An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation /

An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation /

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Bibliographic Details
Author / Creator:Wilkie, W. Keats., author.
Imprint:Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1996.
Description:1 online resource (iv, 58 pages) : illustrations.
Language:English
Series:NASA technical memorandum ; 110252
NASA technical memorandum ; 110252.
Subject:
Aeroelasticity.
Differential equations.
Fibrous composites.
Helicopters.
Numerical integration.
Unsteady flow (Aerodynamics)
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10912984
Hidden Bibliographic Details
Other authors / contributors:Park, K. C., author.
U.S. Army Research Laboratory.
Langley Research Center, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.
Notes:Title from title screen (viewed June 21, 2016).
"May 1996."
"Performing organization: NASA Langley Research Center, Hampton, VA and Vehicle Structures Directorate, U.S. Army Research Laboratory, NASA Langley Research Center, Hampton,VA"--Report documentation page.
"ARL-MR-328."
Includes bibliographical references (pages 22-24).
Sponsored by the National Aeronautics and Space Administration 505-63-36-02
Other form:Microfiche version: Wilkie, W. Keats. Aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:110252

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