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