首页> 美国政府科技报告 >IMPROVED NOZZLE TESTING TECHNIQUES IN TRANSONIC FLOW INFLUENCE OF JET PARAMETERS PART I:NOZZLE THRUST AND DISCHARGE COEFFICIENTS
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IMPROVED NOZZLE TESTING TECHNIQUES IN TRANSONIC FLOW INFLUENCE OF JET PARAMETERS PART I:NOZZLE THRUST AND DISCHARGE COEFFICIENTS

机译:跨音速流动对喷射参数影响的改进喷嘴测试技术第一部分:喷嘴推力和排放系数

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摘要

Internal flow and nozzle characteristice were analysed as part of the program coordinated by the AGARD ad hoo study group. All available data were used in a comparison of the nozzle discharge and thrust coefficients and jet pipe wall stato pressures of similar nodal configurations. lb was found necessary to take into account the distortion of the total pressure profiles in the jet pipe. The mass flow averaged total pressure was used in the calculations. The distortion coefficient DCM proved to be a useful tool in the comparison of the mass flow averaged total pressure with the 1-D. semitropical total pressure, derived from mass flow, temperature and static pressure.

著录项

  • 作者

    C. C. GROOTHOFF;

  • 作者单位
  • 年度 1975
  • 页码 1-46
  • 总页数 46
  • 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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