The N.A.C.A. CYH airfoil section
Description:
The NACA CYH airfoil section is described and its aerodynamic characteristics are given as tested in the NACA variable density wind tunnel at twenty atmosphere pressure. This section has a low drag, a high maximum lift, and a small travel of center of pressure.
Date:
June 1926
Creator:
Higgins, George J.
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