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AN INVESTIGATION OF A THREE-DIMENSIONAL TURBULENT BOUNDARY LAYER IN HYPERSONIC FLOW

机译:超音速流中三维湍流边界层的研究

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摘要

Turbulent heating rates have been measured by means of the shrouded .model technique on a blunted cone at angle of attack. The Reynolds number, based on conditions at the stagnation point, was varied from 1.7 10 to approximately 3.7 10. The enthalpy ratio (stagnation to wall) varied from 2.1 to approximately 1.5.nThe experimental data are compared to the flat-plate reference-enthalpy theory applied along the inviscid streamlines. It is shown that this relatively simple method is in reasonable agreement with the data.

著录项

  • 作者

    GENNARO F. AIELLO;

  • 作者单位
  • 年度 1963
  • 页码 1-51
  • 总页数 51
  • 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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