Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0

An edition of Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 (1993)

Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0

By Ira J. Walker

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Publish Date

1993

Publisher

National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,National Technical Information Service, distributor]

Language

eng

Pages

Description:

subjects: Stabilizers (Fluid dynamics), Canard configurations, Hypersonics, Aerodynamic characteristics, Delta wings, Wind tunnel tests, Research vehicles, Mach number, Hypersonic vehicles, Tail assemblies