The Effect of a Flap and Ailerons on the N.A.C.A. M-6 Airfoil Section (1928)
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5 EFFECT OF A FLAP AND AILERONS ON THE N. A. C. A.-M6 AIRFOIL SECTION 1.6 1.4 1.2 *$I.O $0.8 10.6 8 ^0.4 0.2 0 -0.2 -8" -4° 0° 4° 8° '2° 16' 20' 24° 26° 32° 36' 40' 44° 48° Ang/e of attack, cC Fig. 8.—Life coefficient versus angle of attack of N. A. C. A. M-6 airfoil with different aileron settings … -12' -8' -4° 0° 4' 8° 12" 16° "16° 20' 24' 28' 32° 36° 40° 44' 48' Angle of attack, cL Fio. 9—Drag coefficient versus angle of attack of N. A. C. A. M-6 airfoil with different flap settings 4° 8° 12' 16 -8° -4' Angle of otiack, cC Fig. 10.—Drag coefficient versus angle of attack of N. A. C. A. M-6…
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