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Flow Control Effect of Spanwise Distributed Pulsed Arc Discharge Plasma Actuation on Supersonic Compressor Cascade Flow

SHENG Jiaming WU Yun ZHANG Haideng WANG Yizhou TANG Mengxiao

热科学学报（英文版）2022，Vol.31Issue(5)：1723-1733,11.

Flow Control Effect of Spanwise Distributed Pulsed Arc Discharge Plasma Actuation on Supersonic Compressor Cascade Flow

SHENG Jiaming ¹WU Yun ¹ZHANG Haideng ²WANG Yizhou ¹TANG Mengxiao²

作者信息

1. Science and Technology on Plasma Dynamic Laboratory,Air Force Engineering University,Xi'an 710038,China
2. Institute of Aero-engine,School of Mechanical Engineering,Xi'an Jiaotong University,Xi'an 710049,China
折叠

摘要

关键词

plasma/flow control/supersonic cascade/shock wave/boundary layer interaction/numerical simulation

Key words

plasma/flow control/supersonic cascade/shock wave/boundary layer interaction/numerical simulation

引用本文复制引用

SHENG Jiaming,WU Yun,ZHANG Haideng,WANG Yizhou,TANG Mengxiao..Flow Control Effect of Spanwise Distributed Pulsed Arc Discharge Plasma Actuation on Supersonic Compressor Cascade Flow[J].热科学学报（英文版）,2022,31(5):1723-1733,11.

基金项目

This research is supported by National Natural Science Foundation of China(Grant No.51790511,51906254). （Grant No.51790511,51906254）

热科学学报（英文版）

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ISSN：1003-2169

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