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A simply supported equilateral triangular plate is subjected to uniformly distributed transversal load. Assuming small deformation theory and neglecting self‑weight, the maximum out‑of‑plane deflection of the plate is determined.
Verification Example 000072 | 1
| Number of Nodes | 3 |
| Number of Lines | 3 |
| Number of Surfaces | 1 |
| Number of Load Cases | 1 |
| Dimensions (Metric) | 1.732 x 2.000 x 0.000 m |
| Dimensions (Imperial) | 5.68 x 6.56 x 0 feet |
| Program Version | 5.06.30 |
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