SIMULATION OF THE RESONANT INTERACTIONS BETWEEN A BOUNDARY LAYER AND AN ARRAY OF DEEP CAVITIES

Grigory Shelekhov, J. Bodart, L. Joly
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引用次数: 1

Abstract

We have performed numerical simulations of the interaction between a laminar boundary layer flow and an array of deep slit-aperture cavities solving fully compressible Navier-Stockes equations with a finite-volume solver CharLESX . The cavities are included in the computational domain which allows to study the full interaction i.e. the excitation mechanism of the liner and its acoustic response. The parameter space is explored by varying the cavity depth D, thus shifting the cavity resonant modes fr,m = (2m− 1) c 4D , where m is a positive integer. Four cases, with varying cavity depth were studied. In all cases, the coupling of the grazing shear layer instabilities to the acoustic standing waves inside cavities (resonant interaction) leads to the generation of large Kelvin-Helmholtz (KH) rollers, scaling as λKH = Uc/ fr,1. In some cases, this coupling leads to the excitation of m > 1 resonant modes in the upstream cavities. However vortex merge occurring over the cavities switches the mode m = 1 further downstream. Overall, the results suggest that an array of deep cavities has a promising potential application for passive flow control.
边界层与深空腔阵列之间共振相互作用的模拟
本文利用有限体积求解器CharLESX对层流边界层流动与深缝孔空腔阵列之间的相互作用进行了数值模拟,求解了完全可压缩的Navier-Stockes方程。这些空腔包含在计算域中,从而可以研究衬垫的完全相互作用,即衬垫的激励机制及其声学响应。通过改变腔深D来探索参数空间,从而改变腔谐振模式fr,m = (2m−1)c 4D,其中m为正整数。研究了不同空腔深度的4个病例。在所有情况下,掠切层不稳定性与腔内声波驻波的耦合(共振相互作用)导致了大型开尔文-亥姆霍兹(KH)滚子的产生,其尺度为λKH = Uc/ fr,1。在某些情况下,这种耦合导致上游腔中m > 1谐振模式的激发。然而,在空腔上发生的涡旋合并使模态m = 1进一步下游。总之,研究结果表明,深空腔阵列在被动流动控制方面具有潜在的应用前景。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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