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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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
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
FIG -2. SHEAR FORCE DIAGRAM
FIG 3. BENDING MOMENT DIAGRAM
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
JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = PLANE ------------------
************** END OF LATEST ANALYSIS RESULT **************
29. FINISH
*********** END OF THE STAAD.Pro RUN ***********
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
Fig .8 Bending Moment Diagram
Fig .9 Shear Force Diagram
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
JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = PLANE ------------------
************** END OF LATEST ANALYSIS RESULT **************
29. FINISH
*********** END OF THE STAAD.Pro RUN ***********
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
Fig 11. Joint displacement of truss
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.
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 ------------------
************** END OF LATEST ANALYSIS RESULT **************
24. FINISH
*********** END OF THE STAAD.Pro RUN ***********
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
Fig .13 Joint Displacement
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
ANALYSIS RESULTS
JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = TRUSS ------------------
************** END OF LATEST ANALYSIS RESULT **************
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
Fig. 15
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: * ****************************************************
************** END OF LATEST ANALYSIS RESULT **************
30. FINISH
*********** END OF THE STAAD.Pro RUN ***********
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
Fig 20 Bending Moment Diagram
Fig 21 Shear Force Diagram
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.
29. PRINT ANALYSIS RESULTS ANALYSIS RESULTS
JOINT DISPLACEMENT (CM RADIANS) STRUCTURE TYPE = PLANE ------------------
************** END OF LATEST ANALYSIS RESULT **************
30. FINISH
*********** 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
Fig 23 Bending Moment Diagram
Fig 24 Shear Force Diagram
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.
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
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 * * * *********************************************************
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
************** 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
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
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 ============================================================================
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 ============================================================================
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) ----------------------------------------------------------
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 ============================================================================
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 ============================================================================
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 ============================================================================
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)
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)
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)
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)
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)
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)
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 = 5.22 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)
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)
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
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)
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)
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