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Large eddy simulation of film cooling flow from converging slot-holes

机译:换槽孔的薄膜冷却流的大涡流模拟

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AbstractLarge eddy simulation (LES) was performed for film cooling from converging slot-holes (consoles) at different blowing ratio ofM?=?1.0–3.0, and the Reynolds number,Re?=?21719, based on the mainstream velocity and inlet hole diameter. In time-averaged flow fields of film cooling, counter-rotating vortex pairs (CRVPs) and anti-CRVPs are dominant structures. CRVPs result in the deterioration of film cooling performance, while the effect of anti-CRVPs is opposite. Instantaneous coherent structures for consoles including jet vortex pairs, anti-jet vortex pairs, hairpin vortexes, and leading- and trailing-edge vortexes were analyzed in detail. Jet vortex pairs are firstly generated in consoles, and then enter the mainstream channel, finally evolve into hairpin vortexes. The head, horizontal leg and vertical leg of hairpin vortexes correspond to roller vortexes, CRVPs and upright wake vortexes respectively. Anti-jet vortex pairs are the sources of anti-CRVPs. By time-frequency analysis of pressure signals, it was found that the signals from downstream of the hole centerline exhibit periodicity. The dominant frequency always increases with the increase of the blowing ratio, however, the corresponding amplitude of power spectrum increases firstly, and then decreases.]]>
机译:<![CDATA [ 抽象 对从不同吹风比的换槽孔(控制台)的薄膜冷却进行了大型涡流仿真(LES) m ?=?1.0-3.0,以及雷诺数, re ?=?21719,基于主流速度和入口孔直径。在薄膜冷却的时间平均流场中,反向旋转涡流对(CRVP)和防CRVP是显性结构。 CRVP导致薄膜冷却性能的恶化,而抗CRVP的效果相反。详细分析了包括喷射涡流对,抗射流涡旋对,发夹涡旋和引导和后边缘涡旋的瞬时相干结构。首先在控制台中生成Jet Vortex对,然后进入主流通道,最后进化到发夹涡旋中。发夹涡旋的头部,水平腿部和垂直腿分别对应于滚子涡旋,CRVPS和直立爪涡旋。防射流涡旋对是抗CRVP的来源。通过压力信号的时频分析,发现来自孔中心线下游的信号表现出周期性。主导频率随着吹出比率的增加而始终增加,但是,相应的功率谱首先增加,然后减少。 ]]>

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