Patterson, Elizabeth W.
[Verfasser:in];
Braslow, Albert L.
[Verfasser:in]
Ordinates and theoretical pressure distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively
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Ordinates and theoretical pressure distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively