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Cited article:

Numerical study on the effects of different total temperature inlet distortions on the aerodynamic performance and stability of the centrifugal compressor

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Aerospace Science and Technology 163 110292 (2025)
https://doi.org/10.1016/j.ast.2025.110292

Unsteady numerical study on the effects of inlet distortion parameters on the aerodynamic instability of the centrifugal compressor

Liangrui Zhang, Yanming Liu, Shijun Sun and Jianhua Wang
Physics of Fluids 36 (10) (2024)
https://doi.org/10.1063/5.0235181

Vortex trajectory prediction and mode analysis of compressor stall with strong non-uniformity

Li Fu, Chenxing Hu, Ce Yang, Wenrui Bao and Mi Zhou
Aerospace Science and Technology 105 106031 (2020)
https://doi.org/10.1016/j.ast.2020.106031

Active Flow Control in a Radial Vaned Diffuser for Surge Margin Improvement: A Multislot Suction Strategy

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International Journal of Rotating Machinery 2017 1 (2017)
https://doi.org/10.1155/2017/4120862

Experimental investigation of the influence of the inlet duct configuration on the unstable operation of a single-stage centrifugal blower

Kirill Kabalyk, Władysław Kryłłowicz, Grzegorz Liśkiewicz, Longin Horodko and Radomir Magiera
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy 230 (3) 260 (2016)
https://doi.org/10.1177/0957650915624817