Further comparisons of theoretical and experimental lift and pressure distributions on airfoils in cascade at low-subsonic speed

Samuel Katzoff, Margery E. Hannah
naca-tn-2391
Aug 1951


Comparisons of theoretical and experimental lift coefficients and pressure distributions were made for five compressor-type cascades of highly cambered NACA 6-series airfoils. The experimental lift coefficients, which were between 0.81 and 0.96, were 0.18 to 0.41 less than the theoretical values for the same mean-flow direction.

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