Effects of cooling flow on the flow structure and acoustic oscillation in a swirl-stabilized combustor

著录项

• 来源
  《Journal of Visualization》 |2013年第4期|287-295|共9页
• 作者

  Kwang-Hee Yoo; Jong-Chan Kim; Hong-Gye Sung;

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• 作者单位

  High-speed Propulsion and Combustion Control Laboratory Department of Aerospace and Mechanical Engineering Korea Aerospace University">(1);

  High-speed Propulsion and Combustion Control Laboratory Department of Aerospace and Mechanical Engineering Korea Aerospace University">(1);

  High-speed Propulsion and Combustion Control Laboratory Department of Aerospace and Mechanical Engineering Korea Aerospace University">(1);

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• 收录信息
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  Swirl combustor; Cooling flow injection; Turbulent flow; Large-eddy simulation;

  机译：旋流燃烧室;冷却流注入;湍流;大涡模拟;