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Experimental study of a method of designing the sweptback-wing-fuselage juncture to reduce the drag at moderate supersonic speeds

R. R. Howell

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Key concepts: Juncture, Fuselage, Drag, Supersonic speed, Wing, Aerodynamics, Structural engineering, Engineering

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Experimental study of a method of designing the sweptback-wing-fuselage juncture to reduce the drag at moderate supersonic speeds — Research Paper | ScholarLens