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Chordwise pressure distribution at high subsonic speeds near midsemispan of a tapered 35 degree sweptback wing of aspect ratio 4 having NACA 65A006 airfoil sections and equipped with various spoiler ailerons

Alexander D Hammond, Barbara M Mcmullan

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Key concepts: Airfoil, Wing, Degree (music), Aileron, NACA airfoil, Mathematics, Geology, Aerospace engineering

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Chordwise pressure distribution at high subsonic speeds near midsemispan of a tapered 35 degree sweptback wing of aspect ratio 4 having NACA 65A006 airfoil sections and equipped with various spoiler ailerons — Research Paper | ScholarLens