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
By: Kevin W. Noonan and Gene J. Bingham
Contributors: Bingham, Gene J; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; United States. Army Aviation Research and Development Command; Army Research and Technology Laboratories (U.S.). Structures Laboratory
Series: NASA technical paper -- 1701; AVRADCOM technical report -- 80-B-5
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 82
Subjects: Rotors (Helicopters) -- Testing; Helicopters -- Aerodynamics; Aerofoils -- Testing; Reynolds number
Notes: "Structures Laboratory, AVRADCOM Research and Technology Laboratories."

"U.S. Army AVRADCOM"--Cover

Sept. 1980

Includes bibliographical references