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We study how the performance of a membrane wing is affected by continuously changing the camber. We do this using a dielectric elastomer actuator as the wing material.

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This page is a summary of: Control of Separated Flow Using Actuated Compliant Membrane Wings, AIAA Journal, September 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058277.
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