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Numerical Simulations of hypersonic boundary-layer instability with localized roughness

机译:具有局部粗糙度的高超声速边界层失稳的数值模拟

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The effect of localized roughness on a Ma=4.8 boundary-layer and its instability is investigated by means of unsteady direct numerical simulations. The occurrence of special flow features, such as shocks, boundary-layer separation zones, streamwise vortices and streamwise streaks behind a three-dimensional square-shaped roughness element are discussed. In order to investigate the convective instability of the boundary layer downstream of the roughness, the steady-state flow field with roughness element has been perturbed with a small-amplitude perturbation of fixed frequency upstream of the element. The transformation of a first-mode instability wave upstream of the roughness into a strongly growing localized perturbation downstream of the square-shaped roughness is observed. Preliminary results for an oblique roughness are compared to results obtained for the square-shaped roughness.
机译:通过非稳态直接数值模拟研究了局部粗糙度对Ma = 4.8边界层及其不稳定性的影响。讨论了特殊流动特征的发生,例如激波,边界层分离区,在三维方形粗糙元素后面的沿流涡旋和沿流条纹。为了研究粗糙度下游边界层的对流不稳定性,对带有粗糙度单元的稳态流场进行了扰动,并对该单元的上游进行了固定频率的小幅度扰动。观察到粗糙度上游的第一模式不稳定性波转换为方形粗糙度下游的强烈增长的局部扰动。将斜粗糙度的初步结果与方形粗糙度的结果进行比较。

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