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2D AND 3D STABILITY OF CAVITY FLOWS IN HIGH MACH NUMBER REGIMES

机译:高MACH数型腔中的2D和3D稳定性

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The stability characteristics of an open cavity flow at very high Mach number are examined with BiGlobal stability analysis based on the eigenvalues of the linearized Navier-Stokes equations. During linearization, all possible first-order terms are retained without any approximation, with particular emphasis on extracting the effects of compressibility on the flowfield. The method leverages sparse linear algebra and the implicitly restarted shift-invert Arnoldi algorithm to extract eigenvalues of practical physical consequence. The stability dynamics of cavity flows at four Mach numbers between 1.4 and 4 are considered at a Reynolds number of 502. The basic states are obtained through Large Eddy Simulation (LES). Frequency results from the stability analysis show good agreement when compared to the theoretical values using Rossiter's formula. An examination of the stability modes reveals that the shear layer is increasingly decoupled from the cavity as the Mach number is increased. Additionally, the outer lobes of the Rossiter modes are observed to get stretched and tilted in the direction of the freestream. Future efforts will extend the present analysis to examine current and potential cavity flame holder configurations, which often have downstream walls inclined to the vertical.
机译:基于线性化的Navier-Stokes方程的特征值,通过BiGlobal稳定性分析,研究了在非常高的马赫数下的开腔流动的稳定性特征。在线性化过程中,所有可能的一阶项都被保留而没有任何近似值,特别强调提取可压缩性对流场的影响。该方法利用稀疏线性代数和隐式重启的移位-反转Arnoldi算法来提取实际物理结果的特征值。雷诺数为502时,考虑了四个马赫数在1.4和4之间的空腔流动的稳定性动力学。基本状态是通过大涡模拟(LES)获得的。与使用Rossiter公式的理论值相比,稳定性分析的频率结果显示出良好的一致性。对稳定性模式的检查表明,随着马赫数的增加,剪切层与空腔的分离越来越多。此外,观察到Rossiter模式的外部波瓣在自由流方向上拉伸和倾斜。未来的工作将扩展本分析,以检查当前和潜在的腔体火焰保持器配置,这些配置通常使下游壁向垂直方向倾斜。

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