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

Chung-Hua Wu
naca-tn-2961
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.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1953/naca-tn-2961.pdf