Flow Control Effect of Spanwise Distributed Pulsed Arc Discharge Plasma Actuation on Supersonic Compressor Cascade FlowOA
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
Science and Technology on Plasma Dynamic Laboratory,Air Force Engineering University,Xi'an 710038,ChinaScience and Technology on Plasma Dynamic Laboratory,Air Force Engineering University,Xi'an 710038,ChinaInstitute of Aero-engine,School of Mechanical Engineering,Xi'an Jiaotong University,Xi'an 710049,ChinaScience and Technology on Plasma Dynamic Laboratory,Air Force Engineering University,Xi'an 710038,ChinaInstitute of Aero-engine,School of Mechanical Engineering,Xi'an Jiaotong University,Xi'an 710049,China
plasmaflow controlsupersonic cascadeshock wave/boundary layer interactionnumerical simulation
plasmaflow controlsupersonic cascadeshock wave/boundary layer interactionnumerical simulation
《热科学学报(英文版)》 2022 (5)
等离子体激励调控亚声速压气机叶型附面层流动探索研究
1723-1733,11
This research is supported by National Natural Science Foundation of China(Grant No.51790511,51906254).
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