Table 2 Aerodynamic coefficient comparison between symmetric and full model
From: Aerodynamics and dynamic stability of micro-air-vehicle with four flapping wings in hovering flight
Model | \( {\overline{C}}_L \) | \( {\overline{C}}_D \) |
|---|---|---|
Symmetric model | 2.435 | 3.882 |
Full model | 2.424 | 3.829 |