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

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bayondenoyer_maxime_p_199912_phd_503506.pdf (48.24 MB)
Author(s)
Bayon De Noyer, Maxime P.
Advisor(s)
Editor(s)
Associated Organization(s)
Organizational Unit
Organizational Unit
Daniel Guggenheim School of Aerospace Engineering
The Daniel Guggenheim School of Aeronautics was established in 1931, with a name change in 1962 to the School of Aerospace Engineering
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Series
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Theses and Dissertations
Supplementary to:
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http://hdl.handle.net/1853/12499
Abstract
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Date
1999-12
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246 bytes
Resource Type
Text
Resource Subtype
Dissertation
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