Calculate the tangential stress at point E of the cylindrical shell
under uniform normal pressure of 0.6 MPa and tangential normal pressure of 60 MPa on edge
DC.
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File Name
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Open drive
letter:\Users\Public\Public Documents\SOLIDWORKS\SOLIDWORKS
version\samples\Simulation
Examples\Verification\NAFEMS_IC22.SLDPRT.
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Mesh Type
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Shell mesh. Shell thickness = 0.01 m - Thin shell formulation
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Material Properties
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- Modulus of elasticity =
210 X 103 MPa
- Poisson's ratio (ν) =
0.3
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Results
| Component |
Reference |
SOLIDWORKS Simulation |
| Tangential SY stress (Reference Axis 1) at
point E (MPa) |
60.0 |
59.85 |
Reference
NAFEMS Publication P07, The International Association
for the Engineering Analysis Community, "Linear Statics Benchmarks VOL. 1", D. Hitchings,
A.Kamoulakos, G.A. Davies, VOL. 1, October, 1987.