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THE EQUILIBRIUM TEMPERATURE PROBE, A DEVICE FOR MEASURING TEMPERATURES IN HYPERSONIC BOUNDARY LAYERS

机译:平衡温度探头,一种测量超音速边界层温度的装置

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摘要

The equilibrium temperature probe is a device which may be used to determine the flow temperature in a hypersonic boundary layer. It consists of a sharp, small angled cone of low emissivity metal supported by a thermal insulator. A thermocouple is installed to measure the cone temperature. The cone is held with its axis parallel to the flow. Ideally, the indicated temperature is the adiabatic wall temperature, a property of the flow which when combined with other more easily obtained properties and established relationships provides sufficient information to determine the total temperature of the flow.

著录项

  • 作者

    James E. Danberg;

  • 作者单位
  • 年度 1962
  • 页码 1-35
  • 总页数 35
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工业技术;
  • 关键词

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