Theoretical span loading and moments of tapered wings produced by aileron deflection (1937)
NASA Technical Reports Server (NTRS) · leaf 37
Aspect ratio, A Rath of tip chord to root chord, A figure 14.- Xheoretloa.1 «ddltional-in<J.uoed-4r*g footer due to rqlliag, K, for p « 1.0. Additional induoad drag - iTqjbSfp'b/iJV)2!^. M .e riguxs 17.- Theoxrtlaally obtainaWn rsjuai of- Ratio ofolfmron span 1o wing span, bfb H •o
NASA Technical Reports Server (NTRS)
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