Figure S2. Normalized wing deformation at various time instants. from Effects of spanwise flexibility on performance of flapping flyers in forward flight
2017-11-09T14:16:28Z (GMT) by
Normalized wing deformation as a function of normalized span length for various time instants with thickness of 0.966 mm, wing density of 2000 kg/m3 and Young's modulus of 5 GPa for the goose model at the optimal AR of 5.3.