Subsonic flow of air through a single-stage and a seven-stage compressor

Chung-Hua Wu
Jun 1953

A method recently developed for solving the steady flow of a conviscous compressible fluid along a relative stream surface between two adjacent blades in a turbomachine is applied to investigate the low- and high-speed subsonic air flow through a single-stage and through a seven-stage axial compressor.

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