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

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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