Contribution to the Problem of Airfoils Spanning a Free Jet (1936)
NASA Technical Reports Server (NTRS) · leaf 29
N.A.C.A. Technical Memorandum No, 796 Figs. 11,12,13,14. 123U55789 0123U56789 Figure 11.- Circulation with Figure 12-- Circulation with x/I - 0.25 as a wing placed in middle of jet as a function of X. function of x. *11=0,0625 XkmQ125 … Figure 14.- Circulation with Figure 13.- Circulation with x/l = 0.0625 as x/l = 0.125 as a a function of A. function of X.
NASA Technical Reports Server (NTRS)
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