Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip /

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Bibliographic Details
Author / Creator:	Yeager, William T., author.
Imprint:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1997.
Description:	1 online resource (23 pages) : illustrations.
Language:	English
Series:	NASA technical memorandum ; 4754 ARL technical report ; 1283 NASA technical memorandum ; 4754. ARL-TR (Aberdeen Proving Ground, Md.) ; 1283.
Subject:	Rotors. Transonic wind tunnels.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10757515

Hidden Bibliographic Details
Other authors / contributors:	Langley Research Center, issuing body. United States. National Aeronautics and Space Administration, sponsoring body.
Notes:	Title from title screen (viewed on Feb. 19, 2016). "May 1997." "Performing organizations: Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center; Joint Research Program Office, Aeroflightdynamics Directorate, U.S. Army Aviation and Troop Command, NASA Langley Research Center"--Report documentation page. "ATCOM technical report 97-A-006." Includes bibliographical references (page 6). Sponsored by the National Aeronautics and Space Administration WU 05-63-36-02 PR A5008 L- 17558 NASA TM-4754 ARL-TR- 1283 ATCOM TR-97-A-006
Other form:	Print version: Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip Microfiche version: Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip
GPO item no.:	0830-D (online)
Govt.docs classification:	NAS 1.15:4754

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