1953•Unpublished venueRequires access

The effect at high subsonic speeds of a flap-type aileron on the chordwise pressure distribution near midsemispan of a tapered 35 degree sweptback wing of aspect ratio 4 having NACA 65A006 airfoil section

Alexander D Hammond, Barbara M Keffer

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Key concepts: Aileron, Wing, Aspect ratio (aeronautics), Degree (music), Wing loading, Angle of attack, Mechanics, Materials science

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The effect at high subsonic speeds of a flap-type aileron on the chordwise pressure distribution near midsemispan of a tapered 35 degree sweptback wing of aspect ratio 4 having NACA 65A006 airfoil section — Research Paper | ScholarLens