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Tail buffet alleviation of high performance twin tail aircraft using offset piezoceramic stack actuators and acceleration feedback control

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1. http://hdl.handle.net/1853/12499
2. 503506

Identifer	oai:union.ndltd.org:GATECH/oai:smartech.gatech.edu:1853/12499
Date	12 1900
Creators	Bayon De Noyer, Maxime P.
Publisher	Georgia Institute of Technology
Source Sets	Georgia Tech Electronic Thesis and Dissertation Archive
Language	en_US
Detected Language	English
Type	Dissertation
Format	246 bytes, text/html
Rights	Access restricted to authorized Georgia Tech users only.