Table 1 Grid-independence test parameters
From: Aerodynamics and dynamic stability of micro-air-vehicle with four flapping wings in hovering flight
Mesh | Grid number | Far field size (c) | Time step (T) | \( {\overline{C}}_L \) | \( {\overline{C}}_D \) |
|---|---|---|---|---|---|
Mesh1 | 220,000 | 20 | 0.005 | 2.375 | 3.782 |
Mesh2 | 360,000 | 20 | 0.005 | 2.435 | 3.882 |
Mesh3 | 650,000 | 20 | 0.005 | 2.460 | 3.858 |