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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 14
56 .028 20- •z > 0 o > 48 .024 -20 ^ o 0 20 40 60 80 100 Percent of chord … Figure 7.- N.A.CA. 2412-34 airfoilNASA Technical Reports Server (NTRS)
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