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Numerical Investigation of Passive Flow Control Using Permeable and Wavy Walls in Oblique Shock-Wave/Boundary-Layer Interaction

机译:倾斜冲击波/边界层交互中渗透和波浪壁的无源流量控制的数值研究

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This work investigates the effect of a porous medium/permeable wall in the region of flow separation induced by an impinging oblique shock/boundary-layer interaction (SBLI) at Mach 2.0 using 2D numerical simulations. The study presented here includes an investigation of cases with no control, with permeable walls, and wavy non-permeable walls with varying waviness. The effect of the position and extent of the permeable wall is also investigated. The porous region is modeled as a cavity filled with a square array of circular cylinders (rendered as circles in 2D). The computations are performed using a parallel, finite-volume solver for compressible flows on structured grids. An immersed-boundary method is used to represent the porous region. Menter's k - to SST model is used to model turbulence. Results are presented using pressure contours (to reveal shock structure), streamline patterns, and near-surface velocity and pressure. It is observed from the plots that the limiting case of a non-permeable wall produces better results compared to the permeable wall, indicating that passive blowing (from) and suction (into) the permeable wall does not produce the desired effect of energizing the boundary layer and mitigating flow separation in this case.
机译:该工作研究了多孔介质/可渗透壁在通过2D数值模拟的Mach 2.0中撞击倾斜冲击/边界层相互作用(SBLI)引起的流动分离区域的效果。此处提出的研究包括对没有控制的情况的病例,具有可渗透的壁和波状不渗透壁,具有不同的波纹。还研究了可渗透壁的位置和程度的效果。多孔区域被建模为填充有圆柱形圆柱形的腔体(作为2D中的圆形呈现)。使用并行的有限音量求解器进行计算,用于在结构化网格上的可压缩流。浸没边界方法用于表示多孔区域。导师的K - 至SST模型用于模拟湍流。使用压力轮廓(露出震动结构),流线图案和近表面速度和压力来提出结果。从图中观察到不透水壁的限制壳体与可渗透壁相比产生更好的结果,表明被动吹塑(来自)和吸入(进入)可渗透壁不会产生激励边界的所需效果在这种情况下层和减轻流动分离。

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