Matrix and relaxation solutions that determine subsonic through flow in an axial-flow gas turbine

Chung-Hau Wu
naca-tn-2750
Jul 1952


A method recently developed for determining the steady flow of a nonviscous compressible fluid along a relative stream surface between adjacent blades in a turbomachine was applied to investigate the subsonic through flow in a single-stage axial-flow gas turbine.

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