VANDANA S

ROLL NO:16

ANALYSIS AND DESIGN OF PORTAL FRAME

LOADING DIAGRAM

SHEAR FORCE DIAGRAM

BENDING MOMENT DIAGRAM

 DESIGN DETAILS
_

**********************************************
****** PROBLEM STATISTICS
* * -----------------------------------
* STAAD.Pro *
* Version 22.12.00.142 * NUMBER OF JOINTS 4 NUMBER OF
* Proprietary Program of * MEMBERS 3
* Bentley Systems, Inc. * NUMBER OF PLATES 0 NUMBER OF
* Date= JUL 5, 2024 * SOLIDS 0
* Time= 14:34:24 * NUMBER OF SURFACES 0 NUMBER OF
* * SUPPORTS 2
* Licensed to: *
Using 64-bit analysis engine.
**********************************************
****** SOLVER USED IS THE IN-CORE ADVANCED
_ MATH SOLVER

TOTAL PRIMARY LOAD CASES = 2, TOTAL

1. STAAD SPACE DEGREES OF FREEDOM = 12
INPUT FILE: C:\Users\Student\Desktop\vandana\ TOTAL LOAD COMBINATION CASES = 0 SO
Structure2.STD FAR.
2. START JOB INFORMATION _
3. ENGINEER NAME VANDANA S _ STAAD SPACE --
4. ENGINEER DATE 5/7/2024 PAGE NO. 3
5. END JOB INFORMATION
6. INPUT WIDTH 79
7. UNIT METER KN
8. JOINT COORDINATES LOADING 1 LOADTYPE DEAD TITLE DEAD
9. 1 0 0 0; 2 0 4.00001 0; 3 6.00001 4.00001 0; 4 LOAD
6.00001 0 0 -----------
10. MEMBER INCIDENCES
11. 1 1 2; 2 2 3; 3 3 4 SELFWEIGHT Y -1.000
12. DEFINE MATERIAL START
13. ISOTROPIC CONCRETE ACTUAL WEIGHT OF THE STRUCTURE
14. E 2.17184E+07 =59375100.000 KN
15. POISSON 0.17
16. DENSITY 23.5615
17. ALPHA 5.5E-06 LOADING 2 LOADTYPE LIVE TITLE LIVE
18. DAMP 0.05 LOAD
19. G 9.28137E+06 -----------
20. TYPE CONCRETE
21. STRENGTH FCU 27578.9
22. END DEFINE MATERIAL MEMBER LOAD - UNIT KN METE
23. MEMBER PROPERTY
24. 1 PRIS YD 600 ZD 300 MEMBER UDL L1 L2 CON L LIN1
25. 2 PRIS YD 600 ZD 300 LIN2
26. 3 PRIS YD 600 ZD 300
27. CONSTANTS 1 40.0000 GX 3.00
28. MATERIAL CONCRETE ALL 2 -80.0000 GY 3.00
29. SUPPORTS
30. 1 FIXED
31. 4 FIXED FOR LOADING - 1
32. LOAD 1 LOADTYPE DEAD TITLE DEAD APPLIED JOINT EQUIVALENT LOADS
LOAD JOINT FORCE-X FORCE-Y FORCE-Z
33. SELFWEIGHT Y -1 MOM-X MOM-Y MOM-Z
34. LOAD 2 LOADTYPE LIVE TITLE LIVE LOAD 1 0.00000E+00-8.48216E+06 0.00000E+00
35. MEMBER LOAD 0.00000E+00 0.00000E+00 0.00000E+00
36. 1 CON GX 40 3 1 2 0.00000E+00-2.12054E+07 0.00000E+00
37. 2 CON GY -80 3 3 0.00000E+00 0.00000E+00-1.27233E+07
38. PERFORM ANALYSIS PRINT ALL 3 0.00000E+00-2.12054E+07 0.00000E+00
_ STAAD SPACE -- 0.00000E+00 0.00000E+00 1.27233E+07
PAGE NO. 2 4 0.00000E+00-8.48216E+06 0.00000E+00
0.00000E+00 0.00000E+00 0.00000E+00
_
 STATIC LOAD/REACTION/EQUILIBRIUM -1.04E+02 -2.12E+07 0.00E+00 0.000E+00
SUMMARY FOR CASE NO. 1 0.000E+00 -5.453E+06 111111
LOADTYPE DEAD TITLE DEAD LOAD
4 0.00E+00 -8.48E+06 0.00E+00 0.000E+00
0.000E+00 0.000E+00
CENTER OF FORCE BASED ON Y FORCES 1.04E+02 -2.12E+07 0.00E+00 0.000E+00
ONLY (METE). 0.000E+00 5.453E+06 111111
(FORCES IN NON-GLOBAL DIRECTIONS
WILL INVALIDATE RESULTS) FOR LOADING - 2
APPLIED JOINT EQUIVALENT LOADS
X = 0.300000503E+01 JOINT FORCE-X FORCE-Y FORCE-Z
Y = 0.285714961E+01 MOM-X MOM-Y MOM-Z
Z = 0.000000000E+00 1 6.25009E+00 0.00000E+00 0.00000E+00
_TOTAL APPLIED LOAD 1_ 0.00000E+00 1.00001E+01-7.50011E+00
2 3.37499E+01-4.00001E+01 0.00000E+00
***TOTAL APPLIED LOAD ( KN METE ) 1.20000E+02 2.99999E+01-3.75001E+01
SUMMARY (LOADING 1 ) 3 0.00000E+00-3.99999E+01 0.00000E+00
SUMMATION FORCE-X = 0.00 1.20000E+02 0.00000E+00 6.00000E+01
SUMMATION FORCE-Y = -59375101.01
SUMMATION FORCE-Z = 0.00 STATIC LOAD/REACTION/EQUILIBRIUM
SUMMARY FOR CASE NO. 2
SUMMATION OF MOMENTS AROUND THE LOADTYPE LIVE TITLE LIVE LOAD
ORIGIN-
MX= 0.00 MY= 0.00 MZ= -
178125600.22 CENTER OF FORCE BASED ON X FORCES
ONLY (METE).
_TOTAL REACTION LOAD 1_ (FORCES IN NON-GLOBAL DIRECTIONS
WILL INVALIDATE RESULTS)
***TOTAL REACTION LOAD( KN METE )
SUMMARY (LOADING 1 ) X = 0.000000000E+00
SUMMATION FORCE-X = 0.00 Y = 0.300000537E+01
SUMMATION FORCE-Y = 59375101.01 Z = 0.100000002E+01
SUMMATION FORCE-Z = 0.00
_ STAAD SPACE -- CENTER OF FORCE BASED ON Y FORCES
PAGE NO. 4 ONLY (METE).
(FORCES IN NON-GLOBAL DIRECTIONS
WILL INVALIDATE RESULTS)
SUMMATION OF MOMENTS AROUND THE
ORIGIN- X = 0.281250025E+01
MX= 0.00 MY= 0.00 MZ= Y = 0.400001006E+01
178125600.22 Z = 0.300000011E+01
_TOTAL APPLIED LOAD 2_

MAXIMUM DISPLACEMENTS ( CM /RADIANS) ***TOTAL APPLIED LOAD ( KN METE )

(LOADING 1) SUMMARY (LOADING 2 )
MAXIMUMS AT NODE SUMMATION FORCE-X = 40.00
X = -7.96356E-09 3 SUMMATION FORCE-Y = -80.00
Y = -2.16974E-03 3 SUMMATION FORCE-Z = 0.00
Z = 0.00000E+00 0 _ STAAD SPACE --
RX= 0.00000E+00 0 PAGE NO. 5
RY= 0.00000E+00 0
RZ= 1.85975E-10 3
SUMMATION OF MOMENTS AROUND THE
ORIGIN-
MX= 240.00 MY= 40.00 MZ= -
EXTERNAL AND INTERNAL JOINT LOAD 360.00
SUMMARY ( KN METE )-
_TOTAL REACTION LOAD 2_
JT EXT FX/ EXT FY/ EXT FZ/ EXT MX/
EXT MY/ EXT MZ/ ***TOTAL REACTION LOAD( KN METE )
INT FX INT FY INT FZ INT MX INT SUMMARY (LOADING 2 )
MY INT MZ SUMMATION FORCE-X = -40.00
SUMMATION FORCE-Y = 80.00
SUPPORT=1 SUMMATION FORCE-Z = -0.00
1 0.00E+00 -8.48E+06 0.00E+00 0.000E+00
0.000E+00 0.000E+00 SUMMATION OF MOMENTS AROUND THE
ORIGIN-
 MX= -240.00 MY= -40.00 MZ= * http://www.bentley.com/en/support/
360.00 *
* *
* Details about additional assistance from
MAXIMUM DISPLACEMENTS ( CM /RADIANS) *
(LOADING 2) * Bentley and Partners can be found at program
MAXIMUMS AT NODE menu *
X = 5.77135E-09 2 * Help->Technical Support *
Y = -4.09287E-09 3 * *
Z = 3.57307E-12 2 * Copyright (c) Bentley Systems, Inc.
RX= 1.63713E-14 2 *
RY= 2.55935E-15 2 * http://www.bentley.com *
RZ= -1.58552E-15 2
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EXTERNAL AND INTERNAL JOINT LOAD

SUMMARY ( KN METE )-

JT EXT FX/ EXT FY/ EXT FZ/ EXT MX/

EXT MY/ EXT MZ/
INT FX INT FY INT FZ INT MX INT
MY INT MZ

SUPPORT=1
1 6.25 0.00 0.00 0.00 10.00 -7.50
20.49 -40.00 0.00 120.00 22.02 -
87.46 111111

4 0.00 0.00 0.00 0.00 0.00 0.00

13.26 -40.00 -0.00 120.00 7.97 -
25.03 111111

************ END OF DATA FROM INTERNAL

STORAGE ************

39. START CONCRETE DESIGN

_CONCRETE DESIGN_
40. CODE INDIAN
41. FC 20000 ALL
42. FYMAIN 415000 ALL
43. FYSEC 40000 ALL
44. MAXMAIN 60 ALL
45. MAXSEC 16 ALL
46. MINMAIN 25 ALL
47. MINSEC 12 ALL
48. END CONCRETE DESIGN
49. FINISH
_ STAAD SPACE --
PAGE NO. 6

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

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**** DATE= JUL 5,2024 TIME= 14:34:24

****

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