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LES Study on the Mechanism of Vortex Rings behind Supersonic MVG with Turbulent Inflow

机译:超声速mVG背后涡环机理的LEs研究   湍流流入

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摘要

In this study, we investigate the interaction between vortex rings behind MVGand the oblique shocks in the MVG controlled ramp flow at M=2.5 and Req=5760.Implicit large eddy simulation (ILES) method is used by solving the unfilteredform of the Navier-Stokes equations with the 5th order Bandwidth-optimized WENOscheme. The fully developed inflow is given by a series of turbulent profilesobtained from previous DNS simulation. It shows that the ring structure doesnot break down and keeps its topology after penetrating the strong shock waveand the oblique shocks is influenced a lot by the induced flow field fromrings. The bump of the 3D shock wave surface is discovered and its mechanism isexplained.
机译:在这项研究中,我们研究了MVG后面的涡流环与MVG控制的斜波在M = 2.5和Req = 5760时的斜激波之间的相互作用。通过求解Navier-Stokes的未滤波形式,使用了隐式大涡模拟(ILES)方法具有5阶带宽优化的WENOscheme的方程。充分发展的流入是由先前DNS模拟获得的一系列湍流剖面给出的。结果表明,环结构在穿透强冲击波后不会破坏并保持其拓扑结构,而倾斜冲击受到环流场的影响很大。发现了3D冲击波表面的凹凸并解释了其机理。

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