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Some studies on the aerodynamic effect of the gap between airplane wings and fuselages (1929)
NASA Technical Reports Server (NTRS) · leaf 16
N.A.C.A. Technical ITote STo.327 Fig.9 Kodel 0 Arrangement 1 Arrangement 2 Arrangement 3 … -0.2 0 0.2 0.4 0.6 0,8 1.0 1.2 1.4 1.6 Hi ^la-wing monoplane. Effect of wing location on moment,NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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