Aerodynamic characteristics of a hypersonic research airplane concept having a 70ê swept double-delta wing at Mach number 0.2 View on Open Library

Aerodynamic characteristics of a hypersonic research airplane concept having a 70ê swept double-delta wing at Mach number 0.2

by Jim A Penland

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First published: 1978 1 language
Subjects
Aerodynamics, Supersonic Hypersonic planes Lift (Aerodynamics) Stability of airplanes Supersonic Aerodynamics

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