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Table 1 Grid-independence test parameters

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

Mesh Grid number Far field size (c) Time step (T) \( {\overline{C}}_L \) \( {\overline{C}}_D \)
Mesh1 220,000 20 0.005 2.375 3.782
Mesh2 360,000 20 0.005 2.435 3.882
Mesh3 650,000 20 0.005 2.460 3.858