Analysis Type:
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Prestress Modal
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Model Type:
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3D
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Comparison:
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ANSYS
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Reference:
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Timoshenko, S., and Young, D.H. Vibration Problems in Engineering, 3rd Edition. D. Van Nostrand Co., Inc., New York, 1955.
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Description:
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Determine the first three radially symmetric, out of plane, natural frequencies of a circular membrane. Use stiffness calculated from static analysis where membrane is loaded radially. Edges are simply supported.
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Element Type: | plate | |
Units: | IPS | |
Dimensions: | radius: 15 thickness: 0.01 | |
Material Properties: | Mass Density: 0.00073 Cost Per Unit Mass: 0 Young's Modulus: 3e7 | Poisson's Ratio: 0.3 Thermal Expansion: 0 Conductivity: 0 |
Constraints: | edge simply supported | |
Loads: | radial load of 100 lb/in |
Theory | ANSYS | % Difference | Structure | % Difference | |
Mode 1 | 94.406 | 94.471 | 0.07% | 94.442 | 0.03% |
Mode 6 | 216.77 | 217.38 | 0.28% | 216.99 | 0.101% |
Mode 15 | 339.85 | 342.98 | 0.92% | 341.11 | 0.37% |
Convergence %: 1 % on Frequency | Max P: 8 | No. Equations: 994 |
Results are only for radially symmetric modes—modes 1, 6, and 15 of the solution. These are out-of-plane modes, in other words; they appear in the profile view. |