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Characterization of Low-Frequency Oscillations in the Flowfield About an Iced Airfoil

机译:冰翼型流场中低频振荡的特征

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摘要

Wind-tunnel measurements were used to identify and characterize the low-frequency oscillation present in the flowfield about an NACA 0012 airfoil with a horn-ice shape. This low-frequency mode was identified in the unsteady content of the airfoil lift coefficient and the corresponding Strouhal numbers compared well with those reported in the literature. To study the relationship between the ice-induced separation bubble dynamics and the airfoil circulation, the unsteady shear-layer reattachment location was determined using measurements from a surface-mounted hot-film array. At the low-frequency mode, the lift coefficient led the reattachment location by a phase of /2. Additional characterization of the relationship between the unsteady shear-layer reattachment location and the unsteady airfoil pressure distribution was also completed, along with an analysis of the convective qualities of the low-frequency oscillation throughout the airfoil pressure distribution.
机译:风洞测量被用于识别和表征流场中存在的具有角冰形状的NACA 0012机翼周围的低频振荡。这种低频模式可以通过机翼升力系数的不稳定含量和相应的Strouhal数来确定,与文献报道的结果相比是很好的。为了研究冰引起的分离气泡动力学与翼型循环之间的关系,使用表面贴装热膜阵列的测量值确定了不稳定的剪切层重新附着位置。在低频模式下,升力系数使重新固定位置领先相位/ 2。还完成了非定常剪切层重装位置与非定常翼型压力分布之间关系的附加表征,并分析了整个翼型压力分布中低频振荡的对流性质。

著录项

  • 来源
    《AIAA Journal》 |2015年第3期|629-637|共9页
  • 作者单位

    Univ Illinois, Dept Aerosp Engn, Urbana, IL 61801 USA;

    Univ Illinois, Dept Aerosp Engn, Urbana, IL 61801 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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