Aerodynamic Characteristics at Mach Numbers 2.30, 2.60, and 2.96 of a Supersonic Transport Model Having a Fixed, Warped Wing

Aerodynamic Characteristics at Mach Numbers 2.30, 2.60, and 2.96 of a Supersonic Transport Model Having a Fixed, Warped Wing
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Total Pages: 68
Release: 1965
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Categories: Aerodynamics, Transonic
Type: BOOK - Published: 1966 - Publisher:

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