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Investigation of the Effects of Leading-edge Flaps on the Aerodynamic Characteristics in Pitch at Mach Numbers from 0.40 to 0.93 of a Wing-fuselage Configuration with a 45 Degree Sweptback Wing of Aspect Ratio 4

Kenneth P Spreemann, W. J. Alford

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Key concepts: Fuselage, Aerodynamics, Mach number, Wing, Degree (music), Leading edge, Aerospace engineering, Wing configuration

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Investigation of the Effects of Leading-edge Flaps on the Aerodynamic Characteristics in Pitch at Mach Numbers from 0.40 to 0.93 of a Wing-fuselage Configuration with a 45 Degree Sweptback Wing of Aspect Ratio 4 — Research Paper | ScholarLens