Impact investigation of inlet environmental changes on the rated condition performance of a high-pressure compressor
Author:
Affiliation:
1. Harbin Marine Boiler and Turbine Research Institute , Harbin, China, No. 35, Honghu Road , Harbin , Heilongjiang , China
Abstract
Publisher
Walter de Gruyter GmbH
Subject
Aerospace Engineering
Link
https://www.degruyter.com/document/doi/10.1515/tjj-2022-0022/pdf
Reference32 articles.
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3. Khaleghi, H. A new approach of endwall recirculation in axial compressors. Aero Sci Technol 2020;98:105704. https://doi.org/10.1016/j.ast.2020.105704.
4. Wang, W, Lu, J, Luo, X, Chu, W. Coupling method of stability enhancement based on casing treatments in an axial compressor. Aero Sci Technol 2019;95:105449. https://doi.org/10.1016/j.ast.2019.105449.
5. Lu, H, Yang, Z, Pan, T, Li, Q. Non-uniform stator loss reduction design strategy in a transonic axial-flow compressor stage under inflow distortion. Aero Sci Technol 2019;92:347–62. https://doi.org/10.1016/j.ast.2019.06.015.
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