首页> 外文会议>Congress of the International Council of the Aeronautical Sciences >AN EXPERIMENTAL STUDY OF A PULSED AIR JET AND AN ACOUSTIC SYNTHETIC JET ON A LOW SPEED TURBULENT BOUNDARY LAYER
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AN EXPERIMENTAL STUDY OF A PULSED AIR JET AND AN ACOUSTIC SYNTHETIC JET ON A LOW SPEED TURBULENT BOUNDARY LAYER

机译:低速湍流边界层上脉冲空气射流和声学合成射流的实验研究

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This experimental study compares the effectiveness of steady and pulsed air jet vortex generators (AJVGs) with an acoustic synthetic jet. The results showed that: ⅰ) The flow physics associated with the formation of the boundary later embedded streamwise vortices by steady AJVG blowing is different to that occurring with corresponding pulsed air jet blowing, where a well defined vortex does not appear to be forming. This supports the view that the physical mechanism involved with pulsed air jets involves the formation of a "train" of discrete vortical structures which locally promotes significant levels of mixing and boundary layer re-energization, ⅱ) Acoustic synthetic jets, at least using the technology employed in this study, cannot cause the large scale distortions of turbulent boundary layers in moderate to high speed flows which are seen with AJVG blowing and are known to be effective in promoting the high levels of mixing necessary for the re-energization of turbulent boundary layers.
机译:这项实验研究比较了稳定的和脉冲的空气喷射涡流发生器(AJVG)与声学合成射流的有效性。结果表明:ⅰ)与通过稳定的AJVG吹气形成边界后来嵌入的流状涡流相关的流动物理学与相应的脉冲空气喷射吹气所发生的流物理学不同,在这种情况下,似乎没有形成明确定义的涡流。这支持以下观点:与脉冲空气射流有关的物理机制涉及形成离散涡旋结构的“序列”,从而局部促进显着水平的混合和边界层的重新通电。,)至少使用该技术的声学合成射流在这项研究中使用的方法,不会引起中速到高速流动中湍流边界层的大规模变形,这在AJVG吹气中可以看到,并且已知可以有效地促进湍流边界层重新通电所需的高混合水平。

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