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Flight Measurements with the Douglas D-558-II (buaero No. 37974) Research Airplane : Measurements of the Distribution of the Aerodynamic Load Among the Wing, Fuselage, and Horizontal Tail at Mach Numbers up to 0.87

John P Mayer, George M Valentine

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Key concepts: Fuselage, Airplane, Aerodynamics, Mach number, Wing, Aerospace engineering, Wing loading, Aeronautics

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Flight Measurements with the Douglas D-558-II (buaero No. 37974) Research Airplane : Measurements of the Distribution of the Aerodynamic Load Among the Wing, Fuselage, and Horizontal Tail at Mach Numbers up to 0.87 — Research Paper | ScholarLens