Determination of the air forces and moments produced by the ailerons of an airplane (1928)
NASA Technical Reports Server (NTRS) · leaf 19
N.A.O.A. Technical Memorandum No.488 Figs.8,9,10. .8 p=4.0 4.5 Fig.8 Coefficients 6.0 * of additional lift for like aileron settings. .8 1.0 … Fig.10 Lift coefficient ca vs. angle of attack for different settings, P of full-length ailerons, on N.A.C.A.-M6 airfoil. 16 24 " 32 40 48° a
NASA Technical Reports Server (NTRS)
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