Aeroservoelastic analysis, design and wind tunnel testing of a three degree-of-freedom binary flutter model
Aeroelastic problems are typically limiting factors in the performance and flight envelopes of aircraft. Aeroelastic constraints can be relaxed through active control of the flutter modes at and above the uncontrolled flutter speed of aircraft using primary flight control surfaces. To demonstrate...
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| Format: | Others |
| Language: | en |
| Published: |
2012
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| Online Access: | http://hdl.handle.net/10539/11228 |