Benchmark 38: Access Steel Document SX022a-EN-EU
Project file: Benchmark_(EC_EN_1993)_38.esa
SCIA Engineer Version R18.1
Introduction
This benchmark concerns the example SX022a-EN-EU Calculation of effective section properties for a cold-formed lipped channel section in bending of Access Steel, http://www.access-steel.com/, 2005.
This example deals with the effective properties calculation of a cold formed lipped channel section subjected to bending about its major axis.
Reference Results
The reference gives following results:
Local Buckling calculation | |||||||
Part |
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Flange | 72 | 4,0 | 0,789 | 0,914 | 65,8 | 32,9 | 32,9 |
Edge fold | 19,8 | 0,5 | 0,614 | 1,00 | 19,8 |
Distortional Buckling calculation - Iteration 1 | |
As | 103,3 mm² |
Is | 3663 mm^4 |
b1 | 61,73 mm |
hw | 198 mm |
kf | 0 |
K | 0,439 N/mm^2 |
σcr | 355,78 N/mm^2 |
|
0,992 |
χd | 0,753 |
Distortional Buckling calculation - Iteration n | |
be1 | 32,9 mm |
be2,n | 35,9 mm |
ceff,n | 19,8 mm |
χd,n | 0,737 |
Local Buckling calculation | |||||||
Part |
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Web | 198 | 22,58 | 0,914 | 0,959 | 97,5 | 39 | 58,5 |
Effective section properties |
|
Aeff | 689,2 mm² |
Ieff,y | 4140000 mm^4 |
Weff,y,c | 40460 mm^3 |
Weff,y,t | 43260 mm^3 |
SCIA Engineer Results
Result for the initial calculation i.e. without stiffener iterations:
Result using stiffener iterations:
Comments
- The results correspond to the benchmark results.
- The reference ignores the fact that the principal axis is not parallel to the flanges (alfa = -1,47 deg). As a result, the top flange is not in uniform compression but subject to a stress gradient. SCIA Engineer accounts for the actual stress distribution leading to small differences in the results.
- The reference does not detail the calculation of b2.
- The reference does not detail the different stiffener iteration steps.