SS-V: 1210 Tangential Stress for a Cylindrical Shell

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


Figure 1.
Boundary Conditions
Edges AB
All translations and rotations are zero
Edge AD and edge BC
Symmetry about rθ plane

Figure 2.
The material properties are:
Young's Modulus
2.1e5 MPa
Poisson's Ratio


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