2D and 3D Stability of Cavity Flows in High Mach Number Regimes

Parshwanath S. Doshi, R. Ranjan, D. Gaitonde
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Abstract

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.
高马赫数条件下腔体流动的二维和三维稳定性
采用基于线性化Navier-Stokes方程特征值的全局稳定性分析方法,研究了高马赫数下开腔流动的稳定性特性。在线性化过程中,保留了所有可能的一阶项,没有任何近似,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新启动移位逆Arnoldi算法来提取实际物理结果的特征值。考虑了在雷诺数为502时,在1.4 ~ 4马赫数范围内的空腔流动的稳定性动力学。通过大涡模拟(LES)获得了基本状态。稳定性分析的频率结果与Rossiter公式的理论值相比较,显示出良好的一致性。对稳定模态的研究表明,随着马赫数的增加,剪切层与腔体的去耦越来越大。此外,观察到罗西特模态的外叶在自由流的方向上被拉伸和倾斜。未来的努力将扩展目前的分析,以检查当前和潜在的腔火焰支架配置,通常下游壁倾斜到垂直方向。
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