w5 & w6 report

CONTENTS

Introduction

Material

Design data

Load

ANNNEXURES

Staad Output file for W6 (10.7 m) BeamB Staad Output file for W5 (6m) Beam

1.0

KSU Tower Project

2.0

A

3.0

4.0

Introduction

This calculation report pertains to the design of W5 & W6 beam. Staad. Pro has been used for Modelling,AnalysisandDesign.ReferAppendixAforStaadInputfile.

MaterialGrade of Concrete for foundation = CReinforcement = (Grade 60)Modulus of elasticity of steel = N/mm2

Design data

Beam Size = 400 (mm) x 700 (mm)Beam Length W6 = m

W5 = m

Loads: As per ACI / Saudi Building Code

1) Dead Load (DL) (self weight)

2) Wall Load (WL)Height of wall =Weight on Wall = =Lintel Additional weight = = kN/mTotal Weight = kN/m

3) Load Combination :a) 1.4 (DL + WL) Ultimate Case for strength (Design)b) (DL + WL) Service Case for Deflection (Serviceability)

2.030

kN/m

6

3.0

1.0

Fy 420

4.0

10.7

2.0E+05

616

0.6 x 0.4 x 25

3.9 m1.4 x 0.4 x 18 10

ANNEXURE-A STAAD OUTPUT FOR W6 (10.7m span)

Monday, March 02, 2015, 10:03 AM

PAGE NO. 1

**************************************************** * * * STAAD.Pro * * Version 2007 Build 04 * * Proprietary Program of * * Research Engineers, Intl. * * Date= MAR 2, 2015 * * Time= 9:59:22 * * * * USER ID: ABV Rock Group Ltd. * ****************************************************

1. STAAD PLANE INPUT FILE: W6-10.7m.STD 2. START JOB INFORMATION 3. ENGINEER DATE 02-MAR-15 4. END JOB INFORMATION 5. INPUT WIDTH 79 6. UNIT METER KN 7. JOINT COORDINATES 8. 1 0 0 0; 2 10.7 0 0 9. MEMBER INCIDENCES 10. 1 1 2 11. DEFINE MATERIAL START 12. ISOTROPIC CONCRETE 13. E 2.17185E+007 14. POISSON 0.17 15. DENSITY 23.5616 16. ALPHA 1E-005 17. DAMP 0.05 18. END DEFINE MATERIAL 19. MEMBER PROPERTY 20. 1 PRIS YD 0.7 ZD 0.4 21. CONSTANTS 22. MATERIAL CONCRETE ALL 23. SUPPORTS 24. 1 2 PINNED 25. LOAD 1 LOADTYPE NONE TITLE DEAD LOAD 26. SELFWEIGHT Y -1 LIST 1 27. LOAD 2 LOADTYPE NONE TITLE WALL LOAD 28. MEMBER LOAD 29. 1 UNI GY -16 30. LOAD COMB 3 DL+WL 31. 1 1.0 2 1.0 32. LOAD COMB 4 1.4(DL+WL) 33. 1 1.4 2 1.4 34. PERFORM ANALYSIS

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STAAD PLANE -- PAGE NO. 2

P R O B L E M S T A T I S T I C S ----------------------------------- NUMBER OF JOINTS/MEMBER+ELEMENTS/SUPPORTS = 2/ 1/ 2

SOLVER USED IS THE OUT-OF-CORE BASIC SOLVER

ORIGINAL/FINAL BAND-WIDTH= 1/ 1/ 2 DOF TOTAL PRIMARY LOAD CASES = 2, TOTAL DEGREES OF FREEDOM = 2 SIZE OF STIFFNESS MATRIX = 0 DOUBLE KILO-WORDS REQRD/AVAIL. DISK SPACE = 12.0/ 362996.0 MB

35. PRINT SUPPORT REACTION




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 35.30 0.00 0.00 0.00 0.00 2 0.00 85.60 0.00 0.00 0.00 0.00 3 0.00 120.90 0.00 0.00 0.00 0.00 4 0.00 169.25 0.00 0.00 0.00 0.00 2 1 0.00 35.30 0.00 0.00 0.00 0.00 2 0.00 85.60 0.00 0.00 0.00 0.00 3 0.00 120.90 0.00 0.00 0.00 0.00 4 0.00 169.25 0.00 0.00 0.00 0.00 ************** END OF LATEST ANALYSIS RESULT ************** 36. LOAD LIST 1 TO 3 37. PRINT SECTION DISPL




MEMBER SECTION DISPLACEMENTS ---------------------------- UNIT =INCHES FOR FPS AND CM FOR METRICS/SI SYSTEM MEMB LOAD GLOBAL X,Y,Z DISPL FROM START TO END JOINTS AT 1/12TH PTS 1 1 0.0000 0.0000 0.0000 0.0000 -0.1185 0.0000 0.0000 -0.2281 0.0000 0.0000 -0.3212 0.0000 0.0000 -0.3919 0.0000 0.0000 -0.4360 0.0000 0.0000 -0.4509 0.0000 0.0000 -0.4360 0.0000 0.0000 -0.3919 0.0000 0.0000 -0.3212 0.0000 0.0000 -0.2281 0.0000 0.0000 -0.1185 0.0000 0.0000 0.0000 0.0000 2 0.0000 0.0000 0.0000 0.0000 -0.2875 0.0000 0.0000 -0.5533 0.0000 0.0000 -0.7790 0.0000 0.0000 -0.9504 0.0000 0.0000 -1.0573 0.0000 0.0000 -1.0936 0.0000 0.0000 -1.0573 0.0000 0.0000 -0.9504 0.0000 0.0000 -0.7790 0.0000 0.0000 -0.5533 0.0000 0.0000 -0.2875 0.0000 0.0000 0.0000 0.0000 3 0.0000 0.0000 0.0000 0.0000 -0.4060 0.0000 0.0000 -0.7814 0.0000 0.0000 -1.1002 0.0000 0.0000 -1.3423 0.0000 0.0000 -1.4933 0.0000 0.0000 -1.5446 0.0000 0.0000 -1.4933 0.0000 0.0000 -1.3423 0.0000 0.0000 -1.1002 0.0000 0.0000 -0.7814 0.0000 0.0000 -0.4060 0.0000 0.0000 0.0000 0.0000 MAX LOCAL DISP = 1.54457 AT 535.00 LOAD 3 L/DISP= 692 ************ END OF SECT DISPL RESULTS *********** 38. LOAD LIST 1 TO 4 39. START CONCRETE DESIGN 40. CODE ACI 41. TRACK 0 ALL 42. FC 30000 ALL 43. FYMAIN 413688 ALL 44. FYSEC 413688 ALL 45. TRACK 0 ALL 46. DESIGN BEAM 1




===================================================================== BEAM NO. 1 DESIGN RESULTS - FLEXURE PER CODE ACI 318-05 LEN - 10700. MM FY - 414. FC - 30. MPA, SIZE - 400. X 700. MMS LEVEL HEIGHT BAR INFO FROM TO ANCHOR (MM) (MM) (MM) STA END _____________________________________________________________________

1 61. 7 - 20MM 0. 10641. YES NO

B E A M N O. 1 D E S I G N R E S U L T S - SHEAR

AT START SUPPORT - Vu= 106.51 KNS Vc= 255.05 KNS Vs= 0.00 KNS Tu= 0.00 KN-MET Tc= 12.2 KN-MET Ts= 0.0 KN-MET LOAD 3 NO STIRRUPS ARE REQUIRED FOR TORSION. REINFORCEMENT FOR SHEAR IS PER CL.11.5.5.1. PROVIDE 12 MM 2-LEGGED STIRRUPS AT 320. MM C/C FOR 4714. MM

AT END SUPPORT - Vu= 106.51 KNS Vc= 255.05 KNS Vs= 0.00 KNS Tu= 0.00 KN-MET Tc= 12.2 KN-MET Ts= 0.0 KN-MET LOAD 3 NO STIRRUPS ARE REQUIRED FOR TORSION. REINFORCEMENT FOR SHEAR IS PER CL.11.5.5.1. PROVIDE 12 MM 2-LEGGED STIRRUPS AT 320. MM C/C FOR 4714. MM

___ 1J____________________ 10700X 400X 700_____________________ 2J____ | | | | | | | 16*12c/c320 16*12c/c320 | | 7No20 H 61. 0.TO10641 | ||==========================================================================| | | |___________________________________________________________________________| _______ _______ _______ _______ _______ _______ _______ | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | 7#20 | | 7#20 | | 7#20 | | 7#20 | | 7#20 | | 7#20 | | | |ooooooo| |ooooooo| |ooooooo| |ooooooo| |ooooooo| |ooooooo| | | | | | | | | | | | | | | | | |_______| |_______| |_______| |_______| |_______| |_______| |_______| ********************END OF BEAM DESIGN************************** 47. END CONCRETE DESIGN




48. FINISH *********** END OF THE STAAD.Pro RUN *********** **** DATE= MAR 2,2015 TIME= 9:59:25 **** ************************************************************ * For questions on STAAD.Pro, please contact * * Research Engineers Offices at the following locations * * * * Telephone Email * * USA: +1 (714)974-2500 [email protected] * * CANADA +1 (905)632-4771 [email protected] * * UK +44(1454)207-000 [email protected] * * NORWAY +47 67 57 21 30 [email protected] * * SINGAPORE +65 6225-6158 [email protected] * * INDIA +91(033)4006-2021 [email protected] * * JAPAN +81(03)5952-6500 [email protected] * * CHINA +86(411)8479-1166 [email protected] * * THAILAND +66(0)2645-1018/19 [email protected] * * * * North America [email protected] * * Europe [email protected] * * Asia [email protected] * ************************************************************


ANNEXURE-B STAAD OUTPUT FOR W5 (6 m span)


PAGE NO. 1

**************************************************** * * * STAAD.Pro * * Version 2007 Build 04 * * Proprietary Program of * * Research Engineers, Intl. * * Date= MAR 2, 2015 * * Time= 10:12:36 * * * * USER ID: ABV Rock Group Ltd. * ****************************************************

1. STAAD PLANE INPUT FILE: W6-6m.STD 2. START JOB INFORMATION 3. ENGINEER DATE 02-MAR-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 9. MEMBER INCIDENCES 10. 1 1 2 11. DEFINE MATERIAL START 12. ISOTROPIC CONCRETE 13. E 2.17185E+007 14. POISSON 0.17 15. DENSITY 23.5616 16. ALPHA 1E-005 17. DAMP 0.05 18. END DEFINE MATERIAL 19. MEMBER PROPERTY AMERICAN 20. 1 PRIS YD 0.7 ZD 0.4 21. CONSTANTS 22. MATERIAL CONCRETE ALL 23. SUPPORTS 24. 1 2 PINNED 25. LOAD 1 LOADTYPE NONE TITLE DEAD LOAD 26. SELFWEIGHT Y -1 LIST 1 27. LOAD 2 LOADTYPE NONE TITLE WALL LOAD 28. MEMBER LOAD 29. 1 UNI GY -16 30. LOAD COMB 3 DL+WL 31. 1 1.0 2 1.0 32. LOAD COMB 4 1.4(DL+WL) 33. 1 1.4 2 1.4 34. PERFORM ANALYSIS

Page 1 of 7H:\ABV ROCK GROUP\KSU_University Endowment\Mr. Nader\Report\staad\W6-6m.ANL



P R O B L E M S T A T I S T I C S ----------------------------------- NUMBER OF JOINTS/MEMBER+ELEMENTS/SUPPORTS = 2/ 1/ 2

SOLVER USED IS THE OUT-OF-CORE BASIC SOLVER

ORIGINAL/FINAL BAND-WIDTH= 1/ 1/ 2 DOF TOTAL PRIMARY LOAD CASES = 2, TOTAL DEGREES OF FREEDOM = 2 SIZE OF STIFFNESS MATRIX = 0 DOUBLE KILO-WORDS REQRD/AVAIL. DISK SPACE = 12.0/ 362965.3 MB

35. PRINT SUPPORT REACTION




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 19.79 0.00 0.00 0.00 0.00 2 0.00 48.00 0.00 0.00 0.00 0.00 3 0.00 67.79 0.00 0.00 0.00 0.00 4 0.00 94.91 0.00 0.00 0.00 0.00 2 1 0.00 19.79 0.00 0.00 0.00 0.00 2 0.00 48.00 0.00 0.00 0.00 0.00 3 0.00 67.79 0.00 0.00 0.00 0.00 4 0.00 94.91 0.00 0.00 0.00 0.00 ************** END OF LATEST ANALYSIS RESULT ************** 36. LOAD LIST 1 TO 3 37. PRINT SECTION DISPL




MEMBER SECTION DISPLACEMENTS ---------------------------- UNIT =INCHES FOR FPS AND CM FOR METRICS/SI SYSTEM MEMB LOAD GLOBAL X,Y,Z DISPL FROM START TO END JOINTS AT 1/12TH PTS 1 1 0.0000 0.0000 0.0000 0.0000 -0.0117 0.0000 0.0000 -0.0226 0.0000 0.0000 -0.0318 0.0000 0.0000 -0.0387 0.0000 0.0000 -0.0431 0.0000 0.0000 -0.0446 0.0000 0.0000 -0.0431 0.0000 0.0000 -0.0387 0.0000 0.0000 -0.0318 0.0000 0.0000 -0.0226 0.0000 0.0000 -0.0117 0.0000 0.0000 0.0000 0.0000 2 0.0000 0.0000 0.0000 0.0000 -0.0284 0.0000 0.0000 -0.0547 0.0000 0.0000 -0.0770 0.0000 0.0000 -0.0940 0.0000 0.0000 -0.1045 0.0000 0.0000 -0.1081 0.0000 0.0000 -0.1045 0.0000 0.0000 -0.0940 0.0000 0.0000 -0.0770 0.0000 0.0000 -0.0547 0.0000 0.0000 -0.0284 0.0000 0.0000 0.0000 0.0000 3 0.0000 0.0000 0.0000 0.0000 -0.0401 0.0000 0.0000 -0.0773 0.0000 0.0000 -0.1088 0.0000 0.0000 -0.1327 0.0000 0.0000 -0.1476 0.0000 0.0000 -0.1527 0.0000 0.0000 -0.1476 0.0000 0.0000 -0.1327 0.0000 0.0000 -0.1088 0.0000 0.0000 -0.0773 0.0000 0.0000 -0.0401 0.0000 0.0000 0.0000 0.0000 MAX LOCAL DISP = 0.15271 AT 300.00 LOAD 3 L/DISP= 3928 ************ END OF SECT DISPL RESULTS *********** 38. LOAD LIST 1 TO 4 39. START CONCRETE DESIGN 40. CODE ACI 41. TRACK 0 ALL 42. FC 30000 ALL 43. FYMAIN 413688 ALL 44. FYSEC 413688 ALL 45. TRACK 0 ALL 46. DESIGN BEAM 1




===================================================================== BEAM NO. 1 DESIGN RESULTS - FLEXURE PER CODE ACI 318-05 LEN - 6000. MM FY - 414. FC - 30. MPA, SIZE - 400. X 700. MMS LEVEL HEIGHT BAR INFO FROM TO ANCHOR (MM) (MM) (MM) STA END _____________________________________________________________________

1 57. 8 - 12MM 0. 5810. YES NO

B E A M N O. 1 D E S I G N R E S U L T S - SHEAR

AT START SUPPORT - Vu= 15.59 KNS Vc= 235.94 KNS Vs= 0.00 KNS Tu= 0.00 KN-MET Tc= 12.2 KN-MET Ts= 0.0 KN-MET LOAD 1 STIRRUPS ARE NOT REQUIRED. AT END SUPPORT - Vu= 15.59 KNS Vc= 235.94 KNS Vs= 0.00 KNS Tu= 0.00 KN-MET Tc= 12.2 KN-MET Ts= 0.0 KN-MET LOAD 1 STIRRUPS ARE NOT REQUIRED.

___ 1J____________________ 6000X 400X 700_____________________ 2J____ | | | | | | | | | | | 8No12 H 57. 0.TO 5810 | ||======================================================================== | |___________________________________________________________________________| _______ _______ _______ _______ _______ _______ _______ | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | |ooooooo| |ooooooo| |ooooooo| |ooooooo| |ooooooo| |ooooooo| | | |_______| |_______| |_______| |_______| |_______| |_______| |_______| ********************END OF BEAM DESIGN************************** 47. END CONCRETE DESIGN 48. FINISH




*********** END OF THE STAAD.Pro RUN *********** **** DATE= MAR 2,2015 TIME= 10:12:40 **** ************************************************************ * For questions on STAAD.Pro, please contact * * Research Engineers Offices at the following locations * * * * Telephone Email * * USA: +1 (714)974-2500 [email protected] * * CANADA +1 (905)632-4771 [email protected] * * UK +44(1454)207-000 [email protected] * * NORWAY +47 67 57 21 30 [email protected] * * SINGAPORE +65 6225-6158 [email protected] * * INDIA +91(033)4006-2021 [email protected] * * JAPAN +81(03)5952-6500 [email protected] * * CHINA +86(411)8479-1166 [email protected] * * THAILAND +66(0)2645-1018/19 [email protected] * * * * North America [email protected] * * Europe [email protected] * * Asia [email protected] * ************************************************************


w5 & w6 report

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