Figure S3. Aeroelastic response of the goose model with noticeable second order mode effects. from Effects of spanwise flexibility on performance of flapping flyers in forward flight
2017-11-09T14:16:18Z (GMT) by
Aeroelastic response of the goose model with thickness of 0.966 mm, wing density of 2000 kg/m3 and Young's modulus of 5 GPa for the goose model.