From: Aerodynamics and dynamic stability of micro-air-vehicle with four flapping wings in hovering flight
\( {\overline{C}}_L \) | \( {\overline{C}}_D \) | \( {\overline{C}}_P \) | η | |
---|---|---|---|---|
Wing without Clap-and-fling effect | 2.044 | 2.727 | 2.624 | 1.114 |
Wing with Clap-and-fling effect | 2.436 | 3.882 | 3.253 | 1.168 |