The boundary-layer and stalling characteristics of the NACA 64A010 airfoil section

Robert F. Peterson
naca-tn-2235
Nov 1950


A wind-tunnel investigation of the NACA 64A010 airfoil section was conducted to determine the boundary-layer and stalling characteristics at low speed. The tests were made at a Reynolds number of 4.1 million and included force measurements, pressure-distribution measurements, flow studies by the liquid-film technique, and boundary-layer measurements.

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http://naca.central.cranfield.ac.uk/reports/1950/naca-tn-2235.pdf