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Effects of Pilot Fuel Ratio on Combustion Process:Flow Field Structure and Pollutant Emissions

ZONG Chao JI Chenzhen CHENG Jiaving ZHU Tong

热科学学报(英文版)2023,Vol.32Issue(6):2321-2335,15.
热科学学报(英文版)2023,Vol.32Issue(6):2321-2335,15.DOI:10.1007/S11630-023-1837-4

Effects of Pilot Fuel Ratio on Combustion Process:Flow Field Structure and Pollutant Emissions

Effects of Pilot Fuel Ratio on Combustion Process:Flow Field Structure and Pollutant Emissions

ZONG Chao 1JI Chenzhen 2CHENG Jiaving 2ZHU Tong2

作者信息

  • 1. Postdoctoral Station of Mechanical Engineering,Tongji University,Shanghai 201804,China||School of Mechanical Engineering,Tongji University,Shanghai 201804,China
  • 2. School of Mechanical Engineering,Tongji University,Shanghai 201804,China
  • 折叠

摘要

关键词

micro gas turbine/pilot fuel ratio/flow field structure/carbon monoxide/nitrogen oxide

Key words

micro gas turbine/pilot fuel ratio/flow field structure/carbon monoxide/nitrogen oxide

引用本文复制引用

ZONG Chao,JI Chenzhen,CHENG Jiaving,ZHU Tong..Effects of Pilot Fuel Ratio on Combustion Process:Flow Field Structure and Pollutant Emissions[J].热科学学报(英文版),2023,32(6):2321-2335,15.

基金项目

This work was supported by the Science and Technology Commission of Shanghai Municipality(20dz1204902). (20dz1204902)

热科学学报(英文版)

OACSCDEI

1003-2169

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