OS-V: 0500 Laminated Strip
Test No. R0031/1 OptiStruct examines the bending stress at E, Interlaminar shear stress at D and the z-deflection at E for linear static analysis.
図 1. FE Model with Boundary Conditions and Loadcases
Benchmark Model
Quad4 and Hexa8 elements are used to create one quarter model of the laminated strip simply supported at A. For Quad4 elements Ply laminates are created and for Hexa8 elements PSOLID property is used. A line load of 10N/mm is applied at C.
The material properties for the laminated strip are:
- Property
- Value
- E1
- 1.0 × 105 MPa
- 12
- 0.4
- 23
- 0.3
- E2
- 5.0 × 103 MPa
- G12
- 3.0 × 103 MPa
- G13 = G23
- 2.0 × 103 MPa
- 12/E1
- 21/E2
Linear Static Analysis Results
| Target | OptiStruct Results | Normalized with the Target Value | |
|---|---|---|---|
| Laminated Plate (Quad4): | |||
| Bending Stress at E (MPa) | 683.9 | 570.196 | 1.19941213 |
| Interlaminar Shear Stress at D (MPa) | -4.1 | -4.103 | 0.99926883 |
| Z deflection at E (mm) | -1.06 | -1.045 | 1.01435407 |
| Stacked Brick (Hex8): | |||
| Bending Stress at E (MPa) | 683.9 | 572.81 | 1.19393865 |
| Interlaminar Shear Stress at D (MPa) | -4.1 | -3.229 | 1.26974295 |
| Z deflection at E (mm) | -1.06 | -1.028 | 1.0311284 |
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。
The model files used in this problem include:
- complsq4.fem
- complsh8.fem
Reference
NAFEMS R0031 - Composite Benchmarks, Hardy 2001