Effect of fuselage and engine nacelles on some aerodynamic properties of an airplane wing (1934)
NASA Technical Reports Server (NTRS) · leaf 11
1T.A.C.A. Technical Lleraorandiim ITo. 736 Figs. 4,5,6 Fuselage ct-e Figure 5.- Effective angle of attack induced on fuselage "by wing at zero Figure 4.- Circulation for angle of attack. wing and fuselage plotted against angle of attack. Wing alone 7/ing with fuselage and nacelles … Figure 6.- Lift distribution over span of wing with fuselage and na-celles.
NASA Technical Reports Server (NTRS)
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