OS-V: 0350 Simply-Supported Thin Square Plate Periodic Forced Vibration Response
Test 13P OptiStruct is used to investigate the Peak Displacement in z-direction and extreme fiber bending stress at the center of the plate.

図 1. FE Model with Boundary Conditions and Loadcases
Benchmark Model
The 2nd order and 1st order quad elements are used to model the square plate of thickness 0.05m. The z-rotation and x, y translations are fixed for all the nodes, z-translation is fixed along all four edges, x-rotation is fixed along the edge x=0 and x=10 and y-rotation is fixed along the edge y=0 and y=10. A steady-state harmonic forced vibration F=F0 (sin ωt-sin 3ωt) is induced in the z-direction. (F0=100 N/m2 over whole plate, ω=2πf, f=1.2 Hz). For modal analysis solution, a damping ratio of 0.02 is applied in all 16 modes and for direct solution, Rayleigh damping factor α1=0.299 and α2=1.339×10-3 are given.
- Material Properties
- Value
- Young’s Modulus
- 200 × 109 N/m2
- Poisson’s Ratio
- 0.3
- Density
- 8000 kg/m3
Frequency Response Summary
f*
- Closed form solution
Peak Displacement (mm) | Peak Stress (N/mm2) | |
---|---|---|
Reference Solution | 2.863 | 2.018 |
HOE: | ||
Direct Solution | 2.928 | 2.418 |
Normalized | 0.977800546 | 0.834574028 |
Modal Solution | 2.929 | 2.426 |
Normalized | 0.977466712 | 0.831821929 |
LOE: | ||
Direct Solution | 2.825 | 1.956 |
Normalized | 1.013451327 | 1.031697342 |
Modal Solution | 2.826 | 1.961 |
Normalized | 1.013092711 | 1.029066803 |
Model Files
必要なモデルファイルのダウンロードについては、モデルファイルへのアクセスを参照してください。
- Test13PHOED.fem
- Test13PHOEM.fem
- Test13PLOED.fem
- Test13PLOEM.fem
Reference
NAFEMS R0016 - Selected Benchmarks for Forced Vibration, J Maguire, D J, Dawswell, L Gould 1989