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Contributions of Wing, Tail, and Fuselage to the Aerodynamic Characteristics of a Semispan Model of a Supersonic Airplane Configuration at Transonic Speeds from Tests by the NACA Wing-flow Method

Norman S Silsby, James M Mckay

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Key concepts: Fuselage, Airplane, Wing, Transonic, Aerodynamics, Supersonic speed, Aerospace engineering, Wing configuration

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Contributions of Wing, Tail, and Fuselage to the Aerodynamic Characteristics of a Semispan Model of a Supersonic Airplane Configuration at Transonic Speeds from Tests by the NACA Wing-flow Method — Research Paper | ScholarLens