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Experimental Study on Diffuser Passage of Exit Stage Rotor in a Multistage Axial Compressor

ZHANG Xiaoyu DU Qiang JIN Yun HOU Ruohan MENG Fanxing ZHAO Shidi WANG Wentao LI Jichao GENG Shaojuan ZHANG Hongwu

热科学学报（英文版）2026，Vol.35Issue(3)：717-730,14.

热科学学报（英文版）2026，Vol.35Issue(3)：717-730,14.DOI:10.1007/s11630-026-2289-4

Experimental Study on Diffuser Passage of Exit Stage Rotor in a Multistage Axial Compressor

ZHANG Xiaoyu ¹DU Qiang ¹JIN Yun ²HOU Ruohan ¹MENG Fanxing ¹ZHAO Shidi ¹WANG Wentao ¹LI Jichao ¹GENG Shaojuan ¹ZHANG Hongwu¹

作者信息

1. Advanced Gas Turbine Laboratory,Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China||University of Chinese Academy of Sciences,Beijing 100049,China||National Key Laboratory of Science and Technology on Advanced Light-duty Gas-turbine,Beijing 100049,China
2. School of Aeronautics and Astronautics,Shanghai Jiao Tong University,Shanghai 200240,China
折叠

摘要

关键词

compressor exit stage/diffuser passage design/experiment

Key words

compressor exit stage/diffuser passage design/experiment

引用本文复制引用

ZHANG Xiaoyu,DU Qiang,JIN Yun,HOU Ruohan,MENG Fanxing,ZHAO Shidi,WANG Wentao,LI Jichao,GENG Shaojuan,ZHANG Hongwu..Experimental Study on Diffuser Passage of Exit Stage Rotor in a Multistage Axial Compressor[J].热科学学报（英文版）,2026,35(3):717-730,14.

基金项目

This study is supported by the National Natural Science Foundation of China with Project No.U24A20138,National Natural Science Foundation of China with Project No.52376039,Beijing Natural Science Foundation(No.JQ24017),National Science and Technology Major Project of China(Nos.J2019-Ⅱ-0005-0025 and Y2022-Ⅱ-0002-0005)and the Excellence Research Group Program(ERGP,the former Basic Science Center Program)(No.52488101). （No.JQ24017）

热科学学报（英文版）

ISSN：1003-2169

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