Investigation of the Effect of the Fuselage on the Wing of a Low-Wing Monoplane (1929)
NASA Technical Reports Server (NTRS) · leaf 21
Technical Memorandum No.517 Figs.7 & 9 … Fig.7 Fuselage with tapered wings. 1000 - -J Le-." 115.5 03 o o 03 r- to CO CM Fig.9 Wing with triangular fuselage,angle 120^ \
NASA Technical Reports Server (NTRS)
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