SS-V: 1210 Tangential Stress for a Cylindrical Shell
Test No. VS22 Find outer surface tangential stress for a cylindrical shell.
Definition
Figure 1.
- Boundary Conditions
- Edges AB
- All translations and rotations are zero
- Edge AD and edge BC
- Symmetry about rθ plane
Figure 2.
- Property
- Value
- Young's Modulus
- 2.1e5 MPa
- Poisson's Ratio
- 0.3
Results
The following table summarizes the stress results.
| Tangential stress at Point E | Reference1 | SimSolid | % Difference |
|---|---|---|---|
| Case 1 | 60 MPa | 59.2 MPa | ~1 |
| Case 2 | 60 MPa | 58.7 MPa | ~2 |
1 Test LE2
from NAFEMS Publication NNB, Rev. 3, NAFEMS Linear Benchmarks, 5 Oct
1990