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Preliminary Investigation of Certain Laminar-Flow Airfoils for Application at High Speeds and Reynolds Numbers (1939)
NASA Technical Reports Server (NTRS) · leaf 16
N.A.C.A. Fig.10 … 0 50 100 Percent chord figure 10.- N.A.C.A. 2412-34 airfoil. ct = 0,31 Arrows indicate location of transition corresponding to the Eeynolds Number .in millions. Mc - 0.69.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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