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首页> 外文期刊>Journal of the American Helicopter Society >Fluid Dynamics of the Helicoidal Wake Sheets Trailed from a Hovering Rotor
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Fluid Dynamics of the Helicoidal Wake Sheets Trailed from a Hovering Rotor

机译:悬停转子尾迹的螺旋尾波板的流体动力学

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摘要

High-resolution particle image velocimetry (PIV) masurements were made to understand the behavior of the helicoidal wake sheets trailed by a rotor system, with and without blade twist. PIV measurements were made in hover at two representative blade loading coefficients. The wake sheets were initially laid down behind the span of the blades as small-scale, counterrotating vortical pairs of unequal strengths. This initial concentrated vorticity, however, quickly diffused into zones of concentrated turbulence, which progressively became a significant source of overall turbulence in the downstream rotor wake. Several types of fluid dynamics were documented inside the rotor wake, including interactions of the sheets with the tip vortices, which depended on both blade twist and rotor thrust. At earlier wake ages, a wave was seen to form on the wake sheets, although the growth of wave amplitude was limited as the sheets were stretched in the downstream wake.
机译:进行了高分辨率粒子图像测速(PIV)测量,以了解在有或没有叶片扭曲的情况下,由转子系统​​拖尾的螺旋尾流板的性能。悬停在两个代表性叶片载荷系数下进行PIV测量。尾流片最初以小规模,反向旋转的不等强度的涡旋对形式放置在叶片跨度后面。然而,最初的集中涡旋迅速扩散到集中湍流区域,逐渐成为下游转子尾流中总体湍流的重要来源。在转子尾流内部记录了几种类型的流体动力学,包括薄板与尖端涡旋的相互作用,这取决于叶片扭曲和转子推力。在较早的尾流时代,虽然尾波在下游尾流中拉伸时波幅的增长受到限制,但在尾流片层上仍会形成波浪。

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  • 来源
    《Journal of the American Helicopter Society》 |2016年第1期|012002.1-012002.17|共17页
  • 作者单位

    Univ Maryland, Dept Aerosp Engn, College Pk, MD 20742 USA|US Naval Acad, Annapolis, MD 21402 USA;

    Univ Maryland, Dept Aerosp Engn, College Pk, MD 20742 USA|Embry Riddle Aeronaut Univ, Daytona Beach, FL USA;

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  • 正文语种 eng
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