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Design and Testing of a High-Pressure-Ratio Centrifugal Stage – Probing the Aerodynamic & Mechanical Limits
(Turbomachinery Laboratory, Texas A&M Engineering Experiment Station, 2018)
The paper describes the design, manufacture and testing of a novel high-pressure-ratio, single-stage centrifugal compressor targeted
for use in high molecular weight applications. The stage was designed to deliver a minimum ...