Effect of fuselage and engine nacelles on some aerodynamic properties of an airplane wing (1934)
NASA Technical Reports Server (NTRS) · leaf 13
Pigs. 10,3.1 N.A.C.A. Technical Memorandum lTo.726 , Measured .-i Calculated 20 10 0 10 20 Wing without fuselage Figure 10.-Direction of dovm current at horizontal tail surfaces vs. span($ of serai span) at various angles of attack of wing. … 20 10 0 10 20 Wing with fuselage Figure 11.-Direction of down current at horizontal tail surfaces vs. span($ of semispan) at various angles of attack of wing with fuselage.
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