Wind-tunnel investigation of an NACA 23012 airfoil with two sizes of balanced split flap
Description:
Report presenting an investigation in the 7- by 10-foot wind tunnel of an NACA 23012 airfoil with a 15-percent-chord and a 25-percent-chord balanced split flap of Clark Y profile. The primary purpose was to determine the aerodynamic section characteristics of the airfoil as affected by the size, nose location, and deflection of the flap.
Date:
November 1940
Creator:
Harris, Thomas A. & Purser, Paul E.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department