# SS-V: 1210 Tangential Stress for a Cylindrical Shell

Test No. VS22 Find outer surface tangential stress for a cylindrical shell.

## Definition

**Boundary Conditions**- Edges AB
- All translations and rotations are zero
- Edge AD and edge BC
- Symmetry about rθ plane

**Property****Value**- Young's Modulus
- 2.1e5 MPa
- Poisson's Ratio
- 0.3

## Results

Tangential stress at Point E | Reference^{1} |
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