17.A.C.A. Technical Memorandum IT0.63O Figs.21,22,23 … Fig.22 Balance of no:aonts atout longitudinal axis. Aerodynamic moment of wing against a and cp. cp=-30°,a=27°,%=0 -11 ,2i 320q\cos,AcJ r \ Wing alone 2U0d 1 1 1 1 : l 20° Uo° o0° 80° JJ I :-^Tt -—mmi ' -6 -4 -2 z, m Fig.21 Distribution of normal force across the wing. Fig. 23 Normal and tangential…
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