Table 3 Mesh parameters of Calculate model.
From: Thermal modal analysis of hypersonic composite wing on transient aerodynamic heating
Case | Number of mesh (million) | The first layer height (m) | Calculated value (K) |
|---|---|---|---|
Case1 | 0.83 | 5 \(\times\) 10–7 | 1563.2 |
Case2 | 1.22 | 5 \(\times\) 10–7 | 1587.4 |
Case3 | 1.50 | 5 \(\times\) 10–7 | 1596.9 |
Case4 | 1.74 | 5 \(\times\) 10–7 | 1605.6 |
Case5 | 2.01 | 5 \(\times\) 10–7 | 1611.8 |
