Pressure Distribution Over Airfoils With Fowler Flaps
Description:
Report presents the results of tests made of a Clark y airfoil with a Clark y Fowler flap and of an NACA 23012 airfoil with NACA Fowler flaps. Some of the tests were made in the 7 by 10-foot wind tunnel and others in the 5-foot vertical wind tunnel. The pressures were measured on the upper and lower surfaces at one chord section both on the main airfoils and on the flaps for several angles of attack with the flaps located at the maximum-lift settings.
Date:
November 24, 1937
Creator:
Wenzinger, Carl J. & Anderson, Walter B.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department