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A Study of the Flow over a 45 Degree Sweptback Wing-fuselage Combination at Transonic Mach Numbers

R. T. Whitcomb, Homas C Kelly

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Key concepts: Transonic, Fuselage, Mach number, Wing, Flow (mathematics), Aeronautics, Degree (music), Aerospace engineering

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A Study of the Flow over a 45 Degree Sweptback Wing-fuselage Combination at Transonic Mach Numbers — Research Paper | ScholarLens