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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