Cover Image

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
Description
Item Description:Title from title screen (viewed on Aug. 16, 2016).
"October 1980."
"Performing Organization: NASA Ames Research Center and Aeromechanics Laboratory AVRADCOM Research and Technology Laboratories"--Report documentation page.
Physical Description:1 online resource (29 pages) : illustrations.
Bibliography:Includes bibliographical references (page 19).