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

An edition of Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 (1980)

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

By Jimmy L. Pittman

0 (0 Ratings)

0 Want to read0 Currently reading0 Have read

Publish Date

1980

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch,For sale by the National Technical Information Service]

Language

eng

Pages

113

Description:

subjects: Aerodynamics, Supersonic, Hypersonic planes, Mach number, Supersonic Aerodynamics, Supersonic wind tunnels