Cover Image

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
Description
Item Description:Title from title screen (viewed on Aug. 16, 2016).
"September 1980."
"Performing Organization: NASA Langley Research Center and Structures Laboratory, AVRADCOM Research and Technolocy Laboratories"--Report documentation page.
Physical Description:1 online resource (82 pages) : chiefly illustrations.
Bibliography:Includes bibliographical references (page 13).