Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0

An edition of Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 (1979)

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0

By Jim A. Penland

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Publish Date

1979

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch

Language

eng

Pages

144

Description:

subjects: Aerodynamics, Aerodynamic characteristics, Computational fluid dynamics, Delta wings, Hypersonic aircraft, Wind tunnel tests