Wind Loads UK- Portal Frame WE
Short Description
Download Wind Loads UK- Portal Frame WE...
Description
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
1
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
Localized resource for UK
Example: Elastic analysis of a single bay portal frame A single bay portal frame made of rolled profiles is designed according to EN 1993-1-1. This worked example includes the elastic analysis of the frame using first order theory, and all the verifications of the members under ULS combinations.
,0 72
7,30
5,988
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
α
0 7,2
[m] 30,00
1 Basic data • • • • •
Total length : Spacing: Bay width : Height (max): Roof slope: 3,00
3,00
b = 72.00 m s = 7.20 m d = 30.00 m h = 7.30 m α = 5.0° 3,00
3,00
1
1 : Torsional restraints
3,00
0
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
2
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
2 Loads EN 1991-1-1
2.1 Permanent loads •
self-weight of the beam
•
roofing with purlins
G = 0.30 kN/m2 G = 0.30 × 7.20 = 2.16 kN/m
2.2 Snow loads
EN 1991-1-3
Characteristic values for snow loading on the roof in [kN/m] S = 0.8 × 1.0 × 1.0 × 0.772 = 0.618 kN/m² ⇒
for an internal frame: S = 0.618 × 7.20 = 4.45 kN/m s = 4,45 kN/m
α 7,30
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
for an internal frame:
30,00
[m]
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
3
Title
Example: Elastic analysis of a single bay portal frame
Sheet
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
2.3 Wind loads
EN 1991-1-4
Characteristic values for wind loading in kN/m for an internal frame Zone G: w = 9,18
wind direction
Zone J: w = 5,25
Zone H: w = 5,25
Zone I: w = 5,25
Zone D: w = 4,59 Zone E: w = 3,28
1,46
e/10 = 1,46
30,00
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
3 Load combinations
EN 1990
3.1 Partial safety factor •
γGmax = 1.35
(permanent loads)
•
γGmin = 1.0
(permanent loads)
•
γQ = 1.50
(variable loads)
•
ψ0 = 0.50
(snow)
•
ψ0 = 0.60
(wind)
•
γM0 = 1.0
•
γM1 = 1.0
3.2 ULS Combinations Combination 101 :
γGmax G + γQ Qs
Combination 102 :
γGmin G + γQ Qw
Combination 103 :
γGmax G + γQ Qs + γQ ψ0 Qw
Combination 104 :
γGmin G + γQ Qs + γQ ψ0 Qw
Combination 105 :
γGmax G + γQ ψ0 Qs + γQ Qw
Combination 106 :
γGmin G + γQ ψ0 Qs + γQ Qw
EN 1990 Table A1.1
EN 1990
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
4
Title
Example: Elastic analysis of a single bay portal frame
Sheet
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
3.3 SLS Combinations
EN 1990
Combinations and limits should be specified for each project or by National Annex.
4 Sections z
tf
4.1 Column Try UKB 610x229x125 – Steel grade S275 Depth
h = 612.2 mm
Web Depth
hw = 573.0 mm
tw y
y
Depth of straight portion of the web
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
dw = 547.6 mm Width
b = 229.0 mm
Web thickness
tw = 11.9 mm
Flange thickness
tf = 19.6 mm
Fillet
r = 12.7 mm
Mass
125.1 kg/m
Section area
A = 159 cm2
hw
Second moment of area /yy Iy = 98600 cm4 Second moment of area /zz Iz = 3930 cm4 Torsion constant
It = 154 cm4
Warping constant
Iw = 3.45 x 106 cm6
Elastic modulus /yy
Wel,y = 3220 cm3
Plastic modulus /yy
Wpl,y = 3680 cm3
Elastic modulus /zz
Wel,z = 343 cm3
Plastic modulus /zz
Wpl,z = 535 cm3
z b
h
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
5
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
4.2 Rafter Try UKB 457x191x89 – Steel grade S275 Depth
h = 463.4 mm
Web Depth
hw = 428.0 mm
Depth of straight portion of the web
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
dw = 407.6 mm Width
b = 191.9 mm
Web thickness
tw = 10.5 mm
Flange thickness
tf = 17.7 mm
Fillet
r = 10.2 mm
Mass
89.3 kg/m
Section area
A = 114 cm2
Second moment of area /yy Iy = 41000 cm4 Second moment of area /zz Iz = 2090 cm4 Torsion constant
It = 90.7 cm4
Warping constant
Iw = 1.04 x 106 cm6
Elastic modulus /yy
Wel,y = 1770 cm3
Plastic modulus /yy
Wpl,y = 2014 cm3
Elastic modulus /zz
Wel,z = 218 cm3
Plastic modulus /zz
Wpl,z = 338 cm3
5 Global analysis The joints are assumed to be: •
pinned for column bases
•
rigid for beam to column.
The frame has been modelled using the EFFEL program.
EN 1993-1-1 § 5.2
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
6
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
5.1 Buckling amplification factor αcr
EN 1993-1-1 In order to evaluate the sensitivity of the frame to 2 order effects, a buckling § 5.2.1 analysis is performed to calculate the buckling amplification factor αcr for the load combination giving the highest vertical load: γmax G + γQ QS (combination 101). nd
For this combination: αcr = 12.74
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
The first buckling mode is shown hereafter.
So :
αcr = 12.74 > 10
First order elastic analysis may be used.
5.2 Effects of imperfections The global initial sway imperfection may be determined from
φ = φ0 αh αm = where
1 × 0.740 × 0.866 = 3.204 ⋅10 −3 200
φ0 = 1/200 αh =
2 2 = = 0.740 h 7.30
αm = 0.5(1 +
1 ) = 0.866 m
m = 2 (number of columns)
EN 1993-1-1 § 5.2.1 (3)
EN 1993-1-1 § 5.3.2 (3)
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
7
Title
Example: Elastic analysis of a single bay portal frame
Sheet
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
Sway imperfections may be disregarded where HEd ≥ 0.15 VEd.
EN 1993-1-1 § 5.3.2 (4)
The effects of initial sway imperfection may be replaced by equivalent horizontal forces: Heq = φ VEd in the combination where HEd < 0.15 ⎢VEd ⎢
The following table gives the reactions at supports. Left column 1
Right column 2
Total
ULS
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
0.15 ⎢VEd ⎢
HEd,1
VEd,1
HEd,2
VEd,2
HEd
VEd
kN
kN
Kn
kN
kN
kN
101
-125.5
-161.5
122.4
-172.4
0
-344.70
51.70
102
95.16
80.74
-24.47
58.19
70.69
138.9
20.83
103
-47.06
-91.77
89.48
-105.3
42.42
-197.1
29.56
104
-34.59
-73.03
77.01
-86.56
42.42
-159.6
23.93
105
43.97
11,97
26.72
-10.57
70.69
1.40
0.21
106
56.44
30.71
14.25
8.17
70.69
38.88
5.83
Comb.
The sway imperfection has only to be taken into for the combination 101:
⇒
VEd
Heq = φ.VEd
kN
kN
172.4
0.552
Modelling with Heq for the combination 101
EN 1993-1-1 § 5.3.2 (7)
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
8
Title
Example: Elastic analysis of a single bay portal frame
Sheet
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
5.3 Results of the elastic analysis 5.3.1 Serviceability limit states Combinations and limits should be specified for each project or in National Annex. For this example, the deflections obtained by modeling are as follows: Vertical deflections:
G + Snow:
Dy = 164 mm = L/183
Snow only:
Dy = 105 mm = L/286
Horizontal deflections:
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
Deflection at the top of column by wind only Dx = 38 mm = h/157
5.3.2 Ultimate limit states Moment diagram in kNm Combination 101:
Combination 102:
EN 1993-1-1 § 7 and EN 1990
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
9
of
30
Eurocode Ref
Combination 103:
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
Combination 104:
Combination 105:
Combination 106:
Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
10
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
6 Column verification Profile UKB 610x229x125 - S275 (ε = 0.92)
The verification of the member is carried out for the combination 101 : NEd = VEd = MEd =
161.5 kN (assumed to be constant along the column) 122.4 kN (assumed to be constant along the column) 755 kNm (at the top of the column)
6.1 Classification of the cross section •
The web slenderness is c / tw = 46.02
Web:
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
dN =
α=
N Ed 161500 = = 49.35 mm t w f y 11.9 × 275
d w + d N 547.6 + 49.35 = = 0.545 > 0.50 2d w 2 × 547.6
The limit for Class 1 is : 396ε / (13α -1) = Then : c / tw = 46.02 < 59.87 •
Flange:
396 × 0.92 = 59.87 13 × 0.545 − 1
The web is class 1.
The flange slenderness is c / tf = 95.9/ 19.6= 4.89
The limit for Class 1 is : 9 ε = 9 × 0.92 = 8.28 Then : c / tf = 4.89 < 8.28
The flange is Class 1
So the section is Class 1. The verification of the member will be based on the plastic resistance of the cross-section.
EN 1993-1-1 § 5.5
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
11
Title
Example: Elastic analysis of a single bay portal frame
Sheet
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
6.2 Resistance of cross section NOTE: This example uses a value for yield strength of 275 N/mm2, irrespective of flange thickness. The UK National Annex requires yield strength to be taken from the product standard, which will reduce the value for thicknesses over 16 mm. (UK NA still to be confirmed at April 2007) Verification to shear force
Shear area :
Av = A - 2btf + (tw+2r)tf
Av = 15900 − 2 × 229 × 19.6 + (11.9 + 2 × 12.7) × 19.6 = 7654 mm
2
Av > η.hw.tw = 6819 mm2 (η = 1)
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
Vpl,Rd = Av (fy /
EN 1993-1-1 § 6.2.8 (2)
OK
3 ) /γM0 = (7654×275/ 3 )×10-3
Vpl,Rd = 1215 kN VEd / Vpl,Rd = 122.4 / 1215 = 0.10 < 0.50 The effect of the shear force on the moment resistance may be neglected. Verification to axial force
Npl,Rd = A fy / γM0 = (15900 × 275/1.0) ×10-3
EN 1993-1-1 § 6.2.4
Npl,Rd = 4372.5 kN NEd = 161.5 kN < 0.25 Npl,Rd = 0.25 x 4372.5 = 1093.1 kN and
NEd = 161.5 kN <
0.5hw t w f y
γ M0
0.5 × 573 × 11.9 × 275 = = 937.6 kN 1 × 103
EN 1993-1-1 § 6.2.8 (2)
The effect of the axial force on the moment resistance may be neglected. Verification to bending moment
Mpl,y,Rd = (3680 × 275/1.0) ×10-3 Mpl,y,Rd = 1012 kNm My,Ed = 755 kNm < Mpl,y,Rd = 1012 kNm OK
EN 1993-1-1 § 6.2.5
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
12
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
6.3 Buckling resistance The buckling resistance of the column is sufficient if the following conditions EN 1993-1-1 are fulfilled (no bending about the weak axis, Mz,Ed = 0): § 6.3.3 N Ed + k yy χ y N Rk
γ M1
M y,Ed ≤1 M y,Rk
χ LT
γ M1
M y,Ed ≤1 M y,Rk
N Ed + k zy χ y N Rk
χ LT
γ M1
γ M1
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
The kyy and kzy factors will be calculated using the Annex A of EN 1993-1-1. The frame is not sensitive to second order effects (αcr = 12.7> 10). Then the EN 1993-1-1 buckling length for in-plane buckling may be taken equal to the system length. § 5.2.2 (7) Lcr,y = 5.99 m Note: For a single bay symmetrical frame that is not sensitive to second order effects, the check for in-plane buckling is generally not relevant. The verification of the cross-sectional resistance at the top of the column will be determinant for the design. Regarding the out-of-plane buckling, the member is laterally restrained at both ends only. Then : Lcr,z = 5.99 m Lcr,LT = 5.99 m
and •
Buckling about yy
Lcr,y = 5.99 m
h/b = 2.67 > 1.2 and tf = 19.6 < 40 mm Buckling curve : a (αy = 0.21)
N cr,y = π 2
λy =
EI y L2cr,y
Af y N cr,y
=
210000 × 98600 × 10 4 =π2 =56956 kN 59902 × 103
15900 × 275 = 0.277 56956 × 103
EN 1993-1-1 § 6.3.1.2 (2) Table 6.1 EN 1993-1-1 § 6.3.1.3 (1)
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
13
of
30
Eurocode Ref
[
(
Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
)
]
φy = 0.5 1 + α λ y − 0.2 + λ y = 0.5 × [1 + 0.21(0.277 − 0.2) + 0.2772 ]= 0.546 χy = •
2
1
φy + φy − λ 2
2 y
=
1 0.546 + 0.546 2 − 0.277 2
= 0.984
Lcr,z = 5.99 m
Buckling about zz
EN 1993-1-1 § 6.3.1.2 (2)
Buckling curve : b (αz = 0.34)
Af y
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
λz =
N cr,z
[
Table 6.1
4 EI z 2 210000 × 3930 × 10 π = 2270 kN = L2cr,z 5990 2 ×103
N cr,z = π 2
EN 1993-1-1 § 6.3.1.3 (1)
15900 × 275 = 1.388 2270 ×10 3
=
(
)
]
φz = 0.5 1 + α λ z − 0.2 + λ z = 0.5 × [1 + 0.34(1.388 − 0.2 ) + 1.3882 ] = 1.665
χz =
•
1
φz + φz2 − λ
=
2 z
2
1 1.665 + 1.6652 − 1.3882
= 0.387
Buckling curve : c (αLT = 0.49) Moment diagram with linear variation : ψ = 0 M cr = C1 M cr = 1.77 ×
Lcr,LT
2
5990 × 10 2
Table 6.5
6
4
3.45 × 10 5990 × 80770 × 154 × 10 + 2 4 3930 × 10 π × 210000 × 3930 × 10 4 12
Mcr = 1517 kNm
Wpl,y f y M cr
C1 = 1.77
2
π × 210000 × 3930 × 10
λ LT =
EN 1993-1-1 § 6.3.2.3
I W Lcr,LT GI t + IZ π 2 EI Z
2
=
EN 1993-1-1 § 6.3.1.2 (1)
Lcr,LT = 5.99 m
Lateral torsional buckling
π 2 EI Z
EN 1993-1-1 § 6.3.1.2 (1)
3680 × 103 × 275 = 0.817 1517 × 106
2
4
NCCI SN003
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
14
of
30
Eurocode Ref
[
Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
(
)
2
φLT = 0.5 1 + α LT λ LT − λ LT,0 + βλ LT
]
EN 1993-1-1 § 6.3.2.3 (1)
with λ LT,0 = 0.40 and β =0.75
φLT = 0.5 × [1 + 0.49(0.817 − 0.4) + 0.75 × 0.8172 ] = 0.852 χ LT =
1 2
2 − βλ LT φLT + φLT
=
1 0.852 + 0.8522 − 0.75 × 0.817 2
= 0.754
The influence of the moment distribution on the design buckling resistance moment of the beam is taken into account through the f-factor :
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
[
(
f = 1 − 0.5 × (1 − k c ) 1 − 2 λ LT − 0.8 1 = 0.752 where: kc = 1.33 − 0.33ψ
)]
EN 1993-1-1 § 6.3.2.3 (2) Table 6.6
2
(ψ = 0)
[
]
f = 1 − 0.5 × (1 − 0.752) 1 − 2(0.817 − 0.8) = 0.876 < 1 0.754 χ = 0.861 < 1 χLT,mod = LT = f 0.876 2
Calculation of the factors kyy and kzy according to Annex A of EN 1993-1-1
N Ed 161.5 1− N cr, y 56956 μy = = = 0.999 N Ed 161.5 1 − χy 1 − 0.984 × N cr, y 56956 1−
EN 1993-1-1 Annex A
N Ed 161.5 1− N cr,z 2270 μz = = 0.955 = 161.5 N Ed 1− χz 1 − 0.387 × 2270 N cr,z 1−
wy =
Wpl,y
wz =
Wpl,z
Wel,y
Wel,z
=
3680 = 1.143 < 1.5 3220
=
535 = 1.56 > 1.5 343
EN 1993-1-1 Annex A ⇒
wz = 1.5
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
15
of
30
Eurocode Ref
M cr,0 = C1
Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
π 2 EI Z Lcr,LT
2
I W Lcr,LT GI t + IZ π 2 EI Z
2
NCCI SN003
Mcr,0 is the critical moment for the calculation of λ0 for uniform bending moment as specified in Annex A. ⇒ C1 = 1 M cr,0 = 1×
π 2 × 210000 × 3930 × 10 4 5990 2 × 106
3.45 × 1012 5990 2 × 80770 × 154 × 10 4 + 3930 × 10 4 π 2 × 210000 × 3930 × 10 4
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
M cr,o = 857.2 kNm Wpl,y f y
λ0 =
M cr,o
3680 ×103 × 275 = = 1.087 857.2 × 106
λ 0 lim = 0.2 C1 4 (1 −
N Ed N )(1 − Ed ) N cr,z N cr,TF
with Ncr,TF = Ncr,T
(doubly
EN 1993-1-1 Annex A
symmetrical section)
Critical axial force in the torsional buckling mode
N cr,T
π 2 EI w A = (GI t + ) I0 h2
For a doubly symmetrical section,
I 0 = I y + I z + ( y02 + z02 ) A = 98600 + 3930 = 102530 cm4 N cr,T =
12 15900 4 2 210000 × 3.45 × 10 × ( 80770 × 154 × 10 + π ) × 10 −3 4 2 102530 × 10 5990
Ncr,T = 5019 kN So: λ 0 lim = 0.2 1.77 4 (1 −
161.5 161.5 )(1 − ) = 0.259 2270 5019
λ 0 > λ 0 lim → Section susceptible to torsional deformations
NCCI SN003
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
16
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
C my = C my,0 + (1 − C my,0 )
with
εy =
and aLT = 1 −
ε y a LT 1 + ε y a LT
M y,Ed A 755 × 103 × 159 × 10 2 = 23.08 (class 1) = N Ed Wel,y 161.5 × 3220 × 103 154 It = 0.998 = 1− Iy 98600
Calculation of the factor Cmy,0
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
Cmy,0 = 0.79 + 0.21ψ y + 0.36(ψ y − 0.33)
ψy =0
Cmy,0
N Ed N cr,y
161.5 = 0.79 − 0.1188 = 0.790 56956
EN 1993-1-1 Annex A Table A2
Calculation of the factors Cmy and Cm,LT : C my = Cmy,0 + (1 − C my,0 )
ε y aLT 1 + ε y aLT
Cmy = 0.790 + (1 − 0.790)
23.08 × 0.998 = 0.964 1 + 23.08 × 0.998
a LT
2 C mLT = C my
(1 − CmLT = 0.964 2 ×
N Ed N )(1 − Ed ) N cr,z N cr,T
≥1
0.998 = 0.978 < 1 161.5 161.5 (1 − )(1 − ) 2270 5019
⇒ CmLT = 1
EN 1993-1-1 Annex A
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
17
Title
Example: Elastic analysis of a single bay portal frame
Sheet
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
Calculation of the factors Cyy and Czy :
C yy = 1 + ( wy − 1)[(2 −
npl =
W 1.6 2 1.6 2 2 Cmy λ max − Cmy λ max )npl − bLT ] ≥ el,y wy wy Wpl,y
EN 1993-1-1 Annex A
N Ed 161.5 ×103 = 0.037 = N Rk / γ M1 159 ×102 × 275 / 1
Mz,Ed = 0 ⇒ bLT = 0 and d LT = 0 Cyy = 1 + (1.143 − 1) × [(2 −
λ max = λ z = 1.388
1.6 1.6 × 0.9642 ×1.388 − × 0.9642 ×1.3882 ) × 0.037] 1.143 1.143
Cyy = 0.988
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
Cyy >
Wel,y Wpl,y
=
3220 = 0.875 3680
Czy = 1 + ( wy − 1)[(2 −
w W 14 2 2 Cmy λ max ) npl − d LT ] ≥ 0.6 y el,y 5 wy wz Wpl,y
C zy = 1 + (1 .143 − 1)[( 2 −
Czy > 0.6
wy Wel,y wz Wpl,y
OK
= 0 .6
14 × 0 .964 2 × 1 .388 2 ) × 0 .037 ] = 0 .943 5 1 .143 1.143 3220 × = 0.458 1.5 3680
Calculation of the factors kyy and kzy : k yy = CmyCmLT
μy 1 N 1 − Ed C yy N cr, y
k yy = 0.964 × 1×
1 0.999 × = 0.978 161.5 0.988 1− 56956
OK
EN 1993-1-1 Annex A
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
18
of
30
Eurocode Ref
k zy = CmyCmLT
Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
μz 1−
k zy = 0.964 × 1×
N Ed N cr,y
w 1 0.6 y Czy wz
1 1.143 0.955 × × 0.6 × = 0.513 161.5 0.943 1 . 50 1− 56956
Verification with interaction formulae
N Ed + k yy χ y N Rk
γ M1
M y,Ed ≤1 M y,Rk
χ LT
γ M1
161.5 × 10 755.106 + 0.978 × = 0.88 η.hw.tw = 428×10.5 = 4494 mm2 Vpl,Rd = Av (fy /
3 ) /γM0 = 5154×275/ 3 /1000 = 818.3 kN
VEd / Vpl,Rd = 118.5 / 818.33 = 0.145 < 0.50 OK
Verification to axial force -3
Npl,Rd = 11400 x 275 x 10 = 3135 kN
EN 1993-1-1 § 6.2 EN 1993-1-1 § 6.2.8 (2)
EN 1993-1-1 § 6.2.4
NEd = 136 kN < 0.25 Npl,Rd= 0.25 × 3135 = 783.8 kN and NEd = 136 kN < OK
0.5hw t w f y
γ M0
0.5 × 428 ×10.5 × 275 = ×10−3 = 617.9kN 1
EN 1993-1-1 § 6.2.8 (2)
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
21
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
EN 1993-1-1 § 6.2.5
Verification to bending moment
Mpl,y,Rd = 2014 × 275 × 10-3 = 553.9 kNm My,Ed = 349.1 kNm < Mpl,y,Rd = 553.9 kNm
OK
7.3 Buckling resistance Uniform members in bending and axial compression
Verification with interaction formulae N Ed + k yy χ y N Rk
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
γ M1
•
M y,Ed ≤1 M y,Rk
χ LT
and
γ M1
EN 1993-1-1 § 6.3.3
M y,Ed N Ed ≤1 + k zy χ z N Rk M y,Rk χ LT γ M1 γ M1
Buckling about yy:
For the determination of the buckling length about yy, a buckling analysis is performed to calculate αcr for the load combination giving the highest EN 1993-1-1 vertical load, with a fictitious restraint at top of column: § 6.3.1.2 (2) Combination 101 ⇒ αcr = 32.40 Table 6.1
EN 1993-1-1 § 6.3.1.3 (1)
Buckling curve : a (h/b>2)
⇒ αy = 0.21
N cr,y = α cr N Ed = 32.40 × 136 = 4406 kN λy =
Af y N cr,y
=
11400 × 275 = 0.844 4406.103
EN 1993-1-1 § 6.3.1.2 (2) Table 6.1
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
22
of
30
Eurocode Ref
[
Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
(
)
2
φ y = 0.5 1 + α λ y − 0.2 + λ y
[
]
]
φ y = 0.5 × 1 + 0.21× (0.844 − 0.2) + 0.8442 = 0.924 χy =
•
1 φy + φy − λ 2
2 y
=
1 0.924 + 0.924 2 − 0.844 2
= 0.769
Buckling about zz:
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
For buckling about zz and for lateral torsional buckling, the buckling length is taken as the distance between torsional restraints: Lcr = 6.00m Note: the intermediate purlin is a lateral restraint of the upper flange only. Its influence could be taken into account but it is conservatively neglected in the following.
Flexural buckling
EN 1993-1-1 § 6.3.1.3
Lcr,z = 6.00 m N cr,z = π 2
4 EI z 2 210000 × 2090 × 10 = π = 1203 kN L2cr,z 6000 2 × 10 3
Torsional buckling
NCCI
Lcr,T = 6.00 m N cr,T =
SN003
π 2 EI w A (GI t + ) 2 I0 Lcr,T
with yo = 0 and zo = 0
(doubly symmetrical section)
I 0 = I y + I z + ( y 02 + z 02 )A = 41000 + 2090 = 43090 cm4 N cr,T =
12 11400 4 2 210000 × 1.04.10 −3 × × × × + π 10 ( 80770 90 . 7 10 ) 43090.10 4 6000 2
Ncr,T = 3522 kN
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
23
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
Ncr = min ( Ncr,z ; Ncr,T ) = 1203 kN Af y
λz =
N cr
EN 1993-1-1 § 6.3.1.3 (1)
11400 × 275 = 1.614 1203 × 103
=
Buckling curve : b
EN 1993-1-1 § 6.3.1.2 (1)
αz = 0.34
[
(
)
2
φ z = 0 . 5 1 + α λ z − 0 .2 + λ z
[
]
Table 6.1
]
φ z = 0.5 × 1 + 0.34 × (1.614 − 0.2 ) + 1.614 2 =2.043
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
χz = •
1 φz + φ2z − λ
2 z
=
1 2.043 + 2.0432 − 1.6142
= 0.303
Lateral torsional buckling :
EN 1993-1-1 § 6.3.1.3
Lcr,LT = 6.00 m Buckling curve : c
αLT = 0.49
Table 6.5
Moment diagram along the part of rafter between restraints : Combination 101
Calculation of the critical moment:
NCCI
ψ = - 0.487 q = - 9.56 kN/m ⇒
C1 = 2.75
SN003
qL2 = - 0.123 μ= 8M
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
24
of
30
Eurocode Ref
M cr = C1 M cr = 2.75 ×
π 2 EI Z Lcr,LT
Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
NCCI
2
I W Lcr,LT GI t + IZ π 2 EI Z
2
π2 × 210000 × 2090 ×104 60002 ×106
1.04 ×1012 60002 × 80770 × 90.7 ×104 + 2090 ×104 π 2 × 210000 × 2090 ×104
Mcr = 1100 kNm λ LT =
Wpl, y f y M cr
[
2010 × 103 × 275 = 0.709 1100 × 106
=
(
)
2
φLT = 0.5 1 + α LT λ LT − λ LT,0 + βλ LT
]
EN 1993-1-1 § 6.3.2.3 (1)
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
with λ LT,0 = 0.40 and β =0.75
[
]
φLT = 0.5 × 1 + 0.49 × (0.709 − 0.4) + 0.75 × 0.7092 = 0.764 χ LT =
1 φLT + φ2LT − βλ
kc = 0.91
2 LT
1
=
[
0.764 + 0.7642 − 0.75 × 0.7092
(
f = 1 − 0.5 × (1 − k c ) 1 − 2 λ LT − 0.8
[
)]
= 0.821
2
]
f = 1 − 0.5 × (1 − 0.91) × 1 − 2 × (0.709 − 0.8) = 0.956 < 1
χLT,mod =
2
EN 1993-1-1 § 6.3.2.3 (2) Table 6.6
χ LT 0.821 = = 0.859 < 1 f 0.956
Combination 101
NEd = 136 kN compression My,Ed = 349.1 kNm Mz,Ed = 0 ⇒
Section class1
N Ed + k yy χ y N Rk
γ M1
M y,Ed ≤1 M y,Rk
χ LT
γ M1
ΔMy,Ed = 0 and ΔMz,Ed = 0 N Ed + k zy χ z N Rk
γ M1
M y,Ed ≤1 M y,Rk
χ LT
γ M1
EN 1993-1-1 § 6.3.3
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
25
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
N Ed 136 1− N cr, y 4406 μy = = = 0.993 136 N Ed 1 − 0.769 × 1 − χy 4406 N cr, y 1−
EN 1993-1-1 Annex A
N Ed 136 1− N cr,z 1203 = 0.918 μz = = N Ed 136 1 − χz 1 − 0.303 × N cr,z 1203
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
1−
wy =
Wpl, y
wz =
Wpl, z 338 = = 1.550 > 1.50 Wel,z 218
Wel, y
M cr,0 = C1
=
EN 1993-1-1 Annex A
2010 = 1.136 < 1.50 1770
π 2 EI Z Lcr,LT
2
⇒
wz = 1.50
NCCI
2
I W Lcr,LT GI t + IZ π 2 EI Z
SN003
Mcr,0 is the critical moment for the calculation of λ0 for uniform bending moment as specified in Annex A. ⇒ C1 = 1 π 2 × 210000 × 2090 × 10 4 6000 2 × 106 = 400.2 kNm
M cr,0 = 1 ×
M cr,o
λ0 =
Wpl,y f y M cr,o
=
1.04 × 1012 6000 2 × 80770 × 90.7 × 10 4 + 2 π × 210000 × 2090 × 10 4 2090 × 10 4
EN 1993-1-1 Annex A
2010 ×103 × 275 = 1.175 400.2 ×106
λ 0 lim = 0.2 C1 4 (1 −
N N Ed )(1 − Ed ) N cr, TF N cr, z
with Ncr,TF = Ncr,T
(doubly
λ 0 lim = 0.2 2.75 4 (1 −
with C1 = 2.75
symmetrical section)
136 136 )(1 − ) = 0.319 1203 3522
λ 0 =1.175 > λ 0 lim =0.319
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
26
Title
Example: Elastic analysis of a single bay portal frame
Sheet
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
Cmy = Cmy,0 + (1 − Cmy,0 )
with ε y = and
ε y aLT
EN 1993-1-1 Annex A
1 + ε y aLT
M y,Ed A 349.1×106 11400 = × =16.53 (class 1) 3 N Ed Wel,y 136 × 10 1770 × 103
a LT = 1 −
It 90.7 = 0.998 =1− Iy 41000
EN 1993-1-1 Annex A
Calculation of the factor Cmy,0
Moment diagram along the rafter:
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
Table A2 My,Ed = maximum moment along the rafter = 755kNm
δ = maximum displacement along the rafter = 164 mm
30m
⎡ π 2 EI y δ x ⎤ N Cmy,0 = 1 + ⎢ 2 − 1⎥ Ed ⎢⎣ L M y,Ed ⎥⎦ N cr,y ⎡ π2 × 210000 × 41000 × 104 × 164 ⎤ 136 C my,0 = 1 + ⎢ − 1⎥ =0.978 300002 × 755 × 106 ⎣ ⎦ 4406 Calculation of the factors Cmy and Cm,LT : Cmy = Cmy,0 + (1 − Cmy,0 )
ε y aLT 1 + ε y aLT
C my = 0.978 + (1 − 0.978)
16.53 × 0.998 = 0.996 1 + 16.53 × 0.998
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
27
Title
Example: Elastic analysis of a single bay portal frame
Sheet
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
aLT
2 CmLT = Cmy
(1 −
N Ed N )(1 − Ed ) N cr,z N cr,T
EN 1993-1-1 Annex A
≥1
0.998 = 1.072 > 1 136 136 ) )(1 − (1 − 3522 1203
C mLT = 0.996 2 ×
Calculation of the factors Cyy and Czy
C yy = 1 + ( w y − 1)[(2 −
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
n pl =
W 1.6 2 2 1.6 2 Cmy λ max )n pl − b LT ] ≥ el, y Cmy λ max − wy Wpl, y wy
N Ed 136 × 103 = 0.043 = N Rk / γ M1 11400 × 275 / 1
Mz,Ed = 0 ⇒ bLT = 0 and d LT = 0 C yy = 1 + (1.136 − 1)[( 2 −
C zy = 1 + ( w y − 1)[(2 −
Wel, y 1770 = = 0.88 OK Wpl, y 2010
w y Wel, y 14 2 2 C my λ max ) n pl − d LT ] ≥ 0.6 5 wy w z Wpl, y
C zy = 1 + (1.136 − 1)[(2 − w y Wel, y w z Wpl, y
λ max = λ z = 1.614
1 .6 1. 6 × 0.996 2 × 1.614 − × 0.996 2 × 1.614 2 ) × 0.043] 1.136 1.136
Cyy = 0.977 ≥
C zy ≥ 0.6
EN 1993-1-1 Annex A
14 × 0.996 2 × 1.614 2 ) × 0.043] = 0.900 5 1.136
= 0 .6 ×
1.136 1770 = 0.460 OK 1.50 2010
Calculation of the factors kyy and kzy : k yy = CmyCmLT
μy 1−
N Ed N cr, y
k yy = 0.996 × 1.072 ×
1 C yy
1 0.993 × = 1.120 136 0.977 1− 4406
EN 1993-1-1 Annex A
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
28
of
30
Eurocode Ref
k zy = C myCmLT
Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
wy μz 1 0.6 N wz 1 − Ed Czy N cr, y
k zy = 0.996 × 1.072 ×
1 1.136 0.918 × × 0.6 × = 0.587 136 0.900 1 . 50 1− 4406
Verification with interaction formulae
N Ed + k yy χ y N Rk
γ M1
M y,Ed ≤1 M y,Rk
χ LT
EN 1993-1-1 § 6.3.3 (6.61)
γ M1
136 × 10 349.1 × 106 + 1.120 × = 0.88 < 1 OK 3 11400 × 275 2010 × 10 × 275 0.769 × 0.859 × 1 1
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
3
N Ed + k zy χ z N Rk
γ M1
M y,Ed ≤1 M y,Rk
χ LT
γ M1
136 × 103 349.1 × 106 + 0.587 × = 0.57 < 1 OK 3 11400 × 275 2010 × 10 × 275 0.303 × 0.859 × 1 1
8 Haunch verification For the verification of the haunch, the compression part of the cross-section is considered as alone with a length of buckling about the zz-axis equal to 3.00m (length between the top of column and the first restraint). Maximum forces and moments in the haunch:
NEd = VEd = MEd =
139.2 kN 151.3 kN 755 kNm
(6.62)
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
29
Title
Example: Elastic analysis of a single bay portal frame
Sheet
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
Properties of the whole section:
The calculation of elastic section properties for this case is approximate, ignoring the middle flange. Section area
A = 160.80 cm2
Second moment of area /yy
Iy = 230520 cm4
Second moment of area /zz
Iz = 2141 cm4
Elastic modulus /yy
Wel,y = 4610 cm3
Elastic modulus /zz
Wel,z = 214 cm3
1000 mm
200 mm
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
Properties of the compression part:
Section at the mid-length of the haunch including 1/6th of the web depth A = 44 cm2
Section area Second moment of area /yy
Iy = 554 cm
Second moment of area /zz
Iz =1068 cm4
⇒ iz =
λz =
120 mm
4
1068 = 4.93cm 44
200 mm
L fz 3000 = = 0.704 i z λ1 49.30 × 86.39
Buckling of welded I section with h/b > 2 : ⇒ curve d
[
⇒ α = 0.76
(
)
]
[
]
φz = 0.5 1 + α λ z − 0.2 + λ z = 0.5 × 1 + 0.76 × (0.704 − 0.2 ) + 0.704 2 = 0.939
χz =
2
1 φz + φ − λ 2 z
2 z
=
1 0.939 + 0.9392 − 0.7042
= 0.641
Example: Elastic analysis of a single bay portal frame (GB)
CALCULATION SHEET
Document Ref:
SX029a-EN-GB
Title
Example: Elastic analysis of a single bay portal frame
Sheet
30
of
30
Eurocode Ref Made by
Laurent Narboux
Date
Nov 2006
Checked by
C M King
Date
Dec 2006
Compression in the bottom flange:
N Ed, f = 139.24 ×
4400 755000 × 1000 + × 4400 = 760kN 16080 4610.103 × 1000
Verification of buckling resistance of the bottom flange:
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
N Ed,f 760 × 103 = 0.980 < 1 OK = χ z N Rk 0.641× 4400 × 275
Example: Elastic analysis of a single bay portal frame (GB)
SX029a-EN-UK
Quality Record RESOURCE TITLE
Example: Elastic analysis of a single bay portal frame
Reference(s)
SX029a-EN-GB
Created on Saturday, December 03, 2011 This material is copyright - all rights reserved. Use of this document is subject to the terms and conditions of the Access Steel Licence Agreement
LOCALISED RESOURCE DOCUMENT Name
Company
Date
Created by
Laurent Narboux
SCI
Nov 06
Technical content checked by
Charles King
SCI
Dec 06
Editorial content checked by
D C Iles
SCI
April 2007
Page 31
View more...
Comments