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Numerical, Experimental and Theoretical Studies on Mechanism of K-H Instability and Ring Generation behind Supersonic MVG

机译:超音速MVG产生K-H失稳和环生成机理的数值,实验和理论研究

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This paper illustrates the dominant mechanism of the ring-like vortex formation which was found generated by micro vortex generated (MVG) for shock-boundary layer interaction control by our implicit large eddy simulation (ILES) with high order accuracy and our experiment. An averaged velocity profile after MVG is taken as the base flow. The disturbed viscous incompressible and inviscit compressible stability equations have been derived in a 3D coordinates, axially symmetric in particular. After we introduced the effect of simplified spanwise counter-rotating vortices, we theoretically conclude that the structure of vortex rings behind the MVG is a consequence of the momentum deficit according to the axisymmetic instability theorem.
机译:本文通过隐式大涡模拟(ILES)和高阶精度实验,说明了由微涡产生(MVG)产生的环状涡形成的主要机理,该微涡产生了用于冲击边界层相互作用的控制。 MVG之后的平均速度曲线作为基本流量。已在3D坐标(尤其是轴向对称)中导出了扰动的粘性不可压缩和无粘性可压缩稳定性方程。在介绍了简化的展向方向反向旋转涡流的影响之后,我们从理论上得出结论,根据轴对称不稳定性定理,MVG后面的涡流环结构是动量不足的结果。

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