Experiments on the Influence of a Microramp Array on a Hypersonic Shock Turbulent Boundary Layer Interaction

著录项

• 来源
  《41st AIAA fluid dynamics conference and exhibit 2011》|2011年|p.1307-1322|共16页
• 会议地点 Honolulu HI(US)
• 作者

  Anne-Marie Schreyer; Dipankar Sahoo; Alexander J. Smits;

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• 作者单位

  Institute for Aerodynamics and Gas Dynamics, University of Stuttgart, 70569 Stuttgart, Germany;

  Gas Dynamics Laboratory, Princeton University, Princeton, New Jersey, 08544, United States;

  Gas Dynamics Laboratory, Princeton University, Princeton, New Jersey, 08544, United States;

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• 会议组织
• 原文格式 PDF
• 正文语种 eng
• 中图分类 流体动力学;
• 关键词

  B: Constant on the log-law; M: Mach number; Re_θ: Reynolds number based on momentum thickness; T: Temperature, K; U: Streamwise velocity, m/s;

  机译：B：对数律不变； M：马赫数； Re_θ：基于动量厚度的雷诺数； T：温度，K； U：流向速度，m / s;