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Summary of Airfoil Data
From Summary: "Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar as possible. The flight data consist largely of drag measurements made by the wake-survey method. Most of the data on airfoil section characteristics were obtained in the Langley two-dimensional low-turbulence pressure tunnel. Detail data necessary for the application of NACA 6-serles airfoils to wing design are presented in supplementary figures, together with recent data for the NACA 24-, 44-, and 230-series airfoils."
Date:
March 1945
Creator:
Stivers, Louis S.; Abbott, Ira H. & von Doenhoff, Albert E.
System:
The UNT Digital Library