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Tests of Airfoils Designed to Delay the Compressibility Burble (1939)
NASA Technical Reports Server (NTRS) · leaf 28
A.C.A. Fig". 14 16-106 — 16-109 16-506- -2 '0 .2 .4 .6 .8 W 1.2 Lift coefficient, CL 1.2 … Angle of attack, cC, deg. Cmc/4 Figure 14NASA Technical Reports Server (NTRS)
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