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Preliminary Aerodynamic Design of 13:1 Pressure Ratio Axial-Centrifugal Compressor
J. KIMS Technol. 2003;6(2):83-94.

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Aerodynamic Retrofit Design for a High Pressure Compressor Using a High Hub/Tip Ratio Mixed-Flow Compressor
Volume 2E: Turbomachinery. 2020;   Crossref logo
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Preliminary Design of a Centrifugal Compressor for a Turbocharge
Fluid Mechanics and Thermodynamics of Turbomachinery. 2014;497-505   Crossref logo
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Comparison of Cooling Different Parts in a High Pressure Ratio Centrifugal Compressor
Applied Sciences. 2016;7(1):16   Crossref logo
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Aerodynamic Design Aspects for Stator of Highly Loaded Tandem Bladed Axial Compressor
Volume 2A: Turbomachinery. 2020;   Crossref logo
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Aerodynamic effects of impeller-diffuser axial misalignment in low-flow-coefficient centrifugal compressor
Science China Technological Sciences. 2014;58(1):29-36   Crossref logo
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Impact of Operating Conditions on Rotor/Stator Interaction of a High-Pressure Ratio Centrifugal Compressor
Volume 10B: Turbomachinery — Axial Flow Turbine Aerodynamics; Deposition, Erosion, Fouling, and Icing; Radial Turbomachinery Aerodynamics. 2022;   Crossref logo
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Influences of the Flow Cut and Axial Lift of the Impeller on the Aerodynamic Performance of a Transonic Centrifugal Compressor
Energies. 2019;12(23):4503   Crossref logo
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Aerodynamic preliminary design optimization of a centrifugal compressor turbocharger based on one-dimensional mean-line model
Engineering Computations. 2021;38(9):3438-3469   Crossref logo
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Design of a Novel Axial Flux-Switching PM Machine Integrated with Centrifugal Compressor with Radial Impellers
2019 IEEE Transportation Electrification Conference and Expo (ITEC). 2019;   Crossref logo
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Influence of Splitter Blades on the Performance of a Single-Stage Centrifugal Compressor With Pressure Ratio 12.0
Volume 2E: Turbomachinery. 2020;   Crossref logo
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