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Table 4 Averaged aerodynamic coefficient and power coefficient under different wing root spacing

From: Aerodynamics and dynamic stability of micro-air-vehicle with four flapping wings in hovering flight

d

L

D

P

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