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Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel. III: the effectiveness of a constant-chord aileron

Description: Report presenting a wind-tunnel investigation at a range of Mach numbers with a constant Reynolds number of a semispan model of a thin, unswept wing of aspect ratio 4 and taper ratio 0.5 with a constant-chord aileron and a modified diamond profile. Results regarding lift and rolling-moment characteristics and aileron effectiveness are provided.
Date: November 19, 1948
Creator: Johnson, Ben H., Jr. & Demele, Fred A.
Partner: UNT Libraries Government Documents Department