Date: December 28, 1944
Creator: Weisman, Yale & Holtzclaw, Ralph W.
Description: Tests were conducted at dynamic pressure of 50 lb per square foot with lift drag and pitch moment measurements throughout useful angle of attack range for constant flap deflection and position of a low-drag airfoil. Two slots were investigated and practical flap paths were selected for each Slot shape had a negligible effect on the maximum lift coefficient flap deflected, the rounded-entry slot had lower profile drag.
Contributing Partner: UNT Libraries Government Documents Department