Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7

M. J. Turner, S. Rabinowitz
naca-tn-2213
Oct 1950

Dietze's method for the solution of Possio's integral equation has been used to determine the chordwise distribution of lift on an oscillating airfoil with simple hinged flap in two-dimensional compressible flow (subsonic).

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