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Analysis of pressure fluctuation in transonic cavity flows using modal decomposition

机译:利用模态分解分析跨音速腔流中的压力波动

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Turbulent flows at a free stream Mach number of 1.19 over an open cavity with L/D ratio of 5.0 are numerically investigated using improved delayed detached-eddy simulation based on two-equation shear stress transport model. Modal decompositions including proper orthogonal decomposition (POD) and dynamic mode decomposition (DMD) are applied to analyze the pressure fluctuations. The extracted first six POD modes possess more than 75% of the total energy and contain multiple frequencies. Their spatial structures exhibit well regular and periodic behaviors along the cavity lip line. The DMD algorithm identifies the flow structures associated with single frequencies. Major distribution areas of high intensity pressure fluctuations move upstream as the mode frequency increases, and the structures with high frequencies are prone to break down near the trailing edge. The alternating pressure patterns convection process is clearly presented, and the propagation of acoustic waves validates that the acoustic waves share the same sound source but are radiated following two different paths, consistent with the feedback mechanism. In addition, the effects of free stream Reynolds number on sound pressure spectrum levels are investigated at a fixed pressure and temperature. Results show that free stream Reynolds number has no effect on the non-dimensional frequencies of the dominant modes, while the main recirculation area shrinks as Reynolds number increases. Furthermore, variations of sound pressure levels as a function of Reynolds numbers exhibit significant discrepancies for a fixed free stream pressure or temperature, indicating that the Reynolds number is not critical to the feedback tone amplitude. The enhancement of sound pressure levels mainly attributes to the increment of free flow pressure or the impingement of enlarged fluid velocity due to higher free stream temperature. (C) 2018 Elsevier Masson SAS. All rights reserved.
机译:使用改进的基于两个方程的剪切应力传递模型的延迟分离涡模拟,以自由流马赫数为1.19的自由流马赫数在L / D比为5.0的情况下进行了数值研究。应用包括适当正交分解(POD)和动态模式分解(DMD)在内的模态分解来分析压力波动。提取的前六个POD模式拥有总能量的75%以上,并包含多个频率。它们的空间结构沿腔唇线表现出良好的规则和周期性行为。 DMD算法识别与单个频率关联的流结构。随着模式频率的增加,高强度压力波动的主要分布区域向上游移动,而具有高频率的结构易于在后缘附近分解。清晰地显示了交替的压力模式对流过程,并且声波的传播验证了声波共享相同的声源,但沿着两条不同的路径辐射,这与反馈机制一致。此外,在固定压力和温度下研究了自由流雷诺数对声压谱水平的影响。结果表明,自由流雷诺数对主导模的无量纲频率没有影响,而主循环面积随雷诺数的增加而减小。此外,声压级随雷诺数的变化对于固定的自由流压力或温度表现出明显的差异,这表明雷诺数对于反馈音调幅度并不关键。声压级的提高主要归因于自由流动压力的增加或由于较高自由流温度而导致流体速度增大的影响。 (C)2018 Elsevier Masson SAS。版权所有。

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