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Towards the characterization of micro vortex generators effects on shock wave / turbulent boundary layer interaction using LES

机译:为了表征微涡发生器,利用LES对冲击波/湍流边界层相互作用的影响

摘要

We perform Large Eddy Simulations (LES) of the experimental configuration by Wang et al. (2012): a rake of microramp vortex generators (MVGs) were inserted upstream the SWTBLI. The configuration features MVGs protruding by 0.47 delta in a TBL at M = 2.7 and Re_theta = 3600. We first validate the flow solver and LES strategy on a baseline configuration without control and we retrieve the characteristic length scales and the low frequency motion (StL = 0.03) of the reflected shock foot. The configuration with MVGs exhibits successive regions alternating between either momentum deficit or momentum excess downstream the MVGs, with good agreement with the experiments. Classical wake recovery laws were retrieved as well as the frequency of St = 0.53 characteristic of the shedding of intermittent structures downstream the MVGs and we observe a significant 20% decrease of the separation bubble length.
机译:我们执行了Wang等人的实验配置的大涡模拟(LES)。 (2012年):在SWTBLI的上游插入了一系列微斜坡涡发生器(MVG)。配置的特征是MVG在TBL上以M = 2.7和Re_theta = 3600突出0.47增量。我们首先在没有控制的基准配置上验证流量求解器和LES策略,然后检索特征长度标度和低频运动(StL = 0.03)的反射冲击脚。带有MVG的配置在MVG的下游显示出连续的区域,这些区域在动量不足或动量过量之间交替变化,与实验吻合良好。检索了经典的尾流恢复定律以及MVG下游间歇结构脱落的St = 0.53的频率,我们观察到分离气泡长度显着减少了20%。

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