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This test lets you check analysis results for a simply-supported thin square plate, in the context of a transient dynamic response case. You will use 2D meshes. This test is used to validate the following attributes:
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Reference: NAFEMS-Glasgow, Benchmark newsletter, Report No. E1261/R002, p.21, February 1989. |
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Length: |
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Thickness: |
Young Modulus (material): |
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Poisson's Ratio (material): |
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Density: |
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Restraints: Tx = Ty = Rz = 0
at all nodes |
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You will find here the results for different finite elements:
Type of values |
Reference solution |
Values |
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Linear triangle shell |
Parabolic triangle shell |
Linear quadrangle shell |
Parabolic quadrangle shell |
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Values |
Error |
Values |
Error |
Values |
Error |
Values |
Error |
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Peak displacement [mm] |
3.523 |
3.444 |
2.24 |
3.445 |
2.21 |
3.451 |
2.04 |
3.446 |
2.19 |
Peak stress [MPa] |
2.484 |
2.221 |
10.59 |
2.217 |
10.75 |
2.251 |
9.38 |
2.234 |
10.06 |
Static displacement [mm] |
1.817 |
1.774 |
2.37 |
1.775 |
2.31 |
1.776 |
2.26 |
1.775 |
2.31 |
To Perform the Test:
The Transient_forced_vibration_of_a_simply_supported_thin_square_plate.CATAnalysis document presents a complete analysis of this case, computed with a mesh formed of linear quadrangle elements (QD4).
To compute the case with parabolic quadrangle (QD8), linear triangle (TR3) and parabolic triangle (TR6) elements, proceed as follow:
Open the CATAnalysis document.
In the Advanced Meshing Tools workbench, replace the mesh specifications as indicated above.
In the Generative Structural Analysis workbench, compute the case.