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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

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posted on 2017-11-09, 14:16 authored by Deepa Kodali, Cory Medina, Chang-kwon Kang, Hikaru Aono
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.

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    Journal of the Royal Society Interface

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    animal flightspanwise flexibilityaeroelasticityunsteady aerodynamics

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