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An improved two-zone model for the design of supercritical CO2 centrifugal compressors and verification
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DOI：10.1016/j.ijheatfluidflow.2025.110034.png)
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Abstract
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• An improved two-zone model is proposed for the design of SCO2 centrifugal compressor. • Model accuracy and computational efficiency are enhanced by SOA curves and primary flow deviation angle curves. • Model validity is confirmed against published available data and CFD simulation. • Blade tip leakage effects on compressor aerodynamic performance are elucidated.
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