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Measurement of unsteady force on rotor blade surfaces in axial flow compressor

Jingyuan LIU Jichao LI Feng PENG Yang LIU Hongwu ZHANG

中国航空学报（英文版）2025，Vol.38Issue(2)：31-45,15.

中国航空学报（英文版）2025，Vol.38Issue(2)：31-45,15.DOI:10.1016/j.cja.2024.10.009

Measurement of unsteady force on rotor blade surfaces in axial flow compressor

Jingyuan LIU ¹Jichao LI ¹Feng PENG ¹Yang LIU ¹Hongwu ZHANG¹

作者信息

1. Advanced Gas Turbine Laboratory,Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China||School of Aeronautics and Astronautics,University of Chinese Academy of Sciences,Beijing 100049,China||National Key Laboratory of Science and Technology on Advanced Light-duty Gas-turbine,Beijing 100190,China||Key Laboratory of Advanced Energy and Power,Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China||Innovation Academy for Light-duty Gas-turbine,Chinese Academy of Sciences,Beijing 100190,China
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摘要

关键词

Axial flow compressor/Unsteady blade surface force/Wireless telemetry/Tip leakage flow/Vibration characteristic/Unsteady flow

Key words

Axial flow compressor/Unsteady blade surface force/Wireless telemetry/Tip leakage flow/Vibration characteristic/Unsteady flow

引用本文复制引用

Jingyuan LIU,Jichao LI,Feng PENG,Yang LIU,Hongwu ZHANG..Measurement of unsteady force on rotor blade surfaces in axial flow compressor[J].中国航空学报（英文版）,2025,38(2):31-45,15.

基金项目

This study was funded by the National Natural Science Foun-dation of China(Nos.U24A20138 and No.52376039),the Beijing Natural Science Foundation,China(JQ24017),and the National Science and Technology Major Project of China(Nos.J2019-11-0005-0025 and Y2022-Ⅱ-0002-0005).The authors also thank the Special Fund for the Member of Youth Innovation Promotion Association of Chinese Academy of Sciences,China(No.2018173).The authors are also grateful to Prof.Juan DU and Dr.Chen YANG for their insightful discussion. （Nos.U24A20138 and No.52376039）

中国航空学报（英文版）

ISSN：1000-9361

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