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A class of exact Navier-Stokes solutions for homogeneous flat-plate boundary layers and their linear stability

机译:一类均质平板边界层的精确Navier-Stokes解及其线性稳定性

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We introduce a new boundary layer formalism on the basis of which a class of exact solutions to the Navier-Stokes equations is derived. These solutions describe laminar boundary layer flows past a flat plate under the assumption of one homogeneous direction, such as the classical swept Hiemenz boundary layer (SHBL), the asymptotic suction boundary layer (ASBL) and the oblique impingement boundary layer. The linear stability of these new solutions is investigated, uncovering new results for the SHBL and the ASBL. Previously, each of these flows had been described with its own formalism and coordinate system, such that the solutions could not be transformed into each other. Using a new compound formalism, we are able to show that the ASBL is the physical limit of the SHBL with wall suction when the chordwise velocity component vanishes while the homogeneous sweep velocity is maintained. A corresponding non-dimensionalization is proposed, which allows conversion of the new Reynolds number definition to the classical ones. Linear stability analysis for the new class of solutions reveals a compound neutral surface which contains the classical neutral curves of the SHBL and the ASBL. It is shown that the linearly most unstable G?rtler-H?mmerlin modes of the SHBL smoothly transform into Tollmien-Schlichting modes as the chordwise velocity vanishes. These results are useful for transition prediction of the attachment-line instability, especially concerning the use of suction to stabilize boundary layers of swept-wing aircraft.
机译:我们介绍了一种新的边界层形式主义,在此基础上,得出了Navier-Stokes方程的一类精确解。这些解决方案描述了层流边界层在一个均匀方向的假设下流过平板的情况,例如经典的扫掠海门兹边界层(SHBL),渐近吸力边界层(ASBL)和倾斜撞击边界层。研究了这些新解决方案的线性稳定性,发现了SHBL和ASBL的新结果。以前,已经用自己的形式主义和坐标系描述了这些流程中的每一个,因此解决方案无法相互转化。使用新的复合形式主义,我们能够证明当弦向速度分量消失而保持均匀扫掠速度时,ASBL是壁吸力作用下SHBL的物理极限。提出了相应的无量纲化方法,该方法可以将新的雷诺数定义转换为经典的雷诺数定义。新型溶液的线性稳定性分析显示了复合中性表面,其中包含SHBL和ASBL的经典中性曲线。结果表明,随着弦速的消失,SHBL线性最不稳定的G?rtler-H?mmerlin模式平稳地转变为Tollmien-Schlichting模式。这些结果可用于过渡线不稳定性的过渡预测,特别是在使用吸力来稳定后掠飞机边界层时。

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