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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 15
H.A.C.A. Figure 9.- N.A.C.A. 1412-34 airfoil. cz ■ 0,17 Arrows indicate location of transition corresponding to the Reynolds N-umber in millions. MQ * 0.73.NASA Technical Reports Server (NTRS)
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