Three-Dimensional Supersonic Minimum Length Nozzle Design at High Temperature for Arbitrary Exit Cross Section

著录项

• 来源
  《Arabian Journal for Science and Engineering》 |2014年第11期|8233-8245|共13页
• 作者

  Omar Abada; Toufik Zebbiche; Ahmed Abdallah El-Hirtsi;

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• 作者单位

  1.Department of Mechanical Engineering Faculty of Technology University of Blida 1 BP 270 09000 Blida Algeria;

  2.Aeronautical Sciences Laboratory Institute of Aeronautics and Space Studies University of Blida 1 BP 270 09000 Blida Algeria;

  2.Aeronautical Sciences Laboratory Institute of Aeronautics and Space Studies University of Blida 1 BP 270 09000 Blida Algeria;

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• 收录信息 美国《科学引文索引》(SCI);
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  Nozzle shape; Supersonic flow; High-temperature flow; Axisymmetric MLN nozzle; Method of characteristics; Mach number;

  机译：喷嘴形状;超音速流动;高温流动;轴对称MLN喷嘴;特性方法;马赫数;