Numerical Simulations of the Aeroelastic Response of an Actively Controlled Flexible Wing
A numerical simulation for evaluating methods of predicting and controlling the response of an elastic wing in an airstream is discussed. The technique employed interactively and simultaneously solves for the response in the time domain by considering the air, wing, and controller as elements of a...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/34087 http://scholar.lib.vt.edu/theses/available/etd-072099-103323/ |