Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps (1937)
NASA Technical Reports Server (NTRS) · leaf 5
0°. FlQDBE 12.—BdUng- and yawing-momont coefficients of 02Sc by OJO ij tapered aileron on fi:l tapered wing. Flaps neutral. •a o u . 1' I.-' ! Aileron deflection, 8a, degrees -16 -a 0 8 16 Aileron deflection, 6a, degrees FiouKE 13.—Rolling- and yawing-moment coeflMents of 0.25c by OJO j tapered… … AILERON CHARACTERISTICS. 5:3 TAPERED WING Aileron deflection, 6a, degrees FiausE 17.—Rolling- and yawlng-moment coefficients of O.iSCw by 0.41 ^ tapered Eolling-, yawing-, and hinge-moment coefficients of aileron on S:3 tapered wing. The 0 JSc by 0.£eei tapered split flaps deflected W, the 0.25cb…
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