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The effect of compressibility on the pressure reading of a Prandtl pitot tube at subsonic flow velocity

机译:压缩性对普朗特皮托管在亚音速流速下的压力读数的影响

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摘要

Errors arising from yawed flow were also determined up to 20 degrees angle of attack. In axial flow, the Prandtl pitot tube begins at w/a approx. = 0.8 to give an incorrect static pressure reading, while it records the tank pressure correctly, as anticipated, up to sonic velocity. Owing to the compressibility of the air, the Prandtl pitot tube manifests compression shocks when the air speed approaches velocity of sound. This affects the pressure reading of the instrument. Because of the increasing importance of high speed in aviation, this compressibility effect is investigated in detail.

著录项

  • 作者

    Walchner, O;

  • 作者单位
  • 年度 1939
  • 页码 1-13
  • 总页数 13
  • 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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