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:该实验研究比较了用声学合成射流的稳态和脉冲喷射涡流发生器(AJVGS)的有效性。结果表明:Ⅰ)与边界的形成相关的流量物理通过稳定的AJVG吹塑的嵌入流动涡流与相应的脉冲空气喷射吹送的相应不同,其中良好定义的涡流似乎没有形成。这支持脉冲空气喷射所涉及的物理机制涉及形成离散涡流结构的“列车”,其局部促进显着水平的混合和边界层再通电,Ⅱ)声学合成喷射,至少使用该技术在本研究中使用,不能导致中等至高速流动中的湍流边界层的大规模扭曲,这是用AJVG吹制所看到的,并且已知有效地促进湍流边界层的再通电所需的高水平混合。

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