Numerical simulations of subsonic aeroelastic behavior and flutter suppression by active control
<p>A method for predicting the unsteady, subsonic, aeroservoelastic response of a wing has been developed. The air, wing, and control surface are considered to be a single dynamical system. All equations are solved simultaneously in the time domain by a predictor-corrector method. The scheme a...
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| Format: | Others |
| Language: | en |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/41681 http://scholar.lib.vt.edu/theses/available/etd-03172010-020348/ |