The Effect of a Flap and Ailerons on the N.A.C.A. M-6 Airfoil Section (1928)
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EFFECT OF A FLAP AND AILEKONS ON THE N. A. C. A.-M6 AIRFOIL SECTION 3 … AO' Fin r>.—Polar curves of N. A. C. A. M-6 airfoil with different flap Fir,, fi—Polar curves of N. A. C. A. M-6 airfoil with different settings aileron settings Angle of ottocK, oC Fig. 7.—Lift coefficient versus angle of attack of N. A. C. A. M-6 airfoil with different flap settings
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