Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps (1937)
NASA Technical Reports Server (NTRS) · leaf 6
TAPERED WINGS WITH OBDINAEY AILERONS AND PARTIAL^PAN SPLIT FLAPS 739 For the 5:3 tapered wing, the vaiiation of rolling however, vary in a manner similar to those on the 5:1 moment with aileron deflection is much the same as tapered wing. As in the case of the ailerons on the that of the ailerons… … Aileron deflection, da, degrees FioDBE 18.—HlDge-momenl coeffidents of 0.2Se. by 0.411 tapered aileron on 5:3 TIOUBB au—Boning- and yawlng-moment coefficients of 0.2fic by 0i30 j tapered tapered wing. Flaps nentral. aileron on 6:3 tapered wing. The 0.16e, by 0.706 tapered split flaps deflected 60°.…
NASA Technical Reports Server (NTRS)
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