Coupled Aeroelastic Study of a Flexible Micro Air Vehicle-Scale Flapping Wing in Hovering Flight

Authors :: Inderjit Chopra
James Lankford
Source :: Journal of Aircraft. 59:154-172
Publication Year :: 2022
Publisher :: American Institute of Aeronautics and Astronautics (AIAA), 2022.
Abstract: Instantaneous force and structural deformation experiments were performed on a flexible, structurally characterized, low-aspect-ratio representative flapping wing. A six-component force balance was...

Subjects :: Physics
Scale (ratio)
business.industry
Aerospace Engineering
Micro air vehicle
Multibody system
Aerospace engineering
Force balance
Aeroelasticity
business
Reynolds-averaged Navier–Stokes equations
Vortex
Flapping wing

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