Table 3 Details of the computational domain and mesh
From: Effects of aspect ratio and inclination angle on aerodynamic loads of a flat plate
Aspect Ratio | Inclination angle (α°) | Upstream length (m) | Downstream length (m) | Transverse direction length (m) from the plate in each side | Number of cells |
|---|---|---|---|---|---|
0.5 | 30, 60, 90 | 0.375 | 1.5 | 0.375 | 4,710,000 |
2 | 30, 60, 90 | 1.5 | 6 | 1.5 | 6,368,250 |
5 | 30, 60, 90 | 3.75 | 15 | 3.75 | 7,505,050 |