Section characteristics of an NACA 0006 airfoil with area suction near the leading edge

James A. Weiberg, Robert E. Dannenberg
naca-tn-3285
Jan 1954


An investigation has been made of the low-speed two-dimensional aerodynamic characteristics of an NACA 0006 airfoil with area suction near the leading edge. The maximum lift coefficient of the airfoil was increased from 0.87 to 1.25 for a section flow coefficient of 0.0010 at a free-stream velocity of 162 feet per second.

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http://naca.central.cranfield.ac.uk/reports/1954/naca-tn-3285.pdf