南京航空航天大学学报：英文版2022，Vol.39Issue(6)：P.637-650,14.DOI:10.16356/j.1005-1120.2022.06.001
Effects of Lobe Peak-to-Trough Width Ratio on Mixing and Combustion Performance in ATR Combustors
ZHAO Qingjun 1ZHANG Yuankun 2HU Bin 3WANG Zhonghao 4SHI Qiang 5ZHAO Wei3
作者信息
- 1. Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,P.R.China School of Aeronautics and Astronautics,University of Chinese Academy of Sciences,Beijing 100190,P.R.China Innovation Academy for Light-Duty Gas Turbine,Chinese Academy of Sciences,Beijing 100190,P.R.China Beijing Key Laboratory of Distributed Combined Cooling Heating and Power System,Chinese Academy of Sciences,Beijing 100190,P.R.China
- 2. Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,P.R.China School of Aeronautics and Astronautics,University of Chinese Academy of Sciences,Beijing 100190,P.R.China
- 3. Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,P.R.China School of Aeronautics and Astronautics,University of Chinese Academy of Sciences,Beijing 100190,P.R.China Innovation Academy for Light-Duty Gas Turbine,Chinese Academy of Sciences,Beijing 100190,P.R.China
- 4. Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,P.R.China Innovation Academy for Light-Duty Gas Turbine,Chinese Academy of Sciences,Beijing 100190,P.R.China
- 5. Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,P.R.China
- 折叠
摘要
关键词
ATR combustor/lobed mixer/lobe peak-to-trough width ratio/mixing/combustion/streamwise vortex分类
航空航天引用本文复制引用
ZHAO Qingjun,ZHANG Yuankun,HU Bin,WANG Zhonghao,SHI Qiang,ZHAO Wei..Effects of Lobe Peak-to-Trough Width Ratio on Mixing and Combustion Performance in ATR Combustors[J].南京航空航天大学学报：英文版,2022,39(6):P.637-650,14.基金项目
supported by the National Science and Technology Major Project(No.J2019-Ⅲ-0001-0044)。 （No.J2019-Ⅲ-0001-0044）
