Figs.T&g. 1.0 • 5 0.9 Q • 3 OJ ii •J ►4 H X *H O *rl .1 £ 0.6 Triplane w with x*l/3 0.5 .1 .2 .3 G/b Fig.7. Efficiency K of various wing systens and coefficient of distribution of wing loads x, for the triplane.
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