Figure S2. Normalized wing deformation at various time instants. 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.5585023.v1
https://rs.figshare.com/articles/figure/Figure_S2_Normalized_wing_deformation_at_various_time_instants_from_Effects_of_spanwise_flexibility_on_performance_of_flapping_flyers_in_forward_flight/5585023
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.
2017-11-09 14:16:28
animal flight
spanwise flexibility
aeroelasticity
unsteady aerodynamics