w05-l07-l12 sty
TRANSCRIPT
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SheetJob Number
Job Title
Client
Calcs by Checked by Date
CONSULTANTS LLP
E-Mail : [email protected]
KTP/20/13
ECHELON
M/s KTP CONSULTANTS PTE LTD
HT T&T MAY 2014
C13W05-L07-L12 STY
General column design by PROKON. (GenCol Ver W2.4.01 - 01 Apr 2008)
Design code : CP65 - 1999
Input tables
General design parameters:
CodeX/Radius or
Bar dia. (mm)Y (mm)
Angle ()
+ 10.000
205.000
10.000 10.000
5980.000
-10.000 10.000
-205.000
-10.000 -10.000
-5980.000
+ 43.000 43.000
b 16
+ 182.000 43.000
b 16
+ 182.000 5957.000
b 16
+ 43.000 5957.000
b 16
+ 43.000 216.941b 16.000
+ 182.000 216.941
b 16.000
+ 43.000 390.882
b 16.000
+ 182.000 390.882
b 16.000
+ 43.000 564.824
b 16.000
+ 182.000 564.824
b 16.000
+ 43.000 738.765
b 16.000
+ 182.000 738.765
b 16.000
+ 43.000 912.706
b 16.000
+ 182.000 912.706
b 16.000
+ 43.000 1086.647
b 16.000
+ 182.000 1086.647
b 16.000
+ 43.000 1260.588
b 16.000
SheetJob Number
Job Title
Client
Calcs by Checked by Date
CONSULTANTS LLP
E-Mail : [email protected]
KTP/20/13
ECHELON
M/s KTP CONSULTANTS PTE LTD
HT T&T MAY 2014
+ 182.000 1260.588
b 16.000
+ 43.000 1434.529
b 16.000
+ 182.000 1434.529
b 16.000
+ 43.000 1608.471
b 16.000
+ 182.000 1608.471
b 16.000
+ 43.000 1782.412
b 16.000
+ 182.000 1782.412
b 16.000
+ 43.000 1956.353
b 16.000
+ 182.000 1956.353
b 16.000
+ 43.000 2130.294
b 16.000
+ 182.000 2130.294
b 16.000
+ 43.000 2304.235
b 16.000
+ 182.000 2304.235
b 16.000
+ 43.000 2478.176b 16.000
+ 182.000 2478.176
b 16.000
+ 43.000 2652.118
b 16.000
+ 182.000 2652.118
b 16.000
+ 43.000 2826.059
b 16.000
+ 182.000 2826.059
b 16.000
+ 43.000 3000.000
b 16.000
+ 182.000 3000.000
b 16.000
+ 43.000 3173.941
b 16.000
+ 182.000 3173.941
b 16.000
+ 43.000 3347.882
b 16.000
+ 182.000 3347.882
b 16.000
+ 43.000 3521.824
b 16.000
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8/10/2019 W05-L07-L12 STY
2/5
SheetJob Number
Job Title
Client
Calcs by Checked by Date
CONSULTANTS LLP
E-Mail : [email protected]
KTP/20/13
ECHELON
M/s KTP CONSULTANTS PTE LTD
HT T&T MAY 2014
+ 182.000 3521.824
b 16.000
+ 43.000 3695.765
b 16.000
+ 182.000 3695.765
b 16.000
+ 43.000 3869.706
b 16.000
+ 182.000 3869.706
b 16.000
+ 43.000 4043.647
b 16.000
+ 182.000 4043.647
b 16.000
+ 43.000 4217.588
b 16.000
+ 182.000 4217.588
b 16.000
+ 43.000 4391.529
b 16.000
+ 182.000 4391.529
b 16.000
+ 43.000 4565.471
b 16.000
+ 182.000 4565.471
b 16.000
+ 43.000 4739.412b 16.000
+ 182.000 4739.412
b 16.000
+ 43.000 4913.353
b 16.000
+ 182.000 4913.353
b 16.000
+ 43.000 5087.294
b 16.000
+ 182.000 5087.294
b 16.000
+ 43.000 5261.235b 16.000
+ 182.000 5261.235
b 16.000
+ 43.000 5435.176
b 16.000
+ 182.000 5435.176
b 16.000
+ 43.000 5609.118
b 16.000
+ 182.000 5609.118
b 16.000
+ 43.000 5783.059
b 16.000
SheetJob Number
Job Title
Client
Calcs by Checked by Date
CONSULTANTS LLP
E-Mail : [email protected]
KTP/20/13
ECHELON
M/s KTP CONSULTANTS PTE LTD
HT T&T MAY 2014
+ 182.000 5783.059
b 16.000
+ 112.500 43.000
b 16.000
+ 112.500 5957.000
b 16.000
Loadcase Designation
Ultimate limit state design loads
P (kN) Mx top (kNm) My top (kNm) Mx bot (kNm) My bot (kNm)
1 Axial 16400
2 Axial+Mxx 16400 1500
3 Axial+Myy 16400 100
4 Axial+Mxx+Myy 16400 1500 100
5 Axial+Mecc 16400 1640 1640
Design loads:
0
7500
5000
2500
0
X
X
Y
Y
CP65 - 1999
General design parameters:Given: Lo = 5.000 m fcu = 50 MPa fy = 460 MPa Ac = 1342763 mm
Assumptions: (1) The general conditions of clause 3.8.1 are applicable. (2) The specified design axial loads include the self-weight of the column. (3) The design axial loads are taken constant over the height of the column.
Design approach:The column is designed using an iterative procedure: (1) An area of reinforcement is chosen. (2) The column design charts are constructed. (3) The corresponding slenderness moments are calculated. (4) The design axis and design ultimate moment are determined . (5) The design axial force and moment capacity is checked on the relevant design chart. (6) The safety factor is calculated for this load case.
(7) The procedure is repeated for each load case. (8) The critical load case is identified as the case yielding the lowest safety factor about the design axis
Through inspection: Load case 1 (Axial) is critical.
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SheetJob Number
Job Title
Client
Calcs by Checked by Date
CONSULTANTS LLP
E-Mail : [email protected]
KTP/20/13
ECHELON
M/s KTP CONSULTANTS PTE LTD
HT T&T MAY 2014
Check for miminum eccentricity: 3.8.2.4 Check that the eccentricity exceeds the minimum in the plane of bending: Use emin = 20mmMmin = 184.5 kNm about the X-X axis.
Design of column section for ULS:
The column is checked for applied moment about the design axis. Through inspection: the critical section lies near mid-height of the column. The design axis for the critical load case 1 lies at an angle of 270.00to the X-axis The safety factor for the critical load case 1 is 1.28
For bending about the design axis:
Interaction Diagram
Momentmax=1155kNm@1
1E3kN
-4000-2000
200040006000800010E312E314E316E318E320E322E324E326E328E330E3
32E334E3
-1200
-1000
-800
-600
-400
-200
0.0
0
200
400
600
800
1000
1200
Axialload(kN)
Bending moment (kNm)
16400 kN
813kN
m
Moment distribution along the height of the column for bending about the design axis: At the top, Mx = 406.4 kNm Near mid-height, Mx = 812.9 kNm At the bottom, Mx = 406.4 kNm
SheetJob Number
Job Title
Client
Calcs by Checked by Date
CONSULTANTS LLP
E-Mail : [email protected]
KTP/20/13
ECHELON
M/s KTP CONSULTANTS PTE LTD
HT T&T MAY 2014
Stresses near mid-height of the column for the critical load case 1
0
7500
5000
2500
0
XX
Y
Y
CP65 - 1999
270.0
D
D
Summary of design calculations:
Design table for critical load case:
Moments and Reinforcement for LC 1:Axial
Top Middle Bottom
Madd-x (kNm) 0.0 -0.0 -0.0
Madd-y (kNm) 406.4 -812.9 -406.4
Mx (kNm) 0.0 -0.0 0.0
My (kNm) 406.4 -812.9 406.4
M' (kNm) 406.4 812.9 406.4
Design axis () 90.00 270.00 270.00
Safety factor 1.69 1.28 1.69
Asc (mm) 14476 14476 14476
Percentage 1.07 % 1.07 % 1.07 %
AsNom (mm) 5371 5371 5371
Critical load case: LC 1
Design results for all load cases:
Load case Axis N (kN) M1 (kNm) M2 (kNm) Mi (kNm)Madd (kNm) Design M (kNm) M' (kNm)Safetyfactor
Load case 1 Axial
X-XY-Y 16400.0
0.00.0
0.00.0
0.00.0
0.0812.9 Middle
0.0812.9 812.9 1.279
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SheetJob Number
Job Title
Client
Calcs by Checked by Date
CONSULTANTS LLP
E-Mail : [email protected]
KTP/20/13
ECHELON
M/s KTP CONSULTANTS PTE LTD
HT T&T MAY 2014
Load case Axis N (kN) M1 (kNm) M2 (kNm) Mi (kNm)Madd (kNm) Design M (kNm) M' (kNm)Safetyfactor
Load case 2 Axial+Mxx
Load case 3 Axial+Myy
Load case 4 Axial+Mxx+My
Load case 5 Axial+Mecc
X-XY-Y 16400.0
0.00.0
1500.00.0
900.00.0
315.11.9 Bottom
1500.0813.3 406.6 1.686
X-XY-Y 16400.0
0.00.0
0.0100.0
0.060.0
0.0822.8 Middle
0.0753.3 753.3 1.331
X-XY-Y 16400.0
0.00.0
1500.0100.0
900.060.0
0.00.0 Bottom
1500.0753.3 406.6 1.686
X-XY-Y 16400.0
0.00.0
1640.01640.0
984.0984.0
0.0190.5 Bottom
1640.02046.6 406.6 1.686
Load case 1 (Axial) is critical.