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A flight and wind tunnel investigation of the effect of angle-of-attack rate on maximum lift coefficient

F. Conner, W. J. Twomey, C. S. Willey

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Abstract

Wind tunnel tests to determine effect of angle of attack on maximum lift at stall for half-wing models, and single engine, jet propelled aircraft

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Wind tunnel tests to determine effect of angle of attack on maximum lift at stall for half-wing models, and single engine, jet propelled aircraft

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OpenAlex reports 2 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available abstract

Wind tunnel tests to determine effect of angle of attack on maximum lift at stall for half-wing models, and single engine, jet propelled aircraft

Key concepts: Angle of attack, Lift coefficient, Lift (data mining), Wind tunnel, Environmental science, Aeronautics, Aerodynamics, Meteorology

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A flight and wind tunnel investigation of the effect of angle-of-attack rate on maximum lift coefficient — Research Paper | ScholarLens