An aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation / W. Keats Wilkie, K.C. Park.

Author/creator Wilkie, W. Keats author.
Format Electronic
PublicationHampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1996.
Description1 online resource (iv, 58 pages) : illustrations.
Supplemental Contenthttps://purl.fdlp.gov/GPO/gpo67751

Other author/creatorPark, K. C., author.
Other author/creatorU.S. Army Research Laboratory.
Other author/creatorLangley Research Center, issuing body.
Other author/creatorUnited States. National Aeronautics and Space Administration sponsoring body.
SeriesNASA technical memorandum ; 110252
NASA technical memorandum 110252. ^A467613
General noteTitle from title screen (viewed June 21, 2016).
General note"May 1996."
General note"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.
General note"ARL-MR-328."
General noteGPO Cataloging Record Distribution Program (CRDP).
Bibliography noteIncludes bibliographical references (pages 22-24).
Funding informationSponsored by the National Aeronautics and Space Administration 505-63-36-02
Issued in other formMicrofiche version: Wilkie, W. Keats. Aeroelastic analysis of helicopter rotor blades incorporating piezoelectric fiber composite twist actuation
GPO item number0830-D (online)
Govt. docs number NAS 1.15:110252

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