Buckling of a Beam Frame

A two-beam frame is loaded with a concentrated vertical load at point A. Determine the response of the frame under buckling at the location of the applied load.

File Name

Open drive letter:\Users\Public\Public Documents\SOLIDWORKS\SOLIDWORKS version\samples\Simulation Examples\Verification\NAFEMS_GNL7.SLDPRT.

Study Type

Nonlinear static with large displacement formulation and arc-length option.

Mesh Type

Beam mesh

Restraints

Joints B and C are simply supported. All joints are restrained for out-of-plane translation and rotations.

Material Properties

  • Elasticity modulus (E) = 71.74 x 109 N/m2
  • Poisson's ratio (ν) = 0
  • Mass density (ρ)= 8200 Kg/m3

Loads

Load P = 20000 N is applied incrementally using the arc-length option with automatic adjustment of arc length.

Results

Define a Workflow Sensitive sensor at the target location A, and use the Define Time History Plot tool to plot the graph for the vertical displacement component Uy versus the Load factor.
Scale the graph's axes such that:
  • The X-axis shows the Uy/L, where Uy is the vertical displacement and L is the length of each bar equal to 1.2 m.
  • The Y-axis shows the Load factor * PL2/EI, where PL2/EI = 20.072

The Load factor-deflection curve agrees with the finite element solution provided in the reference.

  Deformation ratio (Uy/L) at Point A
Load Factor (PL2/EI) Reference SOLIDWORKS Simulation
18.552 0.407 0.405
31.887 0.784 0.781

Reference

NAFEMS Non-Linear Benchmarks, The International Association for the Engineering Analysis Community, Glasgow, Oct. 1989, Rev.1, Test No NL7.