论文标题
冲击波/湍流边界层相互作用的低频不稳定机制在向后的步骤上
Low-frequency unsteadiness mechanisms in shock wave/turbulent boundary layer interactions over a backward-facing step
论文作者
论文摘要
在$ ma = 1.7 $和$ re_ \ infty = 1.3718 \ times 10^5 $的湍流中,低频不稳定的动作(bfs)是在湍流中的,使用良好的大型模拟(LES)进行了研究。瞬时流场说明了冲击波/边界层相互作用(SWBLI)系统的不稳定现象,包括剪切层中的涡旋脱落,分离气泡的冲击和呼吸的拍打动作,墙壁附近的流向条纹的呼吸,墙壁和弧形的弧形涡流和弧形的涡旋旋转在分离式的湍流边界层中。光谱分析表明,系统的低频行为与冲击波和分离的剪切层之间的相互作用有关,而中频运动与剪切层涡流的脱落有关。使用三维动态模式分解(DMD),我们分析了所选模式对重新接触区域周围冲击和流式旋转涡流的不稳定的单个贡献。 görtler样涡流是由源自重新触及区域中流线强曲率的离心力引起的,它与当前BFS病例中的低频不稳定密切相关。我们的DMD分析以及与相同但层流的相同情况的比较提供了证据,表明这些不稳定的görtler样涡流受到传入边界层波动的影响。与平板和坡道配置中的SWBLI相比,我们观察到低频模式的非二维频率(基于分离长度)。
The low-frequency unsteady motions behind a backward-facing step (BFS) in a turbulent flow at $Ma=1.7$ and $Re_\infty=1.3718\times 10^5$ is investigated using a well-resolved large-eddy simulation (LES). The instantaneous flow field illustrates the unsteady phenomena of the shock wave/boundary layer interaction (SWBLI) system, including vortex shedding in the shear layer, the flapping motions of the shock and breathing of the separation bubble, streamwise streaks near the wall and arc-shaped vortices in the turbulent boundary layer downstream of the separation bubble. A spectral analysis reveals that the low-frequency behaviour of the system is related to the interaction between shock wave and separated shear layer, while the medium-frequency motions are associated with the shedding of shear layer vortices. Using a three-dimensional dynamic mode decomposition (DMD), we analyse the individual contributions of selected modes to the unsteadiness of the shock and streamwise-elongated vortices around the reattachment region. Görtler-like vortices, which are induced by the centrifugal forces originating from the strong curvature of the streamlines in the reattachment region, are strongly correlated with the low-frequency unsteadiness in the current BFS case. Our DMD analysis and the comparison with an identical but laminar case provide evidence that these unsteady Görtler-like vortices are affected by fluctuations in the incoming boundary layer. Compared to SWBLI in flat plate and ramp configurations, we observe a slightly higher non-dimensional frequency (based on the separation length) of the low-frequency mode.