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A study of the pitching moments and the stability characteristics of monoplanes (1934)

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Figs. 5,6,7 N.A.C.A. Technical Note No.511 … Degrees, da t Figure 5.-Variation of factor Fi, with absolute angle of attack for different aspect ratios. .07 12 .08 10 8 .05 7 6 F3 .4 04 F2 .3 .2 .02 .1 .01 6~S 10 12 14 16 8 12 16 20 24 Effective aspect ratio of wing,Aw Degrees, da Figure 6.-Variation of factor F2 Figure 7.-Variation of factor…

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