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首页> 外文期刊>Experimental Thermal and Fluid Science: International Journal of Experimental Heat Transfer, Thermodynamics, and Fluid Mechanics >Experimental study of interaction between supersonic duct flow and jets surrounded by the porous cavity
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Experimental study of interaction between supersonic duct flow and jets surrounded by the porous cavity

机译:超声速风管流与多孔腔包围射流相互作用的实验研究

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In the experiments, the effect of the combination of jets and a porous cavity on the flow field is studied by means of visualization of schlieren method and the measurements of wall static pressures and the flow direction in the cavity with the thermal tuft probe which is introduced in this paper. These measurements are performed simultaneously, which allow us to evaluate the effect of the jets and the porous cavity. Three cases for the jet arrangements are tested in this experiments. That is (1) no-jets issued only with a porous wall as a reference, (2) a single jet at the middle of the porous region, and (3) three jets in the porous region aligned spanwise to the main flow. As a result, the thermal tuft probe in the cavity is found to be non-disturbing detecting device to the whole flow field according to the shock locations and the wall static pressure measurements. It is also found that the flow direction in the cavity is greatly influenced by the starting shock wave and jet arrangements. The flow direction at the measurement positions in the cavity is always opposite to the main flow, as long as the starting shock wave is located upstream region of the porous wall for all jet patterns as well as the no-jets case. Moreover, in case that the starting shock wave exists downstream of the porous region, that is, the state of the main flow in the porous wall region is supersonic state, the flow direction in the cavity continues to be opposite to the main flow for a single jet issued at the middle of the porous wall. The results in this paper show that the combination of the jets and the porous cavity affects the shock positions and the flow direction in the cavity, which could be one of the promising techniques for the control of the flow field.
机译:在实验中,通过采用谢利伦方法的可视化以及引入的热簇绒探针对壁静压力和腔内流动方向的测量,研究了射流和多孔腔的组合对流场的影响。在本文中。这些测量是同时进行的,这使我们能够评估射流和多孔腔的效果。在本实验中测试了三种喷射装置的情况。即(1)仅以多孔壁作为参考的无喷嘴;(2)在多孔区域的中部的单个喷嘴;(3)在多孔区域中与主流呈展向排列的三个喷嘴。结果,根据冲击位置和壁静压力测量结果,发现腔中的热簇绒探头是整个流场的无干扰检测装置。还发现,腔中的流动方向受到起始冲击波和射流布置的很大影响。只要在所有射流模式和无射流情况下,起始冲击波位于多孔壁的上游区域,空腔中测量位置处的流动方向始终与主流相反。此外,如果起始冲击波存在于多孔区域的下游,也就是说,多孔壁区域中主流的状态为超音速状态,则腔体中的流动方向继续与主流方向相反。在多孔壁的中间发出单次喷射。结果表明,射流和多孔腔的结合会影响腔内的激波位置和流向,这可能是控制流场的有前途的技术之一。

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