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Unsteady actuation of counter-flowing wall jets for gust load attenuation

机译:逆流壁式射流的不稳定驱动,以减轻阵风负荷

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摘要

Counter-flowing wall jets actuated on the upper surface of an airfoil are investigated for the purpose of controlling gust encounters. For periodic and transient actuations, phase-averaged lift force and particle image velocimetry measurements are presented for a NACA 0012 airfoil, at a Reynolds number of 660,000, for a range of reduced frequencies and three jet locations, x(j)/c = 0.08, 0.60 and 0.95. For periodic actuation, amplitude of lift oscillations decrease and phase delay increase with increasing reduced frequency. The effect of reduced frequency on the amplitude and phase is more significant for blowing locations near the leading-edge and with increasing angle of attack. Transient actuation reveals the slow response of the separated flow, and therefore lift, with the delay becoming more pronounced for blowing near the leading-edge. Estimated time constants are similar to previous observations for forced separation and reattachment. (C) 2019 Elsevier Masson SAS. All rights reserved.
机译:为了控制阵风,研究了在机翼上表面上产生的逆流壁射流。对于周期性和瞬态驱动,提出了NACA 0012机翼的雷诺数为660,000的相平均升力和粒子图像测速仪测量结果,用于一系列降低的频率和三个射流位置,x(j)/ c = 0.08 ,0.60和0.95。对于周期性致动,提升振动的幅度随着频率的减小而减小,而相位延迟则增大。频率降低对幅度和相位的影响对于前沿附近的吹气位置和迎角增加的情况更为明显。瞬态致动揭示了分离流的缓慢响应,因此产生了升力,并且随着在前缘附近吹动,延迟变得更加明显。估计的时间常数与以前关于强制分离和重新连接的观察结果相似。 (C)2019 Elsevier Masson SAS。版权所有。

著录项

  • 来源
    《Aerospace science and technology》 |2019年第6期|175-191|共17页
  • 作者单位

    Univ Bath, Dept Mech Engn, Bath BA2 7AY, Avon, England;

    Univ Bath, Dept Mech Engn, Bath BA2 7AY, Avon, England;

    Univ Bath, Dept Mech Engn, Bath BA2 7AY, Avon, England;

  • 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
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