TY - DATA T1 - 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 PY - 2017/11/09 AU - Deepa Kodali AU - Cory Medina AU - Chang-kwon Kang AU - Hikaru Aono UR - 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 DO - 10.6084/m9.figshare.5585014.v1 L4 - https://ndownloader.figshare.com/files/9711847 KW - animal flight KW - spanwise flexibility KW - aeroelasticity KW - unsteady aerodynamics N2 - 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. ER -