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A Theoretical Discussion of High-lift Aerofoils with Leading-edge Porous Suction

机译:具有前缘多孔吸力的高扬程翼型的理论探讨

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摘要

It is shown in this report that by the principle of porous suction high lift coefficients can be obtained on thin aerofoils by the use of surprisingly small amounts of suction. It is more economical to use porous suction than to suck through a slot at or near the leading edge:and it is necessary to realise that in general the principles involved in the two types of suction are rather different. The discussion is restricted to aerofoils with rounded leading edges, since it is difficult to predict theoretically the effect of any type of suction on flow near a sharp edge.nThere are given graphs showing estimates of the quantities of air to be sucked on three different typical thin sections to produce any reasonable desired lift coefficient.

著录项

  • 作者

    B. THWAITES;

  • 作者单位
  • 年度 1949
  • 页码 1-11
  • 总页数 11
  • 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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