Aeroelastic modeling and flutter control in aircraft with low aspect ratio composite wings
A comprehensive study including modeling and control of aeroelastic instabilities in free flying aircraft with flexible wings has been completed. The structural model of the wing consists of a trapezoidal composite plate rigidly attached to a fuselage with rigid-body degrees of freedom. Both quasi-s...
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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/10919/40462 http://scholar.lib.vt.edu/theses/available/etd-12222005-090648/ |