OS-V: 0040 Z-Section Cantilever

Test No. LE5 OptiStruct examines the axial (x-x) stress (compression) at mid-surface, point A for linear static analysis.



Figure 1.

Benchmark Model

Quad4 and Quad8 elements are used to create a uniform mesh of 8 elements along the length with one element across width of flange. All the displacements at one end are maintained zero, at the other end two uniformly distributed force of 0.6MN each are applied.

The material properties are:
Young's Modulus
210 x 103 MPa
Poisson's Ratio
0.3

Linear Static Analysis Results

All results are normalized with the target value (-108 MPa Compression).
Quadrilateral Shells Axial Stress (x-x) at Mid-surface Point A (MPa) Normalized with the Target Value
Quad4 -112.2 0.962566845
Quad8 -110.9 0.973850316

Model Files

The model files used in this problem include:

<install_directory>/hwsolvers/demos/optistruct/verification
  • /LE5Quad4.fem
  • /LE5Quad8.fem

Reference

NAFEMS Ltd, The Standard NAFEMS BENCHMARKS TNSB Rev. 3, NAFEMS Ltd, Scottish Enterprise Technology Park, Whitworth Building, East Kilbride, Glasgow, United Kingdom, 1990.