High-speed wind-tunnel tests of the NACA 23012 and 23012-64 airfoils
Description:
Report presenting force tests of the NACA 23012 and 23012-64 airfoils of 24-inch chord in the high-speed wind tunnel at a range of Mach numbers. The results show the variation with mach number of lift, drag, and pitching-moment coefficients at a range of angles of attack.
Date:
February 1941
Creator:
Becker, John V.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department