NASA NACA-RM-L56J04-1957 Effectiveness at transonic speeds of flap-type ailerons for several spanwise locations on a 4-percent-thick sweptback-wing-fuselage model with and without .pdf

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RESEARCH MEMORANDUM. EFFECTIVENESS AT TRANSONIC SPEEDS OF FLAP-TYPE . AILERONS FOR SEVERAL SPANWISE LOCATIONS ON A 4-PERCENT-THICK SWEPTBACK-WING-FUSEIAGE MODEL WITH AND WITHOUT TAILS ! :; By Gerald Hieser and Charles F. Whitcomb , i. . . I, Langley Aeronautical Laboratory .I I ,_ ,.,. , ,. /. Langley Field, Va. , FOR AERONAUTICS _,: -1 Figure 6.- Variation.of rolling-moment coefficient with angle of attack. Ailerons on right wing; tail off. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-