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Calculation of three-dimensional unsteady transonic flows past helicopter blades /

Bibliographic Details
Main Author: Chattot, J. J. (Author)
Corporate Authors: Ames Research Center, Aeromechanics Laboratory, United States. Army Aviation Research and Development Command
Format: Government Document eBook
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1980.
Series:NASA technical paper ; 1721.
AVRADCOM technical report ; 80-A-2.
Subjects:
Difference equations.
Finite difference theory.
Helicopter design.
Rotor aerodynamics.
Transonic flow.
Helicopters > Aerodynamics.
Rotors (Helicopters) > Aerodynamics.
Unsteady flow (Aerodynamics)
Online Access:https://purl.fdlp.gov/GPO/gpo71128

Internet

https://purl.fdlp.gov/GPO/gpo71128

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Call Number: NAS 1.60:1721
 
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NAS 1.60:1721 Available