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Effects of Dielectric Barrier Discharge Plasma on the Combustion Performances of Reverse-Flow Combustor in an Aero-Engine

DENG Jun PENG Changxin HE Liming WANG Shuai YU Jinlu ZHAO Bingbing

热科学学报(英文版)2019,Vol.28Issue(5):1035-1041,7.
热科学学报(英文版)2019,Vol.28Issue(5):1035-1041,7.

Effects of Dielectric Barrier Discharge Plasma on the Combustion Performances of Reverse-Flow Combustor in an Aero-Engine

Effects of Dielectric Barrier Discharge Plasma on the Combustion Performances of Reverse-Flow Combustor in an Aero-Engine

DENG Jun 1PENG Changxin 2HE Liming 1WANG Shuai 2YU Jinlu 1ZHAO Bingbing1

作者信息

  • 1. Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi'an 710038, China
  • 2. AECC Hunan Aviation Powerplant Research Institute, Zhuzhou 412002, China
  • 折叠

摘要

关键词

aero-engine/reverse-flow combustor/double dielectric barrier discharge/plasma assisted combustion

Key words

aero-engine/reverse-flow combustor/double dielectric barrier discharge/plasma assisted combustion

引用本文复制引用

DENG Jun,PENG Changxin,HE Liming,WANG Shuai,YU Jinlu,ZHAO Bingbing..Effects of Dielectric Barrier Discharge Plasma on the Combustion Performances of Reverse-Flow Combustor in an Aero-Engine[J].热科学学报(英文版),2019,28(5):1035-1041,7.

基金项目

This research was supported by the National Natural Science Foundation of China (Funding Nos.51436008,91741112 and 51806245). (Funding Nos.51436008,91741112 and 51806245)

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