Method of analysis for compressible flow arbitrary turbomachine blades on general surface of revolution

Chung-Hua Wu, Curtis A. Brown
naca-tn-2407
Jul 1951


A method of obtaining the flow of a nonviscous compressible fluid past arbitrary compressor or turbine blades between two neighboring surfaces revolution is presented. The equations of continuity and motion obtained for such flow are combined into a nonlinear second-order differential equation in terms of a stream function defined for such flow.

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