Wind-Tunnel Investigation of Ordinary and Split Flaps on Airfoils of Different Profile
Description:
Report presents the results of wind tunnel tests of the Clark Y, the NACA 23012 and the NACA 23021 airfoils equipped with full-span ordinary flaps and with full-span simple split flaps. The principal object of the tests was to determine the characteristics of the airfoils with ordinary flaps and in addition, to determine the relative merits of the various airfoils when equipped with either ordinary flaps or with simple split flaps. The Clark Y airfoil was tested with 3 widths of ordinary flap, …
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Date:
October 25, 1935
Creator:
Wenzinger, Carl J.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department