From: Aerodynamics and dynamic stability of micro-air-vehicle with four flapping wings in hovering flight
d | C̄L | C̄D | C̄P | η |
---|---|---|---|---|
0.28c | 2.503 | 4.074 | 3.310 | 1.196 |
0.43c | 2.193 | 3.444 | 2.967 | 1.095 |
1.73c | 2.047 | 2.799 | 2.647 | 1.106 |
Without Clap-and-fling effect | 2.044 | 2.727 | 2.624 | 1.114 |