Cover Image

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

Bibliographic Details
Main Author: Yeager, William T. (Author)
Corporate Author: United States. National Aeronautics and Space Administration (sponsoring body.)
Format: Government Document eBook
Language:English
Published: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1997.
Series:NASA technical memorandum ; 4754.
ARL-TR (Aberdeen Proving Ground, Md.) ; 1283.
Subjects:
Rotary wings.
Vibratory loads.
Transonic wind tunnels.
Paddles.
Rotors.
Online Access:https://purl.fdlp.gov/GPO/gpo65467
Description
Item Description: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."
Physical Description:1 online resource (23 pages) : illustrations.
Bibliography:Includes bibliographical references (page 6).