Effect of amplitude and mean angle-of-attack on the boundary layer of an oscillating aerofoil

著录项

• 来源
  《Aeronautical journal》 |2008年第1138期|705-713|共9页
• 作者

  M. R. Soltani; A. Bakhshalipour;

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• 作者单位

  Sharif University of Technology Department of Aerospace Engineering Tehran, Iran;

  Sharif University of Technology Department of Aerospace Engineering Tehran, Iran;

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• 收录信息
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  c: aerofoil chord (m); C_p: pressure coefficient (p-p∞)/q∞; f: oscillation frequency (hz); R_c: chord reynolds number = cU∞/v; rnx/c: distance of a hot-film sensor from the leading edge; et al;

  机译：c：翼型弦（m）;C_p：压力系数（p-p∞）/q∞;f：振荡频率（hz）;R_c：和弦雷诺数＝cU∞/ v;rnx / c：热膜传感器到前端的距离;等;