Pressure distribution over NACA 23012 airfoil with a slotted and a split flap
Description:
A pressure-distribution investigation has been conducted in the NACA 4 by 6-foot vertical wind tunnel to determine the air loads on an NACA 23012 airfoil in combination with a 25.66-percent-chord slotted flap and a 20-percent-chord split flap. Pressures were measured on both the upper and the lower surfaces of the main airfoil and the flaps for several angles of attack and at several flap settings. The data, presented as pressure diagrams and as graphs of the section coefficients for the flap a…
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Date:
May 28, 1940
Creator:
Harris, Thomas A. & Lowry, John G.
Partner:
UNT Libraries Government Documents Department