Aerodynamic Effects Caused by Icing of an Unswept NACA 65A004 Airfoil
Description:
From Summary: "The effects of ice formations on the section lift, drag, and pitching-moment coefficients of an unswept NACA 65A004 airfoil section of 6-foot chord were studied.. The magnitude of the aerodynamic penalties was primarily a function of the shape and size of the ice formation near the leading edge of the airfoil. The exact size and shape of the ice formations were determined photographically and found to be complex functions of the operating and icing conditions."
Date:
February 1958
Creator:
Gray, Vernon H. & von Glahn, Uwe H.
Item Type:
Refine your search to only
Report