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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 12
N.A.d.A. Tochnicr,! Hot3 ITo.327 Fig.5 Model B Arrangement 1 Arrangement 2 1.6 … -0.31 1 1 ! 1 1 1 1 1 0 0.1 0.2 0.3 0.4 Fig.5 Biplane. Effect of upper wing location on drag.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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