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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