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Aerodynamic characteristics of a fixed arrow-wing supersonic cruise aircraft at Mach numbers of 2.30, 2.70, and 2.95. [Langley Unitary Plan wind tunnel tests

O. A. Morris, D. E. Fuller, Carolyn Watson

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Key concepts: Cruise, Mach number, Supersonic speed, Aerodynamics, Aerospace engineering, Supersonic wind tunnel, Wind tunnel, Aeronautics

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Aerodynamic characteristics of a fixed arrow-wing supersonic cruise aircraft at Mach numbers of 2.30, 2.70, and 2.95. [Langley Unitary Plan wind tunnel tests — Research Paper | ScholarLens