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