A rapid approximate method for determining velocity distribution on impeller blades of centrifugal compressors

John D. Stanitz, Vasily D. Prian
naca-tn-2421
Jul 1951


A rapid approximate method of analysis was developed for both compressible and incompressible, noviscous flow through radial- or mixed-flow centrifugal compressors with arbitrary hub and shroud contours and with arbitrary blade shape.

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