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The forces and pressure distribution at subsonic speeds on a cambered and twisted wing having 45 degrees of sweepback and aspect ratio of 3 and a taper ratio of 0.5

Frederick W. Boltz, Carl D Kolbe

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Key concepts: Wing, Aspect ratio (aeronautics), Overall pressure ratio, Mechanics, Distribution (mathematics), Physics, Mathematics, Geometry

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The forces and pressure distribution at subsonic speeds on a cambered and twisted wing having 45 degrees of sweepback and aspect ratio of 3 and a taper ratio of 0.5 — Research Paper | ScholarLens