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 /

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 /

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Bibliographic Details
Main Author: Noonan, Kevin W.
Corporate Authors: 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
Other Authors: Bingham, Gene J.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1980.
Series:AVRADCOM technical report ; 80-B-5.
NASA technical paper ; 1701.
Subjects:
Rotors (Helicopters) > Testing.
Helicopters > Aerodynamics.
Aerofoils > Testing.
Reynolds number.

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Call Number: NAS 1.60:1701
 
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NAS 1.60:1701 Available