Table 2 Comparison of the critical uniform axial buckling stress for different elements.
Name | Nigenvalue | Critical uniform axial buckling stress (MPa) |
|---|---|---|
Classical solution | 199.64 | 6.36 × 103 |
Shell element | 191.78 | 6.11 × 103 |
Solid element (One-layer grid) | 20.033 | 0.64 × 103 |
Solid element (Five-layer grid) | 192.86 | 6.14 × 103 |