Contribution to the Problem of Airfoils Spanning a Free Jet (1936)
NASA Technical Reports Server (NTRS) · leaf 31
Figs. 30,21,33,23. N.A.C.A, Technical Memorandum No, 796 1,6 I I I I I I | severely andde+fects 1A 1,2 Figure 81.- Position of 1,0 reference axis. Q8 Q6 qu 0,2 0 … Figure 22.- Effect of distance Figure 23.- of wing from throat Polars of wing spanning a circular of tunnel on lift and free jet eccentrically, R/t = 4. drag.
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