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Flow mechanism of bimodal phenomenon in intermittent corner separation in a linear compressor cascade using a hybrid RANS/LES method

机译:使用杂交rans方法在线性压缩机级联中间歇角分离中双峰现象的流动机制

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摘要

To gain a better knowledge of the bimodal phenomenon in intermittent corner separation, a hybrid RANS/LES turbulence model is applied to simulate the unsteady flow in a linear cascade. After the validation of the Stress Blended Eddy Simulation (SBES) model with the detailed experimental data, the flow mechanisms of intermittent coherent vortical structures and bimodal phenomenon are clarified according to unsteady numerical results. An indicator is proposed to evaluate the degree of the bimodal phenomenon. Firstly, the intermittency in corner separation is found, which arises from the formation of coherent vortical structures. The collision of the boundary layer and backflow near the trailing edge gives rise to large-scale coherent vortices around the separation surface. Then, according to the histogram of velocity probability density functions (PDF), the bimodal phenomenon found near the separation surface indicates that there are two non-periodic switching flow modes. Combination of vortical structures and velocity distributions manifests that the intermittency of coherent vortical structure is responsible for the switching flow modes around the separation surface. Thirdly, three characteristic parameters are defined to describe the features of two flow modes, corresponding to two Gaussian distributions that PDF decomposed into. The indicator Ra, which measures the difference between two flow modes, is used to evaluate the degree of the bimodal phenomenon. A larger Ra represents the higher probability of bimodal phenomenon occurring in flow fields, which can be used to quantitatively determine the position and fluctuation of the corner separation surface. (C) 2021 Elsevier Masson SAS. All rights reserved.
机译:为了更好地了解间歇角分离中的双峰现象,应用混合RANS湍流模型来模拟线性级联中的不稳定流动。在用详细的实验数据验证应力混合涡流模拟(SBE)模型之后,根据不稳定的数值结果澄清间歇相干涡流结构和双峰现象的流动机制。提出了一个指标来评估双峰现象的程度。首先,找到角落分离中的间歇性,从形成相干涡流结构中产生。后缘附近的边界层和回流的碰撞产生了分离表面周围的大规模相干涡流。然后,根据速度概率密度函数(PDF)的直方图,在分离表面附近发现的双峰现象表明存在两个非周期性开关流动模式。涡流结构和速度分布的组合表明,相干涡流的间歇性是对分离表面周围的开关流模式负责的负责。第三,定义了三个特征参数以描述两个流模式的特征,对应于PDF分解为的两个高斯分布。指标RA,测量两个流动模式之间的差异,用于评估双峰现象的程度。较大的RA表示流场中发生的双峰现象的概率较高,其可用于定量地确定角分离表面的位置和波动。 (c)2021 Elsevier Masson SAS。版权所有。

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  • 来源
    《Aerospace science and technology》 |2021年第10期|106949.1-106949.14|共14页
  • 作者单位

    Shanghai Jiao Tong Univ Sch Aeronaut & Astronaut 800 Dongchuan RD Minhang Dist Shanghai 200240 Peoples R China;

    Shanghai Jiao Tong Univ Sch Aeronaut & Astronaut 800 Dongchuan RD Minhang Dist Shanghai 200240 Peoples R China;

    Shanghai Jiao Tong Univ Sch Aeronaut & Astronaut 800 Dongchuan RD Minhang Dist Shanghai 200240 Peoples R China;

    Shanghai Jiao Tong Univ Sch Aeronaut & Astronaut 800 Dongchuan RD Minhang Dist Shanghai 200240 Peoples R China;

    Shanghai Jiao Tong Univ Sch Aeronaut & Astronaut 800 Dongchuan RD Minhang Dist Shanghai 200240 Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
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