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A flight investigation of the transonic area rule for a 52.5 degree sweptback wing-body configuration at Mach numbers between 0.8 and 1.6

Sherwood Hoffman

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Key concepts: Transonic, Wing, Degree (music), Mach number, Aerospace engineering, Aerodynamics, Mechanics, Physics

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A flight investigation of the transonic area rule for a 52.5 degree sweptback wing-body configuration at Mach numbers between 0.8 and 1.6 — Research Paper | ScholarLens