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Rectangular Plate Bending – Pinned at Edges

Model Details and Parameters

The purpose of this test case is to validate the plate/shell element solver in SkyCiv Structural 3D (S3D). The results were compared against a third-party analysis software. In this test case the following model parameters were used:

  • Analysis Type: Linear Static
  • Material: Structural Steel
  • Young’s Modulus: 200,000 MPa
  • Poisson’s Ratio: 0.27
  • Plate Type: Mindlin Plane Stress
  • Plate Size: 2m x 1m
  • Plate Thickness: 10 mm
  • Edge Boundary Supports: FFFRRR (3D Pin)
  • Pressure Load: 1 kPa normal to plate

pinned-at-edges-model

Results – 8×4 Structured Mesh

Result Location SkyCiv Third-Party 1 Difference 1 Third-Party 2 Difference 2
Max Displacement Z (mm) Node 25 (center of plate) -0.54879 -0.56405 -2.71% -0.54879 0.00%
Max Von Mises Stress – Element (MPa) Element 20 Top 4.63425 4.82904 -4.03% 4.63432 0.00%
Reaction Z (kN) Node 21 0.12649 0.12961 -2.41% 0.12649 0.00%
Max Shear Force XZ – Element (kN/m) Element 28 0.29475 0.33767 -12.71% 0.29475 0.00%

Results – 16×8 Structured Mesh

Result Location SkyCiv Third-Party 1 Difference 1 Third-Party 2 Difference 2
Max Displacement Z (mm) Node 120 (center of plate) -0.55999 -0.56542 -0.96% -0.55999 0.00%
Max Von Mises Stress – Element (MPa) Element 72 Top 5.11488 5.17574 -1.18% 5.11487 0.00%
Reaction Z (kN) Node 71 0.06218 0.06307 -1.41% 0.06218 0.00%
Max Shear Force XZ – Element (kN/m) Element 120 0.35126 0.40086 -12.37% 0.35125 0.00%

Results – Unstructured Mesh

Result Location SkyCiv Third-Party 1 Difference 1 Third-Party 2 Difference 2
Max Displacement Z (mm) Node 182 (center of plate) -0.55988 -0.56293 -0.54% -0.55932 0.10%
Max Von Mises Stress – Element (MPa) Element 170 Top 5.22850 5.25876 -0.58% 5.22487 0.07%
Reaction Z (kN) Node 59 0.04218 0.04217 0.02% 0.04214 0.09%
Max Shear Force XZ – Element (kN/m) Element 62 0.44973 0.49276 -8.73% 0.45013 -0.09%

Extra Considerations

  • This verification model was created and checked on 28 February 2020. Since this date, the plate solver and S3D software may have been further improved to achieved greater accuracy.
  • Plates are not exact elements like beam and frame elements and therefore the mesh plays a huge role in the results. Always try to use a structured mesh when it is possible to do so.
  • Results between software will never be exactly the same since different elements are used and the nature of plates are approximate
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