Cover Image

Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /

Bibliographic Details
Main Authors: Pittman, Jimmy L. (Author), Riebe, Gregory D. (Author)
Corporate Author: Langley Research Center
Format: Government Document eBook
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Series:NASA technical paper ; 1767.
Subjects:
Aerodynamic characteristics.
Aerodynamic configurations.
Angle of attack.
Hypersonic aircraft.
Supersonic aircraft.
Online Access:https://purl.fdlp.gov/GPO/gpo71373
Description
Item Description:Title from title screen (viewed on Aug. 19, 2016).
"December 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Physical Description:1 online resource (113 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 14-15).