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Reduction of lift of a wing due to its drag (1935)

NASA Technical Reports Server (NTRS) · leaf 7

An illustration from Reduction of lift of a wing due to its drag, 1935, leaf 7
ET.A.C.A. Technical Memorandum Mo, 781 Fig, 3,4 … x ?igure 3.- Location of transition point from laminar to turbulent flow, pressure side, X Figure 4— Graph of turbulent friction layer.

NASA Technical Reports Server (NTRS)

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