TALAT Lecture 2301
Design of Members Axial Force Example 5.1 : Axial force resistance of square hollow section 2 pages Advanced Level prepared by Torsten Höglund, Royal Institute of Technology, Stockholm
Date of Issue: 1999 EAA - European Aluminium Association TALAT 2301 – Example 5.1
1
Example 5.1. Axial force resistance of square hollow section
5.4.3
Width
b
70 . mm
6 MPa 10 . Pa
Thickness
t
1.9 . mm
fo
200 . MPa
Column length
L
1000 . mm
E
70000 . MPa
b f = 66.2 mm
bf
β
t
= 34.8
Element classification 250 . MPa
ε
Tab. 5.1
2 .t
b
β 5.4.4
γ M1 1.0
Slenderness parameter bf
kN 1000 . newton
ε = 1.118
fo
β 1 11 . ε β 2 16 . ε
β 1= 12.3 β 2= 17.9
β 3 22 . ε β 3= 24.6 class if β > β 1 , if β > β 2 , if β > β 3 , 4 , 3 , 2 , 1 class = 4 5.4.5
Local buckling
5.4.5 (3) c) heat-treated unwelded
ρ c if
β
22 , 1.0 ,
ε
32
220
β
β
ε
4 .( b
A eff 4
r
b
(b
12
t eff = 1.52 mm
t ) . t eff 2 .t )
ρ c= 0.8
ε
if class 4 , t . ρ ,ct
t eff
I
2
A eff = 414.2 mm
4
2
I = 4.004 . 10 mm 5
12 I
4
According to 5.8.4.1 (1)
r = 31.1 mm
A eff
A .η .f o
λ
N cr
Substitute 5.8.4
Flexural buckling K .L
Table 5.7
K
1
l
Table 5.5 and 5.6
α
0.2
λ o
See to the right
λ
(5.33)
φ φ
5.8.3 (1)
N cr 0.1
k1
1
k2
l. 1 . f o r π E 0.5 . 1
α . λ
λ o
λ
2
TALAT 2301 – Example 5.1
λ 1
χ φ
χ = 0.891 fo .A χ .k 1 .k 2 . eff γ M1
2
l
A ef A
r
φ
2
λ
2
l. 1 . f o r π E
Note: λ with a bar cannot be written
N b.Rd = 73.8 kN
2
η
Result
λ = 0.547
= 0.694
N b.Rd
1
2 π .E .I
I A ef