 42 23.5 6; 370 0 23.5 9; 371 6 23.5 9 74. 372 12 23.5 9; 373 18 23.5 9; 374 24 23.5 9; 375 30 23.5 9; 376 36 23.5 9 75. 377 42 23.5 9; 378 0 23.5 12; 379 6 23.5 12; 380 12 23.5 12; 381 18 23.5 12 76. 382 24 23.5 12; 383 30 23.5 12; 384 36 23.5 12; 385 42 23.5 12; 386 0 26.7 0 77. 387 6 26.7 0; 388 12 26.7 0; 389 18 26.7 0; 390 24 26.7 0; 391 30 26.7 0 78. 392 36 26.7 0; 393 42 26.7 0; 394 0 26.7 3; 395 6 26.7 3; 396 12 26.7 3 79. 397 18 26.7 3; 398 24 26.7 3; 399 30 26.7 3; 400 36 26.7 3; 401 42 26.7 3 80. 402 0 26.7 6; 403 6 26.7 6; 404 12 26.7 6; 405 18 26.7 6; 406 24 26.7 6 81. 407 30 26.7 6; 408 36 26.7 6; 409 42 26.7 6; 410 0 26.7 9; 411 6 26.7 9 82. 412 12 26.7 9; 413 18 26.7 9; 414 24 26.7 9; 415 30 26.7 9; 416 36 26.7 9 83. 417 42 26.7 9; 418 0 26.7 12; 419 6 26.7 12; 420 12 26.7 12; 421 18 26.7 12 84. 422 24 26.7 12; 423 30 26.7 12; 424 36 26.7 12; 425 42 26.7 12; 426 0 29.9 0 85. 427 6 29.9 0; 428 12 29.9 0; 429 18 29.9 0; 430 24 29.9 0; 431 30 29.9 0 86. 432 36 29.9 0; 433 42 29.9 0; 434 0 29.9 3; 435 6 29.9 3; 436 12 29.9 3 87. 437 18 29.9 3; 438 24 29.9 3; 439 30 29.9 3; 440 36 29.9 3; 441 42 29.9 3 88. 442 0 29.9 6; 443 6 29.9 6; 444 12 29.9 6; 445 18 29.9 6; 446 24 29.9 6 89. 447 30 29.9 6; 448 36 29.9 6; 449 42 29.9 6; 450 0 29.9 9; 451 6 29.9 9 90. 452 12 29.9 9; 453 18 29.9 9; 454 24 29.9 9; 455 30 29.9 9; 456 36 29.9 9 91. 457 42 29.9 9; 458 0 29.9 12; 459 6 29.9 12; 460 12 29.9 12; 461 18 29.9 12 92. 462 24 29.9 12; 463 30 29.9 12; 464 36 29.9 12; 465 42 29.9 12; 466 0 33.1 0 93. 467 6 33.1 0; 468 12 33.1 0; 469 18 33.1 0; 470 24 33.1 0; 471 30 33.1 0 94. 472 36 33.1 0; 473 42 33.1 0; 474 0 33.1 3; 475 6 33.1 3; 476 12 33.1 3 95. 477 18 33.1 3; 478 24 33.1 3; 479 30 33.1 3; 480 36 33.1 3; 481 42 33.1 3 96. 482 0 33.1 6; 483 6 33.1 6; 484 12 33.1 6; 485 18 33.1 6; 486 24 33.1 6 97. 487 30 33.1 6; 488 36 33.1 6; 489 42 33.1 6; 490 0 33.1 9; 491 6 33.1 9 98. 492 12 33.1 9; 493 18 33.1 9; 494 24 33.1 9; 495 30 33.1 9; 496 36 33.1 9 99. 497 42 33.1 9; 498 0 33.1 12; 499 6 33.1 12; 500 12 33.1 12; 501 18 33.1 12 100. 502 24 33.1 12; 503 30 33.1 12; 504 36 33.1 12; 505 42 33.1 12; 506 0 36.3 0 101. 507 6 36.3 0; 508 12 36.3 0; 509 18 36.3 0; 510 24 36.3 0; 511 30 36.3 0 102. 512 36 36.3 0; 513 42 36.3 0; 514 0 36.3 3; 515 6 36.3 3; 516 12 36.3 3 103. 517 18 36.3 3; 518 24 36.3 3; 519 30 36.3 3; 520 36 36.3 3; 521 42 36.3 3 104. 522 0 36.3 6; 523 6 36.3 6; 524 12 36.3 6; 525 18 36.3 6; 526 24 36.3 6 105. 527 30 36.3 6; 528 36 36.3 6; 529 42 36.3 6; 530 0 36.3 9; 531 6 36.3 9 106. 532 12 36.3 9; 533 18 36.3 9; 534 24 36.3 9; 535 30 36.3 9; 536 36 36.3 9 107. 537 42 36.3 9; 538 0 36.3 12; 539 6 36.3 12; 540 12 36.3 12; 541 18 36.3 12

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108. 542 24 36.3 12; 543 30 36.3 12; 544 36 36.3 12; 545 42 36.3 12; 546 0 39.5 0 109. 547 6 39.5 0; 548 12 39.5 0; 549 18 39.5 0; 550 24 39.5 0; 551 30 39.5 0 110. 552 36 39.5 0; 553 42 39.5 0; 554 0 39.5 3; 555 6 39.5 3; 556 12 39.5 3 111. 557 18 39.5 3; 558 24 39.5 3; 559 30 39.5 3; 560 36 39.5 3; 561 42 39.5 3 112. 562 0 39.5 6; 563 6 39.5 6; 564 12 39.5 6; 565 18 39.5 6; 566 24 39.5 6 113. 567 30 39.5 6; 568 36 39.5 6; 569 42 39.5 6; 570 0 39.5 9; 571 6 39.5 9 114. 572 12 39.5 9; 573 18 39.5 9; 574 24 39.5 9; 575 30 39.5 9; 576 36 39.5 9 115. 577 42 39.5 9; 578 0 39.5 12; 579 6 39.5 12; 580 12 39.5 12; 581 18 39.5 12 116. 582 24 39.5 12; 583 30 39.5 12; 584 36 39.5 12; 585 42 39.5 12; 586 0 42.7 0 117. 587 6 42.7 0; 588 12 42.7 0; 589 18 42.7 0; 590 24 42.7 0; 591 30 42.7 0 118. 592 36 42.7 0; 593 42 42.7 0; 594 0 42.7 3; 595 6 42.7 3; 596 12 42.7 3 119. 597 18 42.7 3; 598 24 42.7 3; 599 30 42.7 3; 600 36 42.7 3; 601 42 42.7 3 120. 602 0 42.7 6; 603 6 42.7 6; 604 12 42.7 6; 605 18 42.7 6; 606 24 42.7 6 121. 607 30 42.7 6; 608 36 42.7 6; 609 42 42.7 6; 610 0 42.7 9; 611 6 42.7 9 122. 612 12 42.7 9; 613 18 42.7 9; 614 24 42.7 9; 615 30 42.7 9; 616 36 42.7 9 123. 617 42 42.7 9; 618 0 42.7 12; 619 6 42.7 12; 620 12 42.7 12; 621 18 42.7 12 124. 622 24 42.7 12; 623 30 42.7 12; 624 36 42.7 12; 625 42 42.7 12; 626 0 0 15 125. 627 0 1.5 15; 628 6 0 15; 629 6 1.5 15; 630 12 0 15; 631 12 1.5 15 126. 632 18 0 15; 633 18 1.5 15; 634 24 0 15; 635 24 1.5 15; 636 30 0 15 127. 637 30 1.5 15; 638 36 0 15; 639 36 1.5 15; 640 42 0 15; 641 42 1.5 15 128. 642 0 4.3 15; 643 6 4.3 15; 644 12 4.3 15; 645 18 4.3 15; 646 24 4.3 15 129. 647 30 4.3 15; 648 36 4.3 15; 649 42 4.3 15; 650 0 7.5 15; 651 6 7.5 15 130. 652 12 7.5 15; 653 18 7.5 15; 654 24 7.5 15; 655 30 7.5 15; 656 36 7.5 15 131. 657 42 7.5 15; 658 0 10.7 15; 659 6 10.7 15; 660 12 10.7 15; 661 18 10.7 15 132. 662 24 10.7 15; 663 30 10.7 15; 664 36 10.7 15; 665 42 10.7 15; 666 0 13.9 15 133. 667 6 13.9 15; 668 12 13.9 15; 669 18 13.9 15; 670 24 13.9 15; 671 30 13.9 15 134. 672 36 13.9 15; 673 42 13.9 15; 674 0 17.1 15; 675 6 17.1 15; 676 12 17.1 15 135. 677 18 17.1 15; 678 24 17.1 15; 679 30 17.1 15; 680 36 17.1 15; 681 42 17.1 15 136. 682 0 20.3 15; 683 6 20.3 15; 684 12 20.3 15; 685 18 20.3 15; 686 24 20.3 15 137. 687 30 20.3 15; 688 36 20.3 15; 689 42 20.3 15; 690 0 23.5 15; 691 6 23.5 15 138. 692 12 23.5 15; 693 18 23.5 15; 694 24 23.5 15; 695 30 23.5 15; 696 36 23.5 15 139. 697 42 23.5 15; 698 0 26.7 15; 699 6 26.7 15; 700 12 26.7 15; 701 18 26.7 15 140. 702 24 26.7 15; 703 30 26.7 15; 704 36 26.7 15; 705 42 26.7 15; 706 0 29.9 15 141. 707 6 29.9 15; 708 12 29.9 15; 709 18 29.9 15; 710 24 29.9 15; 711 30 29.9 15 142. 712 36 29.9 15; 713 42 29.9 15; 714 0 33.1 15; 715 6 33.1 15; 716 12 33.1 15 143. 717 18 33.1 15; 718 24 33.1 15; 719 30 33.1 15; 720 36 33.1 15; 721 42 33.1 15 144. 722 0 36.3 15; 723 6 36.3 15; 724 12 36.3 15; 725 18 36.3 15; 726 24 36.3 15 145. 727 30 36.3 15; 728 36 36.3 15; 729 42 36.3 15; 730 0 39.5 15; 731 6 39.5 15 146. 732 12 39.5 15; 733 18 39.5 15; 734 24 39.5 15; 735 30 39.5 15; 736 36 39.5 15 147. 737 42 39.5 15; 738 0 42.7 15; 739 6 42.7 15; 740 12 42.7 15; 741 18 42.7 15 148. 742 24 42.7 15; 743 30 42.7 15; 744 36 42.7 15; 745 42 42.7 15 149. MEMBER INCIDENCES 150. 1 1 66; 2 7 67; 3 28 68; 4 29 69; 5 30 70; 6 31 71; 7 32 72; 8 33 73; 9 34 74 151. 10 35 75; 11 36 76; 12 37 77; 13 38 78; 14 39 79; 15 40 80; 16 41 81; 17 42 82 152. 18 43 83; 19 44 84; 20 45 85; 21 46 86; 22 47 87; 23 48 88; 24 49 89; 25 50 90 153. 26 51 91; 27 52 92; 28 53 93; 29 54 94; 30 55 95; 31 56 96; 32 57 97; 33 58 98 154. 34 59 99; 35 60 100; 36 61 101; 37 62 102; 38 63 103; 39 64 104; 40 65 105 155. 41 66 67; 42 67 68; 43 68 69; 44 69 70; 45 70 71; 46 71 72; 47 72 73; 48 74 75 156. 49 75 76; 50 76 77; 51 77 78; 52 78 79; 53 79 80; 54 80 81; 55 82 83; 56 83 84 157. 57 84 85; 58 85 86; 59 86 87; 60 87 88; 61 88 89; 62 90 91; 63 91 92; 64 92 93 158. 65 93 94; 66 94 95; 67 95 96; 68 96 97; 69 98 99; 70 99 100; 71 100 101 159. 72 101 102; 73 102 103; 74 103 104; 75 104 105; 76 66 74; 77 74 82; 78 82 90 160. 79 90 98; 80 67 75; 81 75 83; 82 83 91; 83 91 99; 84 68 76; 85 76 84; 86 84 92 161. 87 92 100; 88 69 77; 89 77 85; 90 85 93; 91 93 101; 92 70 78; 93 78 86 162. 94 86 94; 95 94 102; 96 71 79; 97 79 87; 98 87 95; 99 95 103; 100 72 80 163. 101 80 88; 102 88 96; 103 96 104; 104 73 81; 105 81 89; 106 89 97; 107 97 105 164. 108 66 106; 109 67 107; 110 68 108; 111 69 109; 112 70 110; 113 71 111 165. 114 72 112; 115 73 113; 116 74 114; 117 75 115; 118 76 116; 119 77 117 166. 120 78 118; 121 79 119; 122 80 120; 123 81 121; 124 82 122; 125 83 123 167. 126 84 124; 127 85 125; 128 86 126; 129 87 127; 130 88 128; 131 89 129 168. 132 90 130; 133 91 131; 134 92 132; 135 93 133; 136 94 134; 137 95 135 169. 138 96 136; 139 97 137; 140 98 138; 141 99 139; 142 100 140; 143 101 141 170. 144 102 142; 145 103 143; 146 104 144; 147 105 145; 148 106 107; 149 107 108

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171. 150 108 109; 151 109 110; 152 110 111; 153 111 112; 154 112 113; 155 114 115 172. 156 115 116; 157 116 117; 158 117 118; 159 118 119; 160 119 120; 161 120 121 173. 162 122 123; 163 123 124; 164 124 125; 165 125 126; 166 126 127; 167 127 128 174. 168 128 129; 169 130 131; 170 131 132; 171 132 133; 172 133 134; 173 134 135 175. 174 135 136; 175 136 137; 176 138 139; 177 139 140; 178 140 141; 179 141 142 176. 180 142 143; 181 143 144; 182 144 145; 183 106 114; 184 114 122; 185 122 130 177. 186 130 138; 187 107 115; 188 115 123; 189 123 131; 190 131 139; 191 108 116 178. 192 116 124; 193 124 132; 194 132 140; 195 109 117; 196 117 125; 197 125 133 179. 198 133 141; 199 110 118; 200 118 126; 201 126 134; 202 134 142; 203 111 119 180. 204 119 127; 205 127 135; 206 135 143; 207 112 120; 208 120 128; 209 128 136 181. 210 136 144; 211 113 121; 212 121 129; 213 129 137; 214 137 145; 215 106 146 182. 216 107 147; 217 108 148; 218 109 149; 219 110 150; 220 111 151; 221 112 152 183. 222 113 153; 223 114 154; 224 115 155; 225 116 156; 226 117 157; 227 118 158 184. 228 119 159; 229 120 160; 230 121 161; 231 122 162; 232 123 163; 233 124 164 185. 234 125 165; 235 126 166; 236 127 167; 237 128 168; 238 129 169; 239 130 170 186. 240 131 171; 241 132 172; 242 133 173; 243 134 174; 244 135 175; 245 136 176 187. 246 137 177; 247 138 178; 248 139 179; 249 140 180; 250 141 181; 251 142 182 188. 252 143 183; 253 144 184; 254 145 185; 255 146 147; 256 147 148; 257 148 149 189. 258 149 150; 259 150 151; 260 151 152; 261 152 153; 262 154 155; 263 155 156 190. 264 156 157; 265 157 158; 266 158 159; 267 159 160; 268 160 161; 269 162 163 191. 270 163 164; 271 164 165; 272 165 166; 273 166 167; 274 167 168; 275 168 169 192. 276 170 171; 277 171 172; 278 172 173; 279 173 174; 280 174 175; 281 175 176 193. 282 176 177; 283 178 179; 284 179 180; 285 180 181; 286 181 182; 287 182 183 194. 288 183 184; 289 184 185; 290 146 154; 291 154 162; 292 162 170; 293 170 178 195. 294 147 155; 295 155 163; 296 163 171; 297 171 179; 298 148 156; 299 156 164 196. 300 164 172; 301 172 180; 302 149 157; 303 157 165; 304 165 173; 305 173 181 197. 306 150 158; 307 158 166; 308 166 174; 309 174 182; 310 151 159; 311 159 167 198. 312 167 175; 313 175 183; 314 152 160; 315 160 168; 316 168 176; 317 176 184 199. 318 153 161; 319 161 169; 320 169 177; 321 177 185; 322 146 186; 323 147 187 200. 324 148 188; 325 149 189; 326 150 190; 327 151 191; 328 152 192; 329 153 193 201. 330 154 194; 331 155 195; 332 156 196; 333 157 197; 334 158 198; 335 159 199 202. 336 160 200; 337 161 201; 338 162 202; 339 163 203; 340 164 204; 341 165 205 203. 342 166 206; 343 167 207; 344 168 208; 345 169 209; 346 170 210; 347 171 211 204. 348 172 212; 349 173 213; 350 174 214; 351 175 215; 352 176 216; 353 177 217 205. 354 178 218; 355 179 219; 356 180 220; 357 181 221; 358 182 222; 359 183 223 206. 360 184 224; 361 185 225; 362 186 187; 363 187 188; 364 188 189; 365 189 190 207. 366 190 191; 367 191 192; 368 192 193; 369 194 195; 370 195 196; 371 196 197 208. 372 197 198; 373 198 199; 374 199 200; 375 200 201; 376 202 203; 377 203 204 209. 378 204 205; 379 205 206; 380 206 207; 381 207 208; 382 208 209; 383 210 211 210. 384 211 212; 385 212 213; 386 213 214; 387 214 215; 388 215 216; 389 216 217 211. 390 218 219; 391 219 220; 392 220 221; 393 221 222; 394 222 223; 395 223 224 212. 396 224 225; 397 186 194; 398 194 202; 399 202 210; 400 210 218; 401 187 195 213. 402 195 203; 403 203 211; 404 211 219; 405 188 196; 406 196 204; 407 204 212 214. 408 212 220; 409 189 197; 410 197 205; 411 205 213; 412 213 221; 413 190 198 215. 414 198 206; 415 206 214; 416 214 222; 417 191 199; 418 199 207; 419 207 215 216. 420 215 223; 421 192 200; 422 200 208; 423 208 216; 424 216 224; 425 193 201 217. 426 201 209; 427 209 217; 428 217 225; 429 186 226; 430 187 227; 431 188 228 218. 432 189 229; 433 190 230; 434 191 231; 435 192 232; 436 193 233; 437 194 234 219. 438 195 235; 439 196 236; 440 197 237; 441 198 238; 442 199 239; 443 200 240 220. 444 201 241; 445 202 242; 446 203 243; 447 204 244; 448 205 245; 449 206 246 221. 450 207 247; 451 208 248; 452 209 249; 453 210 250; 454 211 251; 455 212 252 222. 456 213 253; 457 214 254; 458 215 255; 459 216 256; 460 217 257; 461 218 258 223. 462 219 259; 463 220 260; 464 221 261; 465 222 262; 466 223 263; 467 224 264 224. 468 225 265; 469 226 227; 470 227 228; 471 228 229; 472 229 230; 473 230 231 225. 474 231 232; 475 232 233; 476 234 235; 477 235 236; 478 236 237; 479 237 238 226. 480 238 239; 481 239 240; 482 240 241; 483 242 243; 484 243 244; 485 244 245 227. 486 245 246; 487 246 247; 488 247 248; 489 248 249; 490 250 251; 491 251 252 228. 492 252 253; 493 253 254; 494 254 255; 495 255 256; 496 256 257; 497 258 259 229. 498 259 260; 499 260 261; 500 261 262; 501 262 263; 502 263 264; 503 264 265 230. 504 226 234; 505 234 242; 506 242 250; 507 250 258; 508 227 235; 509 235 243 231. 510 243 251; 511 251 259; 512 228 236; 513 236 244; 514 244 252; 515 252 260 232. 516 229 237; 517 237 245; 518 245 253; 519 253 261; 520 230 238; 521 238 246 233. 522 246 254; 523 254 262; 524 231 239; 525 239 247; 526 247 255; 527 255 263

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234. 528 232 240; 529 240 248; 530 248 256; 531 256 264; 532 233 241; 533 241 249 235. 534 249 257; 535 257 265; 536 226 266; 537 227 267; 538 228 268; 539 229 269 236. 540 230 270; 541 231 271; 542 232 272; 543 233 273; 544 234 274; 545 235 275 237. 546 236 276; 547 237 277; 548 238 278; 549 239 279; 550 240 280; 551 241 281 238. 552 242 282; 553 243 283; 554 244 284; 555 245 285; 556 246 286; 557 247 287 239. 558 248 288; 559 249 289; 560 250 290; 561 251 291; 562 252 292; 563 253 293 240. 564 254 294; 565 255 295; 566 256 296; 567 257 297; 568 258 298; 569 259 299 241. 570 260 300; 571 261 301; 572 262 302; 573 263 303; 574 264 304; 575 265 305 242. 576 266 267; 577 267 268; 578 268 269; 579 269 270; 580 270 271; 581 271 272 243. 582 272 273; 583 274 275; 584 275 276; 585 276 277; 586 277 278; 587 278 279 244. 588 279 280; 589 280 281; 590 282 283; 591 283 284; 592 284 285; 593 285 286 245. 594 286 287; 595 287 288; 596 288 289; 597 290 291; 598 291 292; 599 292 293 246. 600 293 294; 601 294 295; 602 295 296; 603 296 297; 604 298 299; 605 299 300 247. 606 300 301; 607 301 302; 608 302 303; 609 303 304; 610 304 305; 611 266 274 248. 612 274 282; 613 282 290; 614 290 298; 615 267 275; 616 275 283; 617 283 291 249. 618 291 299; 619 268 276; 620 276 284; 621 284 292; 622 292 300; 623 269 277 250. 624 277 285; 625 285 293; 626 293 301; 627 270 278; 628 278 286; 629 286 294 251. 630 294 302; 631 271 279; 632 279 287; 633 287 295; 634 295 303; 635 272 280 252. 636 280 288; 637 288 296; 638 296 304; 639 273 281; 640 281 289; 641 289 297 253. 642 297 305; 643 266 306; 644 267 307; 645 268 308; 646 269 309; 647 270 310 254. 648 271 311; 649 272 312; 650 273 313; 651 274 314; 652 275 315; 653 276 316 255. 654 277 317; 655 278 318; 656 279 319; 657 280 320; 658 281 321; 659 282 322 256. 660 283 323; 661 284 324; 662 285 325; 663 286 326; 664 287 327; 665 288 328 257. 666 289 329; 667 290 330; 668 291 331; 669 292 332; 670 293 333; 671 294 334 258. 672 295 335; 673 296 336; 674 297 337; 675 298 338; 676 299 339; 677 300 340 259. 678 301 341; 679 302 342; 680 303 343; 681 304 344; 682 305 345; 683 306 307 260. 684 307 308; 685 308 309; 686 309 310; 687 310 311; 688 311 312; 689 312 313 261. 690 314 315; 691 315 316; 692 316 317; 693 317 318; 694 318 319; 695 319 320 262. 696 320 321; 697 322 323; 698 323 324; 699 324 325; 700 325 326; 701 326 327 263. 702 327 328; 703 328 329; 704 330 331; 705 331 332; 706 332 333; 707 333 334 264. 708 334 335; 709 335 336; 710 336 337; 711 338 339; 712 339 340; 713 340 341 265. 714 341 342; 715 342 343; 716 343 344; 717 344 345; 718 306 314; 719 314 322 266. 720 322 330; 721 330 338; 722 307 315; 723 315 323; 724 323 331; 725 331 339 267. 726 308 316; 727 316 324; 728 324 332; 729 332 340; 730 309 317; 731 317 325 268. 732 325 333; 733 333 341; 734 310 318; 735 318 326; 736 326 334; 737 334 342 269. 738 311 319; 739 319 327; 740 327 335; 741 335 343; 742 312 320; 743 320 328 270. 744 328 336; 745 336 344; 746 313 321; 747 321 329; 748 329 337; 749 337 345 271. 750 306 346; 751 307 347; 752 308 348; 753 309 349; 754 310 350; 755 311 351 272. 756 312 352; 757 313 353; 758 314 354; 759 315 355; 760 316 356; 761 317 357 273. 762 318 358; 763 319 359; 764 320 360; 765 321 361; 766 322 362; 767 323 363 274. 768 324 364; 769 325 365; 770 326 366; 771 327 367; 772 328 368; 773 329 369 275. 774 330 370; 775 331 371; 776 332 372; 777 333 373; 778 334 374; 779 335 375 276. 780 336 376; 781 337 377; 782 338 378; 783 339 379; 784 340 380; 785 341 381 277. 786 342 382; 787 343 383; 788 344 384; 789 345 385; 790 346 347; 791 347 348 278. 792 348 349; 793 349 350; 794 350 351; 795 351 352; 796 352 353; 797 354 355 279. 798 355 356; 799 356 357; 800 357 358; 801 358 359; 802 359 360; 803 360 361 280. 804 362 363; 805 363 364; 806 364 365; 807 365 366; 808 366 367; 809 367 368 281. 810 368 369; 811 370 371; 812 371 372; 813 372 373; 814 373 374; 815 374 375 282. 816 375 376; 817 376 377; 818 378 379; 819 379 380; 820 380 381; 821 381 382 283. 822 382 383; 823 383 384; 824 384 385; 825 346 354; 826 354 362; 827 362 370 284. 828 370 378; 829 347 355; 830 355 363; 831 363 371; 832 371 379; 833 348 356 285. 834 356 364; 835 364 372; 836 372 380; 837 349 357; 838 357 365; 839 365 373 286. 840 373 381; 841 350 358; 842 358 366; 843 366 374; 844 374 382; 845 351 359 287. 846 359 367; 847 367 375; 848 375 383; 849 352 360; 850 360 368; 851 368 376 288. 852 376 384; 853 353 361; 854 361 369; 855 369 377; 856 377 385; 857 346 386 289. 858 347 387; 859 348 388; 860 349 389; 861 350 390; 862 351 391; 863 352 392 290. 864 353 393; 865 354 394; 866 355 395; 867 356 396; 868 357 397; 869 358 398 291. 870 359 399; 871 360 400; 872 361 401; 873 362 402; 874 363 403; 875 364 404 292. 876 365 405; 877 366 406; 878 367 407; 879 368 408; 880 369 409; 881 370 410 293. 882 371 411; 883 372 412; 884 373 413; 885 374 414; 886 375 415; 887 376 416 294. 888 377 417; 889 378 418; 890 379 419; 891 380 420; 892 381 421; 893 382 422 295. 894 383 423; 895 384 424; 896 385 425; 897 386 387; 898 387 388; 899 388 389 296. 900 389 390; 901 390 391; 902 391 392; 903 392 393; 904 394 395; 905 395 396

Page 62: Project File- Finite Element

297. 906 396 397; 907 397 398; 908 398 399; 909 399 400; 910 400 401; 911 402 403 298. 912 403 404; 913 404 405; 914 405 406; 915 406 407; 916 407 408; 917 408 409 299. 918 410 411; 919 411 412; 920 412 413; 921 413 414; 922 414 415; 923 415 416 300. 924 416 417; 925 418 419; 926 419 420; 927 420 421; 928 421 422; 929 422 423 301. 930 423 424; 931 424 425; 932 386 394; 933 394 402; 934 402 410; 935 410 418 302. 936 387 395; 937 395 403; 938 403 411; 939 411 419; 940 388 396; 941 396 404 303. 942 404 412; 943 412 420; 944 389 397; 945 397 405; 946 405 413; 947 413 421 304. 948 390 398; 949 398 406; 950 406 414; 951 414 422; 952 391 399; 953 399 407 305. 954 407 415; 955 415 423; 956 392 400; 957 400 408; 958 408 416; 959 416 424 306. 960 393 401; 961 401 409; 962 409 417; 963 417 425; 964 386 426; 965 387 427 307. 966 388 428; 967 389 429; 968 390 430; 969 391 431; 970 392 432; 971 393 433 308. 972 394 434; 973 395 435; 974 396 436; 975 397 437; 976 398 438; 977 399 439 309. 978 400 440; 979 401 441; 980 402 442; 981 403 443; 982 404 444; 983 405 445 310. 984 406 446; 985 407 447; 986 408 448; 987 409 449; 988 410 450; 989 411 451 311. 990 412 452; 991 413 453; 992 414 454; 993 415 455; 994 416 456; 995 417 457 312. 996 418 458; 997 419 459; 998 420 460; 999 421 461; 1000 422 462; 1001 423 463 313. 1002 424 464; 1003 425 465; 1004 426 427; 1005 427 428; 1006 428 429 314. 1007 429 430; 1008 430 431; 1009 431 432; 1010 432 433; 1011 434 435 315. 1012 435 436; 1013 436 437; 1014 437 438; 1015 438 439; 1016 439 440 316. 1017 440 441; 1018 442 443; 1019 443 444; 1020 444 445; 1021 445 446 317. 1022 446 447; 1023 447 448; 1024 448 449; 1025 450 451; 1026 451 452 318. 1027 452 453; 1028 453 454; 1029 454 455; 1030 455 456; 1031 456 457 319. 1032 458 459; 1033 459 460; 1034 460 461; 1035 461 462; 1036 462 463 320. 1037 463 464; 1038 464 465; 1039 426 434; 1040 434 442; 1041 442 450 321. 1042 450 458; 1043 427 435; 1044 435 443; 1045 443 451; 1046 451 459 322. 1047 428 436; 1048 436 444; 1049 444 452; 1050 452 460; 1051 429 437 323. 1052 437 445; 1053 445 453; 1054 453 461; 1055 430 438; 1056 438 446 324. 1057 446 454; 1058 454 462; 1059 431 439; 1060 439 447; 1061 447 455 325. 1062 455 463; 1063 432 440; 1064 440 448; 1065 448 456; 1066 456 464 326. 1067 433 441; 1068 441 449; 1069 449 457; 1070 457 465; 1071 426 466 327. 1072 427 467; 1073 428 468; 1074 429 469; 1075 430 470; 1076 431 471 328. 1077 432 472; 1078 433 473; 1079 434 474; 1080 435 475; 1081 436 476 329. 1082 437 477; 1083 438 478; 1084 439 479; 1085 440 480; 1086 441 481 330. 1087 442 482; 1088 443 483; 1089 444 484; 1090 445 485; 1091 446 486 331. 1092 447 487; 1093 448 488; 1094 449 489; 1095 450 490; 1096 451 491 332. 1097 452 492; 1098 453 493; 1099 454 494; 1100 455 495; 1101 456 496 333. 1102 457 497; 1103 458 498; 1104 459 499; 1105 460 500; 1106 461 501 334. 1107 462 502; 1108 463 503; 1109 464 504; 1110 465 505; 1111 466 467 335. 1112 467 468; 1113 468 469; 1114 469 470; 1115 470 471; 1116 471 472 336. 1117 472 473; 1118 474 475; 1119 475 476; 1120 476 477; 1121 477 478 337. 1122 478 479; 1123 479 480; 1124 480 481; 1125 482 483; 1126 483 484 338. 1127 484 485; 1128 485 486; 1129 486 487; 1130 487 488; 1131 488 489 339. 1132 490 491; 1133 491 492; 1134 492 493; 1135 493 494; 1136 494 495 340. 1137 495 496; 1138 496 497; 1139 498 499; 1140 499 500; 1141 500 501 341. 1142 501 502; 1143 502 503; 1144 503 504; 1145 504 505; 1146 466 474 342. 1147 474 482; 1148 482 490; 1149 490 498; 1150 467 475; 1151 475 483 343. 1152 483 491; 1153 491 499; 1154 468 476; 1155 476 484; 1156 484 492 344. 1157 492 500; 1158 469 477; 1159 477 485; 1160 485 493; 1161 493 501 345. 1162 470 478; 1163 478 486; 1164 486 494; 1165 494 502; 1166 471 479 346. 1167 479 487; 1168 487 495; 1169 495 503; 1170 472 480; 1171 480 488 347. 1172 488 496; 1173 496 504; 1174 473 481; 1175 481 489; 1176 489 497 348. 1177 497 505; 1178 466 506; 1179 467 507; 1180 468 508; 1181 469 509 349. 1182 470 510; 1183 471 511; 1184 472 512; 1185 473 513; 1186 474 514 350. 1187 475 515; 1188 476 516; 1189 477 517; 1190 478 518; 1191 479 519 351. 1192 480 520; 1193 481 521; 1194 482 522; 1195 483 523; 1196 484 524 352. 1197 485 525; 1198 486 526; 1199 487 527; 1200 488 528; 1201 489 529 353. 1202 490 530; 1203 491 531; 1204 492 532; 1205 493 533; 1206 494 534 354. 1207 495 535; 1208 496 536; 1209 497 537; 1210 498 538; 1211 499 539 355. 1212 500 540; 1213 501 541; 1214 502 542; 1215 503 543; 1216 504 544 356. 1217 505 545; 1218 506 507; 1219 507 508; 1220 508 509; 1221 509 510 357. 1222 510 511; 1223 511 512; 1224 512 513; 1225 514 515; 1226 515 516 358. 1227 516 517; 1228 517 518; 1229 518 519; 1230 519 520; 1231 520 521 359. 1232 522 523; 1233 523 524; 1234 524 525; 1235 525 526; 1236 526 527

Page 63: Project File- Finite Element

360. 1237 527 528; 1238 528 529; 1239 530 531; 1240 531 532; 1241 532 533 361. 1242 533 534; 1243 534 535; 1244 535 536; 1245 536 537; 1246 538 539 362. 1247 539 540; 1248 540 541; 1249 541 542; 1250 542 543; 1251 543 544 363. 1252 544 545; 1253 506 514; 1254 514 522; 1255 522 530; 1256 530 538 364. 1257 507 515; 1258 515 523; 1259 523 531; 1260 531 539; 1261 508 516 365. 1262 516 524; 1263 524 532; 1264 532 540; 1265 509 517; 1266 517 525 366. 1267 525 533; 1268 533 541; 1269 510 518; 1270 518 526; 1271 526 534 367. 1272 534 542; 1273 511 519; 1274 519 527; 1275 527 535; 1276 535 543 368. 1277 512 520; 1278 520 528; 1279 528 536; 1280 536 544; 1281 513 521 369. 1282 521 529; 1283 529 537; 1284 537 545; 1285 506 546; 1286 507 547 370. 1287 508 548; 1288 509 549; 1289 510 550; 1290 511 551; 1291 512 552 371. 1292 513 553; 1293 514 554; 1294 515 555; 1295 516 556; 1296 517 557 372. 1297 518 558; 1298 519 559; 1299 520 560; 1300 521 561; 1301 522 562 373. 1302 523 563; 1303 524 564; 1304 525 565; 1305 526 566; 1306 527 567 374. 1307 528 568; 1308 529 569; 1309 530 570; 1310 531 571; 1311 532 572

Page 64: Project File- Finite Element

375. 1312 533 573; 1313 534 574; 1314 535 575; 1315 536 576; 1316 537 577 376. 1317 538 578; 1318 539 579; 1319 540 580; 1320 541 581; 1321 542 582 377. 1322 543 583; 1323 544 584; 1324 545 585; 1325 546 547; 1326 547 548 378. 1327 548 549; 1328 549 550; 1329 550 551; 1330 551 552; 1331 552 553 379. 1332 554 555; 1333 555 556; 1334 556 557; 1335 557 558; 1336 558 559 380. 1337 559 560; 1338 560 561; 1339 562 563; 1340 563 564; 1341 564 565 381. 1342 565 566; 1343 566 567; 1344 567 568; 1345 568 569; 1346 570 571 382. 1347 571 572; 1348 572 573; 1349 573 574; 1350 574 575; 1351 575 576 383. 1352 576 577; 1353 578 579; 1354 579 580; 1355 580 581; 1356 581 582 384. 1357 582 583; 1358 583 584; 1359 584 585; 1360 546 554; 1361 554 562 385. 1362 562 570; 1363 570 578; 1364 547 555; 1365 555 563; 1366 563 571 386. 1367 571 579; 1368 548 556; 1369 556 564; 1370 564 572; 1371 572 580 387. 1372 549 557; 1373 557 565; 1374 565 573; 1375 573 581; 1376 550 558 388. 1377 558 566; 1378 566 574; 1379 574 582; 1380 551 559; 1381 559 567 389. 1382 567 575; 1383 575 583; 1384 552 560; 1385 560 568; 1386 568 576 390. 1387 576 584; 1388 553 561; 1389 561 569; 1390 569 577; 1391 577 585 391. 1392 546 586; 1393 547 587; 1394 548 588; 1395 549 589; 1396 550 590 392. 1397 551 591; 1398 552 592; 1399 553 593; 1400 554 594; 1401 555 595 393. 1402 556 596; 1403 557 597; 1404 558 598; 1405 559 599; 1406 560 600 394. 1407 561 601; 1408 562 602; 1409 563 603; 1410 564 604; 1411 565 605 395. 1412 566 606; 1413 567 607; 1414 568 608; 1415 569 609; 1416 570 610 396. 1417 571 611; 1418 572 612; 1419 573 613; 1420 574 614; 1421 575 615 397. 1422 576 616; 1423 577 617; 1424 578 618; 1425 579 619; 1426 580 620 398. 1427 581 621; 1428 582 622; 1429 583 623; 1430 584 624; 1431 585 625 399. 1432 586 587; 1433 587 588; 1434 588 589; 1435 589 590; 1436 590 591 400. 1437 591 592; 1438 592 593; 1439 594 595; 1440 595 596; 1441 596 597 401. 1442 597 598; 1443 598 599; 1444 599 600; 1445 600 601; 1446 602 603 402. 1447 603 604; 1448 604 605; 1449 605 606; 1450 606 607; 1451 607 608 403. 1452 608 609; 1453 610 611; 1454 611 612; 1455 612 613; 1456 613 614 404. 1457 614 615; 1458 615 616; 1459 616 617; 1460 618 619; 1461 619 620 405. 1462 620 621; 1463 621 622; 1464 622 623; 1465 623 624; 1466 624 625 406. 1467 586 594; 1468 594 602; 1469 602 610; 1470 610 618; 1471 587 595 407. 1472 595 603; 1473 603 611; 1474 611 619; 1475 588 596; 1476 596 604 408. 1477 604 612; 1478 612 620; 1479 589 597; 1480 597 605; 1481 605 613 409. 1482 613 621; 1483 590 598; 1484 598 606; 1485 606 614; 1486 614 622 410. 1487 591 599; 1488 599 607; 1489 607 615; 1490 615 623; 1491 592 600 411. 1492 600 608; 1493 608 616; 1494 616 624; 1495 593 601; 1496 601 609 412. 1497 609 617; 1498 617 625; 1499 626 627; 1500 628 629; 1501 630 631 413. 1502 632 633; 1503 634 635; 1504 636 637; 1505 638 639; 1506 640 641 414. 1507 627 629; 1508 629 631; 1509 631 633; 1510 633 635; 1511 635 637 415. 1512 637 639; 1513 639 641; 1514 98 627; 1515 99 629; 1516 100 631 416. 1517 101 633; 1518 102 635; 1519 103 637; 1520 104 639; 1521 105 641 417. 1522 627 642; 1523 629 643; 1524 631 644; 1525 633 645; 1526 635 646 418. 1527 637 647; 1528 639 648; 1529 641 649; 1530 642 643; 1531 643 644 419. 1532 644 645; 1533 645 646; 1534 646 647; 1535 647 648; 1536 648 649 420. 1537 138 642; 1538 139 643; 1539 140 644; 1540 141 645; 1541 142 646 421. 1542 143 647; 1543 144 648; 1544 145 649; 1545 642 650; 1546 643 651 422. 1547 644 652; 1548 645 653; 1549 646 654; 1550 647 655; 1551 648 656 423. 1552 649 657; 1553 650 651; 1554 651 652; 1555 652 653; 1556 653 654 424. 1557 654 655; 1558 655 656; 1559 656 657; 1560 178 650; 1561 179 651 425. 1562 180 652; 1563 181 653; 1564 182 654; 1565 183 655; 1566 184 656 426. 1567 185 657; 1568 650 658; 1569 651 659; 1570 652 660; 1571 653 661 427. 1572 654 662; 1573 655 663; 1574 656 664; 1575 657 665; 1576 658 659 428. 1577 659 660; 1578 660 661; 1579 661 662; 1580 662 663; 1581 663 664 429. 1582 664 665; 1583 218 658; 1584 219 659; 1585 220 660; 1586 221 661 430. 1587 222 662; 1588 223 663; 1589 224 664; 1590 225 665; 1591 658 666 431. 1592 659 667; 1593 660 668; 1594 661 669; 1595 662 670; 1596 663 671 432. 1597 664 672; 1598 665 673; 1599 666 667; 1600 667 668; 1601 668 669 433. 1602 669 670; 1603 670 671; 1604 671 672; 1605 672 673; 1606 258 666 434. 1607 259 667; 1608 260 668; 1609 261 669; 1610 262 670; 1611 263 671

Page 65: Project File- Finite Element

435. 1612 264 672; 1613 265 673; 1614 666 674; 1615 667 675; 1616 668 676 436. 1617 669 677; 1618 670 678; 1619 671 679; 1620 672 680; 1621 673 681 437. 1622 674 675; 1623 675 676; 1624 676 677; 1625 677 678; 1626 678 679 438. 1627 679 680; 1628 680 681; 1629 298 674; 1630 299 675; 1631 300 676 439. 1632 301 677; 1633 302 678; 1634 303 679; 1635 304 680; 1636 305 681 440. 1637 674 682; 1638 675 683; 1639 676 684; 1640 677 685; 1641 678 686 441. 1642 679 687; 1643 680 688; 1644 681 689; 1645 682 683; 1646 683 684 442. 1647 684 685; 1648 685 686; 1649 686 687; 1650 687 688; 1651 688 689 443. 1652 338 682; 1653 339 683; 1654 340 684; 1655 341 685; 1656 342 686 444. 1657 343 687; 1658 344 688; 1659 345 689; 1660 682 690; 1661 683 691 445. 1662 684 692; 1663 685 693; 1664 686 694; 1665 687 695; 1666 688 696 446. 1667 689 697; 1668 690 691; 1669 691 692; 1670 692 693; 1671 693 694 447. 1672 694 695; 1673 695 696; 1674 696 697; 1675 378 690; 1676 379 691 448. 1677 380 692; 1678 381 693; 1679 382 694; 1680 383 695; 1681 384 696 449. 1682 385 697; 1683 690 698; 1684 691 699; 1685 692 700; 1686 693 701 450. 1687 694 702; 1688 695 703; 1689 696 704; 1690 697 705; 1691 698 699 451. 1692 699 700; 1693 700 701; 1694 701 702; 1695 702 703; 1696 703 704 452. 1697 704 705; 1698 418 698; 1699 419 699; 1700 420 700; 1701 421 701 453. 1702 422 702; 1703 423 703; 1704 424 704; 1705 425 705; 1706 698 706 454. 1707 699 707; 1708 700 708; 1709 701 709; 1710 702 710; 1711 703 711 455. 1712 704 712; 1713 705 713; 1714 706 707; 1715 707 708; 1716 708 709 456. 1717 709 710; 1718 710 711; 1719 711 712; 1720 712 713; 1721 458 706 457. 1722 459 707; 1723 460 708; 1724 461 709; 1725 462 710; 1726 463 711 458. 1727 464 712; 1728 465 713; 1729 706 714; 1730 707 715; 1731 708 716 459. 1732 709 717; 1733 710 718; 1734 711 719; 1735 712 720; 1736 713 721 460. 1737 714 715; 1738 715 716; 1739 716 717; 1740 717 718; 1741 718 719 461. 1742 719 720; 1743 720 721; 1744 498 714; 1745 499 715; 1746 500 716 462. 1747 501 717; 1748 502 718; 1749 503 719; 1750 504 720; 1751 505 721 463. 1752 714 722; 1753 715 723; 1754 716 724; 1755 717 725; 1756 718 726 464. 1757 719 727; 1758 720 728; 1759 721 729; 1760 722 723; 1761 723 724 465. 1762 724 725; 1763 725 726; 1764 726 727; 1765 727 728; 1766 728 729 466. 1767 538 722; 1768 539 723; 1769 540 724; 1770 541 725; 1771 542 726 467. 1772 543 727; 1773 544 728; 1774 545 729; 1775 722 730; 1776 723 731 468. 1777 724 732; 1778 725 733; 1779 726 734; 1780 727 735; 1781 728 736 469. 1782 729 737; 1783 730 731; 1784 731 732; 1785 732 733; 1786 733 734 470. 1787 734 735; 1788 735 736; 1789 736 737; 1790 578 730; 1791 579 731 471. 1792 580 732; 1793 581 733; 1794 582 734; 1795 583 735; 1796 584 736 472. 1797 585 737; 1798 730 738; 1799 731 739; 1800 732 740; 1801 733 741 473. 1802 734 742; 1803 735 743; 1804 736 744; 1805 737 745; 1806 738 739 474. 1807 739 740; 1808 740 741; 1809 741 742; 1810 742 743; 1811 743 744 475. 1812 744 745; 1813 618 738; 1814 619 739; 1815 620 740; 1816 621 741 476. 1817 622 742; 1818 623 743; 1819 624 744; 1820 625 745 477. DEFINE MATERIAL START 478. ISOTROPIC CONCRETE 479. E 2.17185E+007 480. POISSON 0.17 481. DENSITY 24 482. ALPHA 1E-005 483. DAMP 0.05 484. END DEFINE MATERIAL 485. MEMBER PROPERTY INDIAN 486. 148 TO 182 255 TO 289 362 TO 396 469 TO 503 576 TO 610 683 TO 717 790 TO 824 - 487. 897 TO 931 1004 TO 1038 1111 TO 1145 1218 TO 1252 1325 TO 1359 1432 TO 1466 - 488. 1530 TO 1536 1553 TO 1559 1576 TO 1582 1599 TO 1605 1622 TO 1628 - 489. 1645 TO 1651 1668 TO 1674 1691 TO 1697 1714 TO 1720 1737 TO 1743 - 490. 1760 TO 1766 1783 TO 1789 1806 TO 1812 PRIS YD 0.6 ZD 0.23 491. 41 TO 107 183 TO 214 290 TO 321 397 TO 428 504 TO 535 611 TO 642 718 TO 749 - 492. 825 TO 856 932 TO 963 1039 TO 1070 1146 TO 1177 1253 TO 1284 1360 TO 1391 - 493. 1467 TO 1498 1507 TO 1521 1537 TO 1544 1560 TO 1567 1583 TO 1590 - 494. 1606 TO 1613 1629 TO 1636 1652 TO 1659 1675 TO 1682 1698 TO 1705 - 495. 1721 TO 1728 1744 TO 1751 1767 TO 1774 1790 TO 1797 1813 TO 1819 - 496. 1820 PRIS YD 0.45 ZD 0.23 497. 438 TO 443 446 TO 451 454 TO 459 545 TO 550 553 TO 558 561 TO 566 652 TO 657 -

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498. 660 TO 665 668 TO 673 759 TO 764 767 TO 772 775 TO 780 866 TO 871 - 499. 874 TO 879 882 TO 887 973 TO 978 981 TO 986 989 TO 994 1080 TO 1085 1088 - 500. 1089 TO 1093 1096 TO 1101 1187 TO 1192 1195 TO 1200 1203 TO 1208 1294 TO 1299 - 501. 1302 TO 1307 1310 TO 1315 1401 TO 1406 1409 TO 1414 1417 TO 1421 - 502. 1422 PRIS YD 0.75 ZD 0.3 503. 429 TO 437 444 445 452 453 460 TO 468 536 TO 544 551 552 559 560 567 TO 575 - 504. 643 TO 651 658 659 666 667 674 TO 682 750 TO 758 765 766 773 774 781 TO 789 - 505. 857 TO 865 872 873 880 881 888 TO 896 964 TO 972 979 980 987 988 995 TO 1003 - 506. 1071 TO 1079 1086 1087 1094 1095 1102 TO 1110 1178 TO 1186 1193 1194 1201 - 507. 1202 1209 TO 1217 1285 TO 1293 1300 1301 1308 1309 1316 TO 1324 1392 TO 1400 - 508. 1407 1408 1415 1416 1423 TO 1431 1591 TO 1598 1614 TO 1621 1637 TO 1644 1660 - 509. 1661 TO 1667 1683 TO 1690 1706 TO 1713 1729 TO 1736 1752 TO 1759 1775 TO 1782 - 510. 1798 TO 1805 PRIS YD 0.75 ZD 0.3 511. MEMBER PROPERTY 512. 1 TO 40 108 TO 147 215 TO 254 322 TO 361 1499 TO 1506 1522 TO 1529 - 513. 1545 TO 1552 1568 TO 1575 PRIS YD 0.9 ZD 0.3 514. CONSTANTS 515. MATERIAL CONCRETE ALL 516. SUPPORTS 517. 1 7 28 TO 65 626 628 630 632 634 636 638 640 FIXED 518. *66 TO 625 627 629 631 633 635 637 639 641 TO 745 PINNED 519. ******* DL+0.5LL********* 520. DEFINE 1893 LOAD 521. ZONE 0.24 RF 5 I 1.5 SS 1 ST 1 DM 0.05 522. SELFWEIGHT 1 523. MEMBER WEIGHT 524. 148 TO 154 255 TO 261 362 TO 368 469 TO 475 576 TO 582 683 TO 689 790 TO 796 - 525. 897 TO 903 1004 TO 1010 1111 TO 1117 1218 TO 1224 1325 TO 1331 1530 TO 1536 - 526. 1553 TO 1559 1576 TO 1582 1599 TO 1605 1622 TO 1628 1645 TO 1651 - 527. 1668 TO 1674 1691 TO 1697 1714 TO 1720 1737 TO 1743 1760 TO 1766 - 528. 1783 TO 1789 UNI 12 529. 183 TO 186 211 TO 214 290 TO 293 318 TO 321 397 TO 400 425 TO 428 504 TO 507 - 530. 532 TO 535 611 TO 614 639 TO 642 718 TO 721 746 TO 749 825 TO 828 - 531. 853 TO 856 932 TO 935 960 TO 963 1039 TO 1042 1067 TO 1070 1146 TO 1149 1174 - 532. 1175 TO 1177 1253 TO 1256 1281 TO 1284 1360 TO 1363 1388 TO 1391 1537 1544 - 533. 1560 1567 1583 1590 1606 1613 1629 1636 1652 1659 1675 1682 1698 1705 1721 - 534. 1728 1744 1751 1767 1774 1790 1797 UNI 12.7 535. 1432 TO 1438 1467 TO 1470 1495 TO 1498 1806 TO 1813 1820 UNI 5 536. ONEWAY LOAD 537. YRANGE 3 42 ONE 5.1 538. YRANGE 42 42.7 ONE 4.35 539. LOAD 1 LOADTYPE SEISMIC TITLE EQX 540. 1893 LOAD X 1 541. LOAD 2 LOADTYPE SEISMIC TITLE EQZ 542. 1893 LOAD Z 1 543. LOAD 4 LOADTYPE DEAD TITLE DL 544. SELFWEIGHT Y -1 545. MEMBER LOAD 546. 148 TO 154 255 TO 261 362 TO 368 469 TO 475 576 TO 582 683 TO 689 790 TO 796 - 547. 897 TO 903 1004 TO 1010 1111 TO 1117 1218 TO 1224 1325 TO 1331 1530 TO 1536 - 548. 1553 TO 1559 1576 TO 1582 1599 TO 1605 1622 TO 1628 1645 TO 1651 - 549. 1668 TO 1674 1691 TO 1697 1714 TO 1720 1737 TO 1743 1760 TO 1766 - 550. 1783 TO 1789 UNI GY -12 551. 183 TO 186 211 TO 214 290 TO 293 318 TO 321 397 TO 400 425 TO 428 504 TO 507 - 552. 532 TO 535 611 TO 614 639 TO 642 718 TO 721 746 TO 749 825 TO 828 - 553. 853 TO 856 932 TO 935 960 TO 963 1039 TO 1042 1067 TO 1070 1146 TO 1149 1174 - 554. 1175 TO 1177 1253 TO 1256 1281 TO 1284 1360 TO 1363 1388 TO 1391 1537 1544 - 555. 1560 1567 1583 1590 1606 1613 1629 1636 1652 1659 1675 1682 1698 1705 1721 - 556. 1728 1744 1751 1767 1774 1790 1797 UNI GY -12.7 557. 1432 TO 1438 1467 TO 1470 1495 TO 1498 1806 TO 1813 1820 UNI GY -5 558. ONEWAY LOAD

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559. YRANGE 3 42.7 ONE -3.6 GY 560. LOAD 5 LOADTYPE LIVE TITLE LL 561. ONEWAY LOAD 562. YRANGE 3 42 ONE -3 GY 563. YRANGE 42 42.7 ONE -1.5 GY 564. ************ FOR LUMP MASS CALCULATION 565. LOAD COMBINATION 100 566. 4 1.0 5 0.5 567. ***********FOR MEMBER DESIGN 568. LOAD COMB 101 1.5DL+1.5LL 569. 4 1.5 5 1.5 570. LOAD COMB 102 1.2DL+1.2LL+1.2EQX 571. 4 1.2 5 1.2 1 1.2 572. LOAD COMB 103 1.2DL+1.2LL-1.2EQX 573. 4 1.2 5 1.2 1 -1.2 574. LOAD COMB 104 1.2DL+1.2LL+1.2EQZ 575. 4 1.2 5 1.2 2 1.2 576. LOAD COMB 105 1.2DL+1.2LL-1.2EQZ 577. 4 1.2 5 1.2 2 -1.2 583. ************* CONCRETE DESIGN 584. PERFORM ANALYSIS

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

NUMBER OF JOINTS 720 NUMBER OF MEMBERS 1820 NUMBER OF PLATES 0 NUMBER OF SOLIDS 0 NUMBER OF SURFACES 0 NUMBER OF SUPPORTS 48

SOLVER USED IS THE IN-CORE ADVANCED SOLVER TOTAL PRIMARY LOAD CASES = 4, TOTAL DEGREES OF FREEDOM = 4032 TOTAL LOAD COMBINATION CASES = 8 SO FAR.

**WARNING: IF THIS UBC/IBC ANALYSIS HAS TENSION/COMPRESSION OR REPEAT LOAD OR RE-ANALYSIS OR SELECT OPTIMIZE, THEN EACH UBC/IBC CASE SHOULD BE FOLLOWED BY PERFORM ANALYSIS & CHANGE.

********************************************************* * * * TIME PERIOD FOR X 1893 LOADING = 1.25280 SEC * * SA/G PER 1893= 0.798, LOAD FACTOR= 1.000 * * VB PER 1893= 0.0287 X 85806.23= 2465.69 KN * * * *********************************************************

********************************************************* * * * TIME PERIOD FOR Z 1893 LOADING = 1.25280 SEC * * SA/G PER 1893= 0.798, LOAD FACTOR= 1.000 * * VB PER 1893= 0.0287 X 85806.23= 2465.69 KN * * * *********************************************************

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585. *LOAD LIST 100 586. *PRINT SUPORT REACTION 587. ******************** 588. LOAD LIST 101 TO 105MEMBER END FORCES STRUCTURE TYPE = SPACE ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

105 81 -1.42 47.38 0.02 0.00 -0.03 66.49 89 1.42 -38.44 -0.02 0.00 -0.03 62.23

106 101 89 -1.79 5.59 0.00 0.00 0.00 2.80 97 1.79 5.59 0.00 0.00 0.00 -2.80 102 89 -1.43 4.47 0.00 0.00 0.00 2.24 97 1.43 4.47 0.00 0.00 0.00 -2.24 103 89 -1.44 4.47 0.00 0.00 0.00 2.24 97 1.44 4.47 0.00 0.00 0.00 -2.24 104 89 -1.44 -38.64 -0.02 0.00 0.03 -62.43 97 1.44 47.59 0.02 0.00 0.03 -66.91 105 89 -1.44 47.59 0.02 0.00 -0.03 66.91 97 1.44 -38.64 -0.02 0.00 -0.03 62.43

107 101 97 -1.87 5.53 0.00 0.00 0.00 2.67 105 1.87 5.64 0.00 0.00 0.00 -2.83 102 97 -1.49 4.43 0.00 0.01 0.00 2.14 105 1.49 4.51 0.00 -0.01 0.01 -2.26 103 97 -1.50 4.43 0.00 0.00 0.00 2.13 105 1.50 4.52 0.00 0.00 0.00 -2.27 104 97 -1.42 -38.44 -0.02 0.00 0.03 -62.23 105 1.42 47.38 0.02 0.00 0.03 -66.49 105 97 -1.57 47.29 0.02 0.00 -0.02 66.50 105 1.57 -38.35 -0.02 0.00 -0.02 61.96

108 101 66 2359.12 -24.04 3.49 -0.01 -3.21 -12.34 106 -2331.91 24.04 -3.49 0.01 -6.57 -54.99 102 66 1566.50 28.56 2.79 0.02 -2.57 124.90 106 -1544.73 -28.56 -2.79 -0.02 -5.26 -44.92 103 66 2208.10 -67.04 2.79 -0.05 -2.56 -144.65 106 -2186.32 67.04 -2.79 0.05 -5.25 -43.06 104 66 1215.90 -19.17 -40.42 0.15 70.71 -9.77 106 -1194.13 19.17 40.42 -0.15 42.46 -43.90 105 66 2558.70 -19.30 46.00 -0.18 -75.84 -9.97 106 -2536.92 19.30 -46.00 0.18 -52.97 -44.08

109 101 67 3173.42 -2.50 0.67 -0.01 -0.95 -1.00 107 -3146.21 2.50 -0.67 0.01 -0.94 -5.99 102 67 2515.51 64.24 0.54 0.01 -0.76 148.71 107 -2493.74 -64.24 -0.54 -0.01 -0.75 31.18 103 67 2561.97 -68.24 0.54 -0.03 -0.76 -150.31 107 -2540.19 68.24 -0.54 0.03 -0.75 -40.76 104 67 1851.00 -1.90 -43.40 0.22 73.77 -0.69 107 -1829.22 1.90 43.40 -0.22 47.76 -4.64 105 67 3226.48 -2.09 44.48 -0.23 -75.28 -0.92 107 -3204.71 2.09 -44.48 0.23 -49.26 -4.95

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MEMBER END FORCES STRUCTURE TYPE = SPACE ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

110 101 68 3253.52 -1.20 0.58 -0.01 -0.87 -0.70 108 -3226.31 1.20 -0.58 0.01 -0.76 -2.67 102 68 2600.53 65.54 0.47 0.02 -0.69 148.79 108 -2578.76 -65.54 -0.47 -0.02 -0.61 34.71 103 68 2605.11 -67.46 0.47 -0.03 -0.69 -149.92 108 -2583.34 67.46 -0.47 0.03 -0.61 -38.98 104 68 1902.62 -0.90 -44.11 0.15 74.91 -0.49 108 -1880.85 0.90 44.11 -0.15 48.60 -2.03 105 68 3303.02 -1.03 45.04 -0.16 -76.30 -0.64 108 -3281.24 1.03 -45.04 0.16 -49.82 -2.23

111 101 69 3261.10 -0.38 0.58 0.00 -0.86 -0.27 109 -3233.88 0.38 -0.58 0.00 -0.76 -0.80 102 69 2608.72 66.37 0.46 0.02 -0.69 149.18 109 -2586.95 -66.37 -0.46 -0.02 -0.60 36.65 103 69 2609.03 -66.98 0.46 -0.02 -0.69 -149.61 109 -2587.26 66.98 -0.46 0.02 -0.60 -37.94 104 69 1902.89 -0.29 -44.45 0.05 75.48 -0.19 109 -1881.12 0.29 44.45 -0.05 48.97 -0.61 105 69 3314.87 -0.33 45.37 -0.05 -76.86 -0.24 109 -3293.09 0.33 -45.37 0.05 -50.18 -0.68

112 101 70 3261.10 0.38 0.58 0.00 -0.86 0.27 110 -3233.88 -0.38 -0.58 0.00 -0.76 0.80 102 70 2609.03 66.98 0.46 0.02 -0.69 149.61 110 -2587.26 -66.98 -0.46 -0.02 -0.60 37.94 103 70 2608.72 -66.37 0.46 -0.02 -0.69 -149.18 110 -2586.95 66.37 -0.46 0.02 -0.60 -36.65 104 70 1902.89 0.29 -44.45 -0.05 75.48 0.19 110 -1881.12 -0.29 44.45 0.05 48.97 0.61 105 70 3314.87 0.33 45.37 0.05 -76.86 0.24 110 -3293.09 -0.33 -45.37 -0.05 -50.18 0.68

113 101 71 3253.52 1.20 0.58 0.01 -0.87 0.70 111 -3226.31 -1.20 -0.58 -0.01 -0.76 2.67 102 71 2605.11 67.46 0.47 0.03 -0.69 149.92 111 -2583.34 -67.46 -0.47 -0.03 -0.61 38.98 103 71 2600.53 -65.54 0.47 -0.02 -0.69 -148.79 111 -2578.76 65.54 -0.47 0.02 -0.61 -34.71 104 71 1902.62 0.90 -44.11 -0.15 74.91 0.49 111 -1880.85 -0.90 44.11 0.15 48.60 2.03 105 71 3303.02 1.03 45.04 0.16 -76.30 0.64 111 -3281.24 -1.03 -45.04 -0.16 -49.82 2.23

114 101 72 3173.42 2.50 0.67 0.01 -0.95 1.00 112 -3146.21 -2.50 -0.67 -0.01 -0.94 5.99

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MEMBER END FORCES STRUCTURE TYPE = SPACE ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

102 72 2561.97 68.24 0.54 0.03 -0.76 150.31 112 -2540.19 -68.24 -0.54 -0.03 -0.75 40.76 103 72 2515.51 -64.24 0.54 -0.01 -0.76 -148.71 112 -2493.74 64.24 -0.54 0.01 -0.75 -31.18 104 72 1851.00 1.90 -43.40 -0.22 73.77 0.69 112 -1829.22 -1.90 43.40 0.22 47.76 4.64 105 72 3226.48 2.09 44.48 0.23 -75.28 0.92 112 -3204.71 -2.09 -44.48 -0.23 -49.26 4.95

115 101 73 2359.12 24.04 3.49 0.01 -3.21 12.34 113 -2331.91 -24.04 -3.49 -0.01 -6.57 54.99 102 73 2208.10 67.04 2.79 0.05 -2.56 144.65 113 -2186.32 -67.04 -2.79 -0.05 -5.25 43.06 103 73 1566.50 -28.56 2.79 -0.02 -2.57 -124.90 113 -1544.73 28.56 -2.79 0.02 -5.26 44.92 104 73 1215.90 19.17 -40.42 -0.15 70.71 9.77 113 -1194.13 -19.17 40.42 0.15 42.46 43.90 105 73 2558.70 19.30 46.00 0.18 -75.84 9.97 113 -2536.92 -19.30 -46.00 -0.18 -52.97 44.08

116 101 74 2558.53 -21.78 0.27 -0.01 -0.35 -11.39 114 -2531.32 21.78 -0.27 0.01 -0.39 -49.58 102 74 1726.40 30.24 0.21 0.03 -0.28 125.25 114 -1704.63 -30.24 -0.21 -0.03 -0.32 -40.59 103 74 2367.25 -65.08 0.21 -0.05 -0.28 -143.47 114 -2345.48 65.08 -0.21 0.05 -0.31 -38.75 104 74 1987.95 -17.42 -68.89 0.07 104.50 -9.12 114 -1966.18 17.42 68.89 -0.07 88.41 -39.66 105 74 2105.70 -17.42 69.32 -0.09 -105.06 -9.10 114 -2083.92 17.42 -69.32 0.09 -89.04 -39.67

117 101 75 3113.80 -1.84 -0.23 -0.01 0.26 -0.58 115 -3086.59 1.84 0.23 0.01 0.38 -4.57 102 75 2467.80 64.58 -0.18 0.02 0.20 148.59 115 -2446.03 -64.58 0.18 -0.02 0.30 32.22 103 75 2514.28 -67.51 -0.18 -0.04 0.20 -149.51 115 -2492.51 67.51 0.18 0.04 0.30 -39.53 104 75 2430.61 -1.47 -70.45 0.13 106.75 -0.47 115 -2408.84 1.47 70.45 -0.13 90.50 -3.65 105 75 2551.48 -1.47 70.09 -0.14 -106.34 -0.45 115 -2529.70 1.47 -70.09 0.14 -89.90 -3.66

118 101 76 3174.65 -1.03 -0.29 -0.01 0.33 -0.58 116 -3147.44 1.03 0.29 0.01 0.49 -2.31 102 76 2537.43 65.48 -0.23 0.03 0.26 148.43 116 -2515.66 -65.48 0.23 -0.03 0.39 34.90

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MEMBER END FORCES STRUCTURE TYPE = SPACE ----------------- ALL UNITS ARE -- KN METE (LOCAL )

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

103 76 2542.01 -67.13 -0.23 -0.04 0.26 -149.36 116 -2520.24 67.13 0.23 0.04 0.39 -38.59 104 76 2478.01 -0.82 -71.52 0.09 108.36 -0.47 116 -2456.24 0.82 71.52 -0.09 91.89 -1.84 105 76 2601.43 -0.82 71.05 -0.10 -107.83 -0.46 116 -2579.66 0.82 -71.05 0.10 -91.11 -1.85

119 101 77 3181.13 -0.33 -0.30 0.00 0.34 -0.23 117 -3153.92 0.33 0.30 0.00 0.50 -0.70 102 77 2544.75 66.21 -0.24 0.03 0.27 148.75 117 -2522.98 -66.21 0.24 -0.03 0.40 36.64 103 77 2545.06 -66.74 -0.24 -0.03 0.27 -149.11 117 -2523.29 66.74 0.24 0.03 0.40 -37.76 104 77 2482.60 -0.26 -72.05 0.03 109.17 -0.18 117 -2460.83 0.26 72.05 -0.03 92.58 -0.56 105 77 2607.21 -0.26 71.58 -0.03 -108.63 -0.18 117 -2585.43 0.26 -71.58 0.03 -91.79 -0.56

120 101 78 3181.13 0.33 -0.30 0.00 0.34 0.23 118 -3153.92 -0.33 0.30 0.00 0.50 0.70 102 78 2545.06 66.74 -0.24 0.03 0.27 149.11 118 -2523.29 -66.74 0.24 -0.03 0.40 37.76 103 78 2544.75 -66.21 -0.24 -0.03 0.27 -148.75 118 -2522.98 66.21 0.24 0.03 0.40 -36.64 104 78 2482.60 0.26 -72.05 -0.03 109.17 0.18 118 -2460.83 -0.26 72.05 0.03 92.58 0.56 105 78 2607.21 0.26 71.58 0.03 -108.63 0.18 118 -2585.43 -0.26 -71.58 -0.03 -91.79 0.56

121 101 79 3174.65 1.03 -0.29 0.01 0.33 0.58 119 -3147.44 -1.03 0.29 -0.01 0.49 2.31 102 79 2542.01 67.13 -0.23 0.04 0.26 149.36 119 -2520.24 -67.13 0.23 -0.04 0.39 38.59 103 79 2537.43 -65.48 -0.23 -0.03 0.26 -148.43 119 -2515.66 65.48 0.23 0.03 0.39 -34.90 104 79 2478.01 0.82 -71.52 -0.09 108.36 0.47 119 -2456.24 -0.82 71.52 0.09 91.89 1.84 105 79 2601.43 0.82 71.05 0.10 -107.83 0.46 119 -2579.66 -0.82 -71.05 -0.10 -91.11 1.85

122 101 80 3113.80 1.84 -0.23 0.01 0.26 0.58 120 -3086.59 -1.84 0.23 -0.01 0.38 4.57 102 80 2514.28 67.51 -0.18 0.04 0.20 149.51 120 -2492.51 -67.51 0.18 -0.04 0.30 39.53 103 80 2467.80 -64.58 -0.18 -0.02 0.20 -148.59 120 -2446.03 64.58 0.18 0.02 0.30 -32.22

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

103 624 0.47 5.42 -0.17 -0.07 0.23 3.28 744 -0.47 3.52 0.17 0.07 0.27 -0.44 104 624 -7.91 4.96 -2.84 -0.13 3.91 5.54 744 7.91 3.98 2.84 0.13 4.62 -4.06 105 624 8.83 5.87 2.67 -0.10 -3.66 1.02 744 -8.83 3.07 -2.67 0.10 -4.36 3.20

1820 101 625 7.87 12.43 -0.09 0.04 0.14 0.43 745 -7.87 21.25 0.09 -0.04 0.14 -13.68 102 625 6.36 9.92 -0.07 -0.03 0.11 0.32 745 -6.36 17.02 0.07 0.03 0.09 -10.97 103 625 6.24 9.96 -0.08 0.09 0.11 0.38 745 -6.24 16.98 0.08 -0.09 0.14 -10.91 104 625 -0.99 10.07 -2.13 0.02 2.81 3.31 745 0.99 16.87 2.13 -0.02 3.57 -13.52 105 625 13.59 9.81 1.98 0.04 -2.59 -2.61 745 -13.59 17.13 -1.98 -0.04 -3.34 -8.36

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

590. START CONCRETE DESIGNCONCRETE DESIGN 591. CODE INDIAN 592. UNIT MMS NEWTON 593. FC 25 ALL 594. FYMAIN 500 ALL 595. FYSEC 500 ALL 596. CLEAR 30 ALL 597. ELY 0.65 ALL 598. DESIGN COLUMN 1 TO 40 108 TO 147 215 TO 254 322 TO 361 429 TO 468 536 TO 575 - 599. 643 TO 682 750 TO 789 857 TO 896 964 TO 1003 1071 TO 1110 1178 TO 1217 1285 - 600. 1286 TO 1324 1392 TO 1431 1499 TO 1506 1522 TO 1529 1545 TO 1552 1568 TO 1575 - 601. 1591 TO 1598 1614 TO 1621 1637 TO 1644 1660 TO 1667 1683 TO 1690 - 602. 1706 TO 1713 1729 TO 1736 1752 TO 1759 1775 TO 1782 1798 TO 1805

============================================================================

C O L U M N N O. 1 D E S I G N R E S U L T S

M25 Fe500 (Main) Fe500 (Sec.)

LENGTH: 1500.0 mm CROSS SECTION: 300.0 mm X 900.0 mm COVER: 40.0 mm

** GUIDING LOAD CASE: 105 END JOINT: 1 SHORT COLUMN

REQD. STEEL AREA : 1887.75 Sq.mm. REQD. CONCRETE AREA: 268112.25 Sq.mm. MAIN REINFORCEMENT : Provide 20 - 12 dia. (0.84%, 2261.95 Sq.mm.) (Equally distributed) TIE REINFORCEMENT : Provide 8 mm dia. rectangular ties @ 190 mm c/c

SECTION CAPACITY BASED ON REINFORCEMENT REQUIRED (KNS-MET) ---------------------------------------------------------- Puz : 3724.17 Muz1 : 357.65 Muy1 : 108.29

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INTERACTION RATIO: 0.48 (as per Cl. 39.6, IS456:2000)

SECTION CAPACITY BASED ON REINFORCEMENT PROVIDED (KNS-MET) ---------------------------------------------------------- WORST LOAD CASE: 105 END JOINT: 1 Puz : 3860.28 Muz : 400.19 Muy : 119.23 IR: 0.41 ============================================================================

============================================================================

C O L U M N N O. 2 D E S I G N R E S U L T S

M25 Fe500 (Main) Fe500 (Sec.)

LENGTH: 1500.0 mm CROSS SECTION: 300.0 mm X 900.0 mm COVER: 40.0 mm

** GUIDING LOAD CASE: 105 END JOINT: 7 SHORT COLUMN

REQD. STEEL AREA : 2808.00 Sq.mm. REQD. CONCRETE AREA: 267192.00 Sq.mm. MAIN REINFORCEMENT : Provide 16 - 16 dia. (1.19%, 3216.99 Sq.mm.) (Equally distributed) TIE REINFORCEMENT : Provide 8 mm dia. rectangular ties @ 255 mm c/c

SECTION CAPACITY BASED ON REINFORCEMENT REQUIRED (KNS-MET) ---------------------------------------------------------- Puz : 4058.91 Muz1 : 274.34 Muy1 : 79.53

INTERACTION RATIO: 0.88 (as per Cl. 39.6, IS456:2000)

SECTION CAPACITY BASED ON REINFORCEMENT PROVIDED (KNS-MET) ---------------------------------------------------------- WORST LOAD CASE: 105 END JOINT: 7 Puz : 4207.68 Muz : 330.95 Muy : 96.29 IR: 0.61 ============================================================================

============================================================================

C O L U M N N O. 3 D E S I G N R E S U L T S

M25 Fe500 (Main) Fe500 (Sec.)

LENGTH: 1500.0 mm CROSS SECTION: 300.0 mm X 900.0 mm COVER: 40.0 mm

** GUIDING LOAD CASE: 105 END JOINT: 28 SHORT COLUMN

REQD. STEEL AREA : 3024.00 Sq.mm. REQD. CONCRETE AREA: 266976.00 Sq.mm. MAIN REINFORCEMENT : Provide 16 - 16 dia. (1.19%, 3216.99 Sq.mm.) (Equally distributed) TIE REINFORCEMENT : Provide 8 mm dia. rectangular ties @ 255 mm c/c

SECTION CAPACITY BASED ON REINFORCEMENT REQUIRED (KNS-MET) ---------------------------------------------------------- Puz : 4137.48 Muz1 : 277.36 Muy1 : 79.71

INTERACTION RATIO: 0.90 (as per Cl. 39.6, IS456:2000)

SECTION CAPACITY BASED ON REINFORCEMENT PROVIDED (KNS-MET) ----------------------------------------------------------

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WORST LOAD CASE: 105 END JOINT: 28 Puz : 4207.68 Muz : 303.92 Muy : 87.57 IR: 0.75 ============================================================================

C O L U M N N O. 4 D E S I G N R E S U L T S

M25 Fe500 (Main) Fe500 (Sec.)

LENGTH: 1500.0 mm CROSS SECTION: 300.0 mm X 900.0 mm COVER: 40.0 mm

** GUIDING LOAD CASE: 105 END JOINT: 29 SHORT COLUMN

REQD. STEEL AREA : 3024.00 Sq.mm. REQD. CONCRETE AREA: 266976.00 Sq.mm. MAIN REINFORCEMENT : Provide 16 - 16 dia. (1.19%, 3216.99 Sq.mm.) (Equally distributed) TIE REINFORCEMENT : Provide 8 mm dia. rectangular ties @ 255 mm c/c

SECTION CAPACITY BASED ON REINFORCEMENT REQUIRED (KNS-MET) ---------------------------------------------------------- Puz : 4137.48 Muz1 : 273.92 Muy1 : 78.39

INTERACTION RATIO: 0.94 (as per Cl. 39.6, IS456:2000)

SECTION CAPACITY BASED ON REINFORCEMENT PROVIDED (KNS-MET) ---------------------------------------------------------- WORST LOAD CASE: 105 END JOINT: 29 Puz : 4207.68 Muz : 299.77 Muy : 86.17 IR: 0.78 ============================================================================

============================================================================

C O L U M N N O. 5 D E S I G N R E S U L T S

M25 Fe500 (Main) Fe500 (Sec.)

LENGTH: 1500.0 mm CROSS SECTION: 300.0 mm X 900.0 mm COVER: 40.0 mm

** GUIDING LOAD CASE: 105 END JOINT: 30 SHORT COLUMN

REQD. STEEL AREA : 3024.00 Sq.mm. REQD. CONCRETE AREA: 266976.00 Sq.mm. MAIN REINFORCEMENT : Provide 16 - 16 dia. (1.19%, 3216.99 Sq.mm.) (Equally distributed) TIE REINFORCEMENT : Provide 8 mm dia. rectangular ties @ 255 mm c/c

SECTION CAPACITY BASED ON REINFORCEMENT REQUIRED (KNS-MET) ---------------------------------------------------------- Puz : 4137.48 Muz1 : 273.92 Muy1 : 78.39

INTERACTION RATIO: 0.94 (as per Cl. 39.6, IS456:2000)

SECTION CAPACITY BASED ON REINFORCEMENT PROVIDED (KNS-MET) ---------------------------------------------------------- WORST LOAD CASE: 105 END JOINT: 30 Puz : 4207.68 Muz : 299.77 Muy : 86.17 IR: 0.78 ============================================================================

============================================================================

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C O L U M N N O. 6 D E S I G N R E S U L T S

M25 Fe500 (Main) Fe500 (Sec.)

LENGTH: 1500.0 mm CROSS SECTION: 300.0 mm X 900.0 mm COVER: 40.0 mm

** GUIDING LOAD CASE: 105 END JOINT: 31 SHORT COLUMN

REQD. STEEL AREA : 3024.00 Sq.mm. REQD. CONCRETE AREA: 266976.00 Sq.mm. MAIN REINFORCEMENT : Provide 16 - 16 dia. (1.19%, 3216.99 Sq.mm.) (Equally distributed) TIE REINFORCEMENT : Provide 8 mm dia. rectangular ties @ 255 mm c/c

SECTION CAPACITY BASED ON REINFORCEMENT REQUIRED (KNS-MET) ---------------------------------------------------------- Puz : 4137.48 Muz1 : 277.36 Muy1 : 79.71

INTERACTION RATIO: 0.90 (as per Cl. 39.6, IS456:2000)

SECTION CAPACITY BASED ON REINFORCEMENT PROVIDED (KNS-MET) ---------------------------------------------------------- WORST LOAD CASE: 105 END JOINT: 31 Puz : 4207.68 Muz : 303.92 Muy : 87.57 IR: 0.75 ============================================================================

C O L U M N N O. 7 D E S I G N R E S U L T S

M25 Fe500 (Main) Fe500 (Sec.)

LENGTH: 1500.0 mm CROSS SECTION: 300.0 mm X 900.0 mm COVER: 40.0 mm

** GUIDING LOAD CASE: 105 END JOINT: 32 SHORT COLUMN

REQD. STEEL AREA : 2808.00 Sq.mm. REQD. CONCRETE AREA: 267192.00 Sq.mm. MAIN REINFORCEMENT : Provide 16 - 16 dia. (1.19%, 3216.99 Sq.mm.) (Equally distributed) TIE REINFORCEMENT : Provide 8 mm dia. rectangular ties @ 255 mm c/c

SECTION CAPACITY BASED ON REINFORCEMENT REQUIRED (KNS-MET) ---------------------------------------------------------- Puz : 4058.91 Muz1 : 274.34 Muy1 : 79.53

INTERACTION RATIO: 0.88 (as per Cl. 39.6, IS456:2000)

SECTION CAPACITY BASED ON REINFORCEMENT PROVIDED (KNS-MET) ---------------------------------------------------------- WORST LOAD CASE: 105 END JOINT: 32 Puz : 4207.68 Muz : 330.95 Muy : 96.29 IR: 0.61 ============================================================================

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Beam Design ============================================================================ B E A M N O. 1816 D E S I G N R E S U L T S

M25 Fe500 (Main) Fe500 (Sec.)

LENGTH: 3000.0 mm SIZE: 230.0 mm X 450.0 mm COVER: 25.0 mm

SUMMARY OF REINF. AREA (Sq.mm) ---------------------------------------------------------------------------- SECTION 0.0 mm 750.0 mm 1500.0 mm 2250.0 mm 3000.0 mm ---------------------------------------------------------------------------- TOP 163.83 163.83 163.83 163.83 163.83 REINF. (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm)

BOTTOM 0.00 163.83 163.83 163.83 163.83 REINF. (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) ----------------------------------------------------------------------------

SUMMARY OF PROVIDED REINF. AREA ---------------------------------------------------------------------------- SECTION 0.0 mm 750.0 mm 1500.0 mm 2250.0 mm 3000.0 mm ---------------------------------------------------------------------------- TOP 3-12í 3-12í 3-12í 3-12í 3-12í REINF. 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s)

BOTTOM 2-12í 3-12í 3-12í 3-12í 3-12í REINF. 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s)

SHEAR 2 legged 8í 2 legged 8í 2 legged 8í 2 legged 8í 2 legged 8í REINF. @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c ---------------------------------------------------------------------------- SHEAR DESIGN RESULTS AT DISTANCE d (EFFECTIVE DEPTH) FROM FACE OF THE SUPPORT -----------------------------------------------------------------------------

SHEAR DESIGN RESULTS AT 569.0 mm AWAY FROM START SUPPORT VY = 5.24 MX = 0.00 LD= 101 Provide 2 Legged 8í @ 145 mm c/c

SHEAR DESIGN RESULTS AT 569.0 mm AWAY FROM END SUPPORT VY = -1.96 MX = 0.01 LD= 104 Provide 2 Legged 8í @ 145 mm c/c

============================================================================ B E A M N O. 1817 D E S I G N R E S U L T S

M25 Fe500 (Main) Fe500 (Sec.)

LENGTH: 3000.0 mm SIZE: 230.0 mm X 450.0 mm COVER: 25.0 mm

SUMMARY OF REINF. AREA (Sq.mm) ---------------------------------------------------------------------------- SECTION 0.0 mm 750.0 mm 1500.0 mm 2250.0 mm 3000.0 mm ---------------------------------------------------------------------------- TOP 163.83 163.83 163.83 163.83 163.83 REINF. (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm)

BOTTOM 0.00 163.83 163.83 163.83 163.83 REINF. (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) ----------------------------------------------------------------------------

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SUMMARY OF PROVIDED REINF. AREA ---------------------------------------------------------------------------- SECTION 0.0 mm 750.0 mm 1500.0 mm 2250.0 mm 3000.0 mm ---------------------------------------------------------------------------- TOP 3-12í 3-12í 3-12í 3-12í 3-12í REINF. 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s)

BOTTOM 2-12í 3-12í 3-12í 3-12í 3-12í REINF. 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s)

SHEAR 2 legged 8í 2 legged 8í 2 legged 8í 2 legged 8í 2 legged 8í REINF. @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c ----------------------------------------------------------------------------

SHEAR DESIGN RESULTS AT DISTANCE d (EFFECTIVE DEPTH) FROM FACE OF THE SUPPORT -----------------------------------------------------------------------------

SHEAR DESIGN RESULTS AT 569.0 mm AWAY FROM START SUPPORT VY = 5.24 MX = 0.00 LD= 101 Provide 2 Legged 8í @ 145 mm c/c

SHEAR DESIGN RESULTS AT 569.0 mm AWAY FROM END SUPPORT VY = -1.96 MX = -0.01 LD= 104 Provide 2 Legged 8í @ 145 mm c/c

============================================================================ B E A M N O. 1818 D E S I G N R E S U L T S

M25 Fe500 (Main) Fe500 (Sec.)

LENGTH: 3000.0 mm SIZE: 230.0 mm X 450.0 mm COVER: 25.0 mm

SUMMARY OF REINF. AREA (Sq.mm) ---------------------------------------------------------------------------- SECTION 0.0 mm 750.0 mm 1500.0 mm 2250.0 mm 3000.0 mm ---------------------------------------------------------------------------- TOP 163.83 163.83 163.83 163.83 163.83 REINF. (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm)

BOTTOM 0.00 163.83 163.83 163.83 163.83 REINF. (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) ----------------------------------------------------------------------------

SUMMARY OF PROVIDED REINF. AREA ---------------------------------------------------------------------------- SECTION 0.0 mm 750.0 mm 1500.0 mm 2250.0 mm 3000.0 mm ---------------------------------------------------------------------------- TOP 3-12í 3-12í 3-12í 3-12í 3-12í REINF. 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s)

BOTTOM 2-12í 3-12í 3-12í 3-12í 3-12í REINF. 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s)

SHEAR 2 legged 8í 2 legged 8í 2 legged 8í 2 legged 8í 2 legged 8í REINF. @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c ----------------------------------------------------------------------------

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SHEAR DESIGN RESULTS AT DISTANCE d (EFFECTIVE DEPTH) FROM FACE OF THE SUPPORT -----------------------------------------------------------------------------

SHEAR DESIGN RESULTS AT 569.0 mm AWAY FROM START SUPPORT VY = 5.22 MX = -0.01 LD= 101 Provide 2 Legged 8í @ 145 mm c/c

SHEAR DESIGN RESULTS AT 569.0 mm AWAY FROM END SUPPORT VY = -1.96 MX = -0.02 LD= 104 Provide 2 Legged 8í @ 145 mm c/c

============================================================================ B E A M N O. 1819 D E S I G N R E S U L T S

M25 Fe500 (Main) Fe500 (Sec.)

LENGTH: 3000.0 mm SIZE: 230.0 mm X 450.0 mm COVER: 25.0 mm

SUMMARY OF REINF. AREA (Sq.mm) ---------------------------------------------------------------------------- SECTION 0.0 mm 750.0 mm 1500.0 mm 2250.0 mm 3000.0 mm ---------------------------------------------------------------------------- TOP 163.83 163.83 163.83 163.83 163.83 REINF. (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm)

BOTTOM 0.00 163.83 163.83 163.83 163.83 REINF. (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) ----------------------------------------------------------------------------

SUMMARY OF PROVIDED REINF. AREA ---------------------------------------------------------------------------- SECTION 0.0 mm 750.0 mm 1500.0 mm 2250.0 mm 3000.0 mm ---------------------------------------------------------------------------- TOP 3-12í 3-12í 3-12í 3-12í 3-12í REINF. 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s)

BOTTOM 2-12í 3-12í 3-12í 3-12í 3-12í REINF. 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s)

SHEAR 2 legged 8í 2 legged 8í 2 legged 8í 2 legged 8í 2 legged 8í REINF. @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c ----------------------------------------------------------------------------

SHEAR DESIGN RESULTS AT DISTANCE d (EFFECTIVE DEPTH) FROM FACE OF THE SUPPORT -----------------------------------------------------------------------------

SHEAR DESIGN RESULTS AT 569.0 mm AWAY FROM START SUPPORT VY = 4.67 MX = -0.15 LD= 101 Provide 2 Legged 8í @ 145 mm c/c

SHEAR DESIGN RESULTS AT 569.0 mm AWAY FROM END SUPPORT VY = -2.30 MX = -0.15 LD= 101 Provide 2 Legged 8í @ 145 mm c/c

============================================================================

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B E A M N O. 1820 D E S I G N R E S U L T S

M25 Fe500 (Main) Fe500 (Sec.)

LENGTH: 3000.0 mm SIZE: 230.0 mm X 450.0 mm COVER: 25.0 mm

SUMMARY OF REINF. AREA (Sq.mm) ---------------------------------------------------------------------------- SECTION 0.0 mm 750.0 mm 1500.0 mm 2250.0 mm 3000.0 mm ---------------------------------------------------------------------------- TOP 163.83 0.00 0.00 163.83 163.83 REINF. (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm)

BOTTOM 163.83 163.83 163.83 163.83 0.00 REINF. (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) (Sq. mm) ----------------------------------------------------------------------------

SUMMARY OF PROVIDED REINF. AREA ---------------------------------------------------------------------------- SECTION 0.0 mm 750.0 mm 1500.0 mm 2250.0 mm 3000.0 mm ---------------------------------------------------------------------------- TOP 3-12í 2-12í 2-12í 3-12í 3-12í REINF. 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s)

BOTTOM 3-12í 3-12í 3-12í 3-12í 2-12í REINF. 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s) 1 layer(s)

SHEAR 2 legged 8í 2 legged 8í 2 legged 8í 2 legged 8í 2 legged 8í REINF. @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c @ 145 mm c/c ----------------------------------------------------------------------------

SHEAR DESIGN RESULTS AT DISTANCE d (EFFECTIVE DEPTH) FROM FACE OF THE SUPPORT -----------------------------------------------------------------------------

SHEAR DESIGN RESULTS AT 569.0 mm AWAY FROM START SUPPORT VY = 6.08 MX = 0.04 LD= 101 Provide 2 Legged 8í @ 145 mm c/c

SHEAR DESIGN RESULTS AT 569.0 mm AWAY FROM END SUPPORT VY = -14.91 MX = 0.04 LD= 101 Provide 2 Legged 8í @ 145 mm c/c

============================================================================

********************END OF BEAM DESIGN RESULTS********************

615. END CONCRETE DESIGN 616. FINISH

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