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Investigation of Flow Characteristics in Supersonic Cavity Using LES

机译:利用LES研究超声速腔内的流动特性

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The formation of large scale structures for the supersonic flow over a rectangular cavity is studied using Large Eddy Simulation (LES) and Proper Orthogonal Decomposition (POD), while the sub-grid scales (SGS) are modelled using dynamic Smagorinsky model. The Pressure distribution along the cavity walls obtained through the simulation is in good agreement with the empirical results presented in [1]. The Isosurfaces of Q show the evolution of structures inside as well as in the wake of the cavity. The contours of vorticity magnitude clearly show the flapping of the shear layer which is responsible for the generation of a feedback mechanism in the cavity. The density gradient contours show the propagation of transverse as well as longitudinal waves from the cavity. The large scale vortical structures in the mid plane along with the bending of the flow inside the cavity are captured by the POD basis functions.
机译:使用大涡模拟(LES)和适当的正交分解(POD)研究了矩形腔上超音速流动的大型结构的形成,而使用动态Smagorinsky模型对子网格尺度(SGS)进行了建模。通过模拟获得的沿腔壁的压力分布与[1]中给出的经验结果非常吻合。 Q的等值面显示了腔体内以及腔体内部结构的演变。涡度大小的轮廓清楚地显示出剪切层的拍打,这负责在空腔中产生反馈机制。密度梯度等值线显示了来自腔的横向波和纵向波的传播。 POD基函数可捕获中平面的大型旋涡结构以及空腔内部流动的弯曲。

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