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2025-09-16

Cross-Section Resistance Design and Stability Analysis According to DIN EN 1993-1-3:2010-12

Description

The example shows the cross-section resistance design and stability analysis according to DIN EN 1993-1-3:2010-12 [1] for a frame column.
The column is designed as a simply supported beam in the z-direction. It is laterally supported in the y-direction at one-third of the column height. In addition, rotation about the x-axis is prevented in the column center.
The cross-section consists of two C-sections arranged back-to-back and connected by pairs of bolts in the web area. The connection is designed in such a way that local buckling across the entire web width is not prevented.
The column is subjected to an axial compressive force and three lateral loads.
The model is based on Example L from the design examples in ECCS-TC7 [2].

Material Modulus of elasticity E 210,000.00 N/mm²
Poisson's ratio ν 0.30
Shear modulus G 80,769.23 N/mm²
Basic yield strength S350GD fyb 350.00 N/mm²
Partial safety factor for the cross-section resistance γM0 1.00
Partial safety factor for the component resistance against stability failure γM1 1.00
Geometry System Column height L 8,000.00 mm
Distance of the load application from the base xF1 2,000.00 mm
Distance of the load application from the base xF2 4,000.00 mm
Distance of the load application from the base xF3 6,000.00 mm
Length of the rigid load application ss 64.00 mm
Cross-Section Height h 250.00 mm
Width of the partial cross-section b1 80.00 mm
Thickness t 2.50 mm
Inner radius ri 5.00 mm
Stiffening height c 40.00 mm
Loads Compressive force Nd 40.00 kN
Transverse load Fd 8.00 kN

RFEM Settings

Modeled in RFEM 6.11.0011
First-order analysis
Isotropic linear-elastic material model

Results

Reference Value ECCS RFEM 6 Deviation
Shear resistance according to 6.1.5
Shear load-bearing capacity Vb,Rd 150.90 kN 150.90 kN 0.00 %
Utilization η 0.08 0.08 0.00 %
Local load introduction according to 6.1.7
Cross-section resistance for local load introduction Rw,Rd 59.24 kN 59.24 kN 0.00 %
Utilization η 0.14 0.14 0.00 %
Combined stress from compression and bending according to 6.1.9
Limit compressive force Nc,Rd 551.00 kN 518.21 kN 5.95 %
Utilization η 0.61 0.61 0.00 %
Combined stress from bending and local load introduction or support reaction according to 6.1.11
Moment resistance Mc,Rd 59.94 kNm 59.93 kNm 0.02 %
Utilization η according to (6.28c) 0.54 0.54 0.00 %
Flexural buckling about y-axis according to 6.2.2
Elastic critical buckling load Ncr,y 700.14 kN 700.10 kN 0.01 %
Load-bearing capacity for flexural buckling Nb,y,Rd 409.04 kN 393.57 kN 3.78 %
Flexural buckling about z-axis according to 6.2.2
Elastic critical buckling load Ncr,z 2001.65 kN 2001.63 kN 0.00 %
Load-bearing capacity for flexural buckling Nb,z,Rd 481.10 kN - - 1)
Torsional buckling and lateral-torsional buckling according to 6.2.3
Elastic critical buckling load Ncr,T 924.29 kN 939.24 kN 1.62 %
Load-bearing capacity for torsional buckling or lateral-torsional buckling Nb,T,Rd 408.57 kN 393.33 kN 3.73 %
Bending and centric compressive force according to 6.2.5
Ideal elastic critical moment for lateral-torsional buckling Mcr for destabilizing effect of transverse loads 133.18 kNm 222.07 kNm 66.74 % 2)
Utilization η 0.81 0.77 4.93 %

1) The load-bearing capacity for flexural buckling is not calculated, as the flexural buckling design may be omitted according to EN 1993-1-1, 6.3.1.2(4).
2) The ideal elastic critical moment for lateral-torsional buckling is calculated in [2&# 93; is calculated for a simplified structural system according to ENV 1993-1-1:1992, Appendix F, Table F.1.1. In RFEM, however, the calculation is performed using an eigenvalue analysis on the real structural system, which results in a higher ideal elastic critical moment for lateral-torsional buckling.


References


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