Rotating shake test and modal analysis of a model helicopter rotor blade /

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Bibliographic Details
Author / Creator:	Wilkie, W. Keats, author.
Imprint:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 1997.
Description:	1 online resource (15 pages.) : illustrations.
Language:	English
Series:	NASA technical memorandum ; 4760 NASA technical memorandum ; 4760.
Subject:	Aeroelasticity. Helicopters. Torsion.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10758181

Hidden Bibliographic Details
Other authors / contributors:	Mirick, Paul H., author. Langston, Chester W., author. Vehicle Technology Center (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 on Feb. 18, 2016). "June 1997." "Performing organizations: NASA Langley Research Center, Hampton, VA [and] Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center, Hampton, VA"--Report documentation page. "ARL technical report 1389." Includes bibliographical references (page 15). Sponsored by the National Aeronautics and Space Administration WU 505-63-36-02 A5008 L-17352
Other form:	Print version: Rotating shake test and modal analysis of a model helicopter rotor blade Microfiche version: Wilkie, W. Keats. Rotating shake test and modal analysis of a model helicopter rotor blade
GPO item no.:	0830-D (online)
Govt.docs classification:	NAS 1.15:4760

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