http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip
National Aeronautics and Space Administration,
1 online resource (23 pages) : illustrations.
William T. Yeager, Jr. [and four others].
Title from title screen (viewed on Feb. 19, 2016).
"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."
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
ARL-TR (Aberdeen Proving Ground, Md.) ; 1283