Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section

Hamilton A. Smith, Raymond F. Schaefer
naca-tn-2074
Apr 1950


An investigation has been made of the two-dimensional aerodynamic characteristics of three airfoil sections formed by removing 1.5, 4.0, and 12.5 percent of the original chord from the trailing edge of the NACA 0012 airfoil section.

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