Seismic Design of Steel Structures in Accordance with CSA-S16-09
CSA S16-01 Example 001
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Transcript of CSA S16-01 Example 001
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8/13/2019 CSA S16-01 Example 001
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Software VerificationPROGRAM NAME: SAP2000
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CSA S16-01 Example 001 - 1
CSA S16-01 Example 001
WIDE FLANGE MEMBER UNDER BENDING
EXAMPLE DESCRIPTION
The frame object moment and shear strength is tested in this example.
In the example a simply supported beam is (a) laterally restrained along its fulllength, (b) laterally restrained along its quarter points, at mid-span and at the
ends (c) laterally restrained along at mid-span and is subjected to a uniformfactored load of DL = 7 kN/m and LL = 15 kN/m. This example was tested using
the CSA S16-01 steel frame design code. The moment and shear strengths arecompared with Handbook of Steel construction (9thEdition) results.
GEOMETRY,PROPERTIES AND LOADING
L = 8.0 m
TECHNICAL FEATURES TESTED
Section Compactness Check (Bending) Member Bending Capacity, Mr (Fully Restrained) Member Bending Capacity, Mr (Buckling) Member Bending Capacity, Mr (LTB)
Material Properties
E = 2x108kN/m2
Fy = 350 kN/m2
Loading
WD = 7 kN/mWL = 15 kN/m
Design Properties
ASTM A992CSA G40.21 350W
W410X46
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CSA S16-01 Example 001 - 2
RESULT COMPARISON
Independent results are taken from Example 1, 2 and 3 on page 5-84 and 5-85 ofthe Hand Book of Steel Construction to CSA S16-01 published by Canadian
Institute of Steel Construction.
Output Parameter SAP2000 IndependentPercent
Difference
Compactness Class 1 Class 1 0.00%
Design Moment, Mf(kN-m) 250.0 250.0 0.00%
(a) Moment Capacity, Mr33of
W410X46 (kN-m) w/ lb= 0 m
278.775 278.775 0.00%
(b) Moment Capacity, Mr33of
W410X46 (kN-m) w/ lb= 2 m
268.57 268.42 0.06%
(c) Moment Capacity, Mr33ofW410X60 (kN-m) w/ lb= 4 m
287.69 287.64 0.02%
COMPUTER FILE: CSAS16-01EX001
CONCLUSION
The results show an exact match with the independent results.
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CSA S16-01 Example 001 - 3
HAND CALCULATION
Properties:
Material: CSA G40.21 Grade 350W
fy= 350 MPa
E = 200,000 MPa
G = 76923 MPa
Section: W410x46
bf= 140 mm, tf= 11.2 mm, d = 404 mm, tw= 7 mm
2 404 2 11.2 381.6fh d t mm
Ag= 5890 mm2
I22= 5,140,000 mm4
Z33= 885,000 mm3
J = 192,000 mm4
11 61.97 10
w
C mm
Section: W410x60
bf= 178 mm, tf= 12.8 mm, d = 408 mm, tw= 7.7 mm
2 408 2 12.8 382.4fh d t mm
Ag= 7580 mm2
I22= 12,000,000 mm4
Z33= 1,190,000 mm3
J = 328,000 mm4
11 64.68 10wC mm
Member:
L = 8 m
= 0.9
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CSA S16-01 Example 001 - 4
Loadings:
wf= (1.25wd+ 1.5wl)=1.25(7) + 1.5(15) = 31.25 kN/m
2 231.25 8
8 8
f
f
w LM
250fM kN m
Section Compactness:
Localized Buckling for Flange:
.1
145 1457.75
350Cl
yF
W410x46
1406.25
2 2 11.2
f
f
b
t
.1Cl , No localized flange buckling
Flange is Class 1.W410x60
1786.95
2 2 12.8
f
f
b
t
.1Cl , No localized flange buckling
Flange is Class 1.
Localized Buckling for Web:
.1
1100 1100 01 0.39 1 0.39 58.8
5890 350350
f
Cl
yy
C
CF
W410x46
381.654.51
7w
h
t
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CSA S16-01 Example 001 - 5
.1Cl , No localized web buckling
Web is Class 1.
Section is Class 1
W410x60
382.449.66
7.7w
h
t
.1Cl , No localized web buckling
Web is Class 1.
Section is Class 1
Section Bending Capacity for W410x46:
75.30910/000,885350 6
33 ZFM yp kN-m
775.27875.3099.0 pM kN-m
Member Bending Capacity for L b=0 mm (Ful ly Restrained):
Braced segment center moment is greater than the braced segment end moments, so
2 = 1.000
2
2
22 22 0
u w
EM EI GJ I C as L
L L
33
33 33 331.15 1 0.28
p
r p p
u
MM M M
M
33
0.28 0p
u
u
MasM
M
33 33 331.15r p pleading to M M M
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CSA S16-01 Example 001 - 6
So
33 33 278.775r pM M kN m
Member Bending Capacity for L b=2000 mm:
Braced segment center moment is greater than the braced segment end moments, so
2 = 1.000
2
2
22 22u w
EM EI GJ I C
L L
5 6 3
25
6 9
2. 10 5.14 10 76923 192 10
1.02. 10
2000 5.14 1 0 197 102000
uM
6532.96 10 532.96uM N mm kN m
0.67 0.67 309.75 208 532.96 ,p uM M kN m so
33
33
3333 28.0115.1
p
u
p
pr M
M
MMM
33
309.751.15 0.9 309.75 1 0.28 268.42 278.775
532.96r
M kN m kN m
33 268.42
rM kN m
Section Bending Capacity for W410x60:
6
33 350 1,190,000 /10 416.5p yM F Z kN m
85.3745.4169.0 pM kN-m
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CSA S16-01 Example 001 - 7
Member Bending Capacity for L b= 4000 m:
Braced segment center moment is greater than the braced segment end moments, so
2 = 1.000
2
2
22 22u w
EM EI GJ I C
L L
5 6 3
25
6 9
2. 10 12 10 76923 328 10
1.02. 10
4000 12 10 468 104000
uM
6350.47 10 350.47uM N mm kN m
0.67 0.67 309.75 279 350.47 ,p uM M kN m so
33
33
3333 28.0115.1 p
u
p
pr M
M
MMM
33
416.51.15 0.9 416.5 1 0.28 287.64 278.775
350.47r
M kN m kN m
33 287.64
rM kN m