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title: National Advisory Committee for Aeronautics -- Reports
Tests of four racing type airfoils in the twenty-foot propeller research tunnel
Effect of partial-span split flaps on aerodynamic characteristics of clark Y wing
Wind tunnel pressure distribution tests on an airfoil with trailing edge flap
Development of N.A.C.A. Slot-lip aileron
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack
Drag testing. Full scale drag tests on various parts of sperry messenger airplane