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
Deepa Kodali
Cory Medina
Chang-kwon Kang
Hikaru Aono
10.6084/m9.figshare.5585014.v1
https://rs.figshare.com/articles/figure/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/5585014
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.
2017-11-09 14:16:18
animal flight
spanwise flexibility
aeroelasticity
unsteady aerodynamics