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