Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /

Bibliographic Details
Main Authors:	Noonan, Kevin W. (Author), Bingham, Gene J. (Author)
Corporate Authors:	Langley Research Center, United States. Army Aviation Research and Development Command, Army Research and Technology Laboratories (U.S.). Structures Laboratory
Format:	Government Document eBook
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980.
Series:	NASA technical paper ; 1701. AVRADCOM technical report ; 80-B-5.
Subjects:	Aerodynamic characteristics. Airfoils. Helicopters. Reynolds number. Wind tunnel tests. Aerofoils > Testing. Helicopters > Aerodynamics. Rotors (Helicopters) > Testing.
Online Access:	https://purl.fdlp.gov/GPO/gpo71094

Available Online