Aerodynamic characteristics and flap loads of perforated double split flaps on a rectangular NACA 23012 airfoil
Description:
From Introduction: "The results of the load tests and some additional aerodynamic characteristics of perforated double split flaps on a rectangular NACA 23012 airfoil are given in the present report."
Date:
January 1943
Creator:
Turner, Thomas R.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department