Loads and performance data from a wind-tunnel test of generic model helicopter rotor blades /

Bibliographic Details

Main Author:	Yeager, William T.
Corporate Author:	Langley Research Center
Other Authors:	Wilbur, Matthew L.
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2005]
Series:	NASA technical paper ; 213937.
Subjects:	Rotary wings. Helicopters. Vibratory loads. Rotors. Shafts (Machine elements) Torsion. Radial distribution. Angle of attack.
Online Access:	https://purl.fdlp.gov/GPO/LPS124423