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Mechanisms of interaction between stationary crossflow instabilities and forward-facing steps

机译:静止跨流量不稳定性与正面步骤之间的交互机制

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We study the interaction between a stationary crossflow instability and forward-facing steps in a swept-wing boundary layer using Direct Numerical Simulations (DNS). The stationary primary crossflow mode is imposed at the inflow. Steps of several heights are modeled. Particular emphasis is placed on ensuring a fully stationary solution, in order to isolate the modulation of the primary instability at the step and the generation of stationary secondary perturbations. The main features of the base flow are step-induced flow reversal and secondary inflection points. When approaching the step, the incoming crossflow instability lifts up and passes over it. Additional perturbation streaks arise, which are accompanied by secondary stationary vortices that have the same spanwise wavenumber as the fundamental crossflow disturbance. For sufficiently high steps, secondary perturbation structures attain amplitude values comparable in magnitude to primary instability in the vicinity of the step. We propose metrics to quantify the impact of the step on the development of the crossflow disturbance upon interaction. Considering energy-based criteria, we find that the crossflow perturbation is amplified upstream of the step. Interestingly, the incoming primary crossflow instability undergoes strong stabilization immediately downstream of the largest step. The mechanisms revealed in this work provide a first insight into the possible causes of transition on swept wings due to forward-facing steps.
机译:我们使用直接数值模拟(DNS)研究扫翼边界层中的静止交叉流出不稳定性和面对前部步骤之间的相互作用。静止的主横流模式施加在流入中。建模几个高度的步骤。特别强调确保完全固定的解决方案,以分离在步骤中的初级不稳定性和静止的二级扰动的产生。碱基流的主要特征是阶梯诱导的流动反转和次要拐点。在接近步骤时,传入的Crossflow不稳定升高并通过它。出现额外的扰动条纹,其伴随着具有与基本跨流干扰相同的翼展波数的二级固定涡流。对于足够高的步骤,二次扰动结构在步骤附近的初始不稳定性的幅度上获得相当的幅度值。我们提出指标来量化步骤对互动时交叉流扰动的发展的影响。考虑到基于能量的标准,我们发现跨流扰动在步骤的上游扩增。有趣的是,传入的主要跨流量不稳定性在最大步骤下行的下游发生强烈稳定性。在本工作中揭示的机制提供了对由于前后步骤引起的扫过翼的可能原因的第一洞察力。

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