Effect of fuselage and engine nacelles on some aerodynamic properties of an airplane wing (1934)
NASA Technical Reports Server (NTRS) · leaf 10
N.A.C.A. Technical Memorandum Ho. 736 Pigs. 1,2,3 6030'->|\/r FT i ■i 0 *2 ti ^2 1*° r Figure 1.-Arrangement of fuselage and engine nacelles. Wing without fuselage. … 333 .383 .5 .5 Figure 2.-Lift distribution over span of wing with fuselage. a, Fuselage c, Wing d, Total downward velocity .259 .259 .866 .383 .383 .966 .5 k. 5 Figure 3.-Distribution of induced velocity over span of wing with fuselage.
NASA Technical Reports Server (NTRS)
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