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Effects of a fuselage flap dive brake on the aerodynamic characteristics of 1/30 scale semispan model of the Bell X-5 variable-sweep airplane at a Mach number 1.24 as determined by the NACA wing flow method

Robert M. Kennedy

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Key concepts: Fuselage, Airplane, Mach number, Aerodynamics, Aerospace engineering, Scale (ratio), Brake, Aeronautics

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Effects of a fuselage flap dive brake on the aerodynamic characteristics of 1/30 scale semispan model of the Bell X-5 variable-sweep airplane at a Mach number 1.24 as determined by the NACA wing flow method — Research Paper | ScholarLens