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Aerodynamic characteristics of a supersonic cruise airplane configuration at Mach numbers of 2.30, 2.96, and 3.30. [Langley Unitary Plan wind tunnel test

Barrett L. Shrout, R. H. Fournier

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

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Aerodynamic characteristics of a supersonic cruise airplane configuration at Mach numbers of 2.30, 2.96, and 3.30. [Langley Unitary Plan wind tunnel test — Research Paper | ScholarLens