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首页> 外文期刊>Studies in Applied Mathematics >Effects of suction on the nonstationary lower branch modes of a compressible boundary layer flow due to a rotating disk
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Effects of suction on the nonstationary lower branch modes of a compressible boundary layer flow due to a rotating disk

机译:吸力对旋转圆盘引起的可压缩边界层流的非平稳下部分支模态的影响

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In this paper, suction and injection effects are investigated theoretically on the structure of the lower branch neutral stability modes of three-dimensional small disturbances imposed on the compressible boundary layer flow due to a rotating disk. In a recent study [1], it was demonstrated that the short-wavelength stationaryonstationary compressible crossflow vortex modes at sufficiently high Reynolds numbers with reasonably small scaled frequencies can be described by an asymptotic expansion procedure as set up in [2] for the incompressible stationary modes, which rigorously takes into account the nonparallel effects. Employing this rational asymptotic technique, it is shown here that the wavenumber and the orientation of the compressible lower branch modes are governed by an eigenrelation that is under the strong influence of a suction/injection parameter (s) over bar, which, when set to zero, the relation turns out to be the one obtained previously by Turkyilmazoglu [1] for zero-suction compressible modes.The boundary layer growth contributes in the way of destabilizing all the modes, in particular for the compressible modes, though the wall cooling in the case of suction and the wall insulation and heating in the case of injection are found to persist to the destabilization for the modes in the vicinity of the stationary mode. From a linear stability analysis point of view, suction is found to be stabilizing, whereas injection enhances the instability as compared to the no suction through the surface of the disk. In both cases, positive frequency waves are found to be highly destabilized as compared to the waves having negative frequencies. The findings of the work are also fully supported after a comparison between the numerical results obtained from directly solving the linearized compressible system with a usual parallel flow approximation and the asymptotic compressible data obtained at a high Reynolds number.
机译:本文从理论上研究了由于旋转圆盘对可压缩边界层流动施加的三维小扰动的下支路中性稳定模式的结构的吸力和注入效应。在最近的一项研究中[1],证明了可以通过[2]中为该模型建立的渐近展开过程来描述足够高的雷诺数和合理的小比例频率下的短波固定/非平稳可压缩横流涡旋模式。不可压缩的平稳模式,严格考虑了非平行效应。利用这种有理渐近技术,此处表明,波数和可压缩下部分支模式的方向由本征关系控制,该本征关系受杆上吸/射参数的强烈影响,将其设置为零吸力可压缩模式的关系原来是由Turkyilmazoglu [1]获得的。边界层的增长以破坏所有模式的方式做出了贡献,特别是对于可压缩模式,尽管壁冷对于固定模式附近的模式,发现吸气和壁绝缘以及加热的情况持续不稳定。从线性稳定性分析的观点来看,发现吸力是稳定的,而与通过磁盘表面的无吸力相比,注入增强了不稳定性。在这两种情况下,与具有负频率的波相比,发现正频率波高度不稳定。在通过直接求解具有通常的平行流近似的线性化可压缩系统获得的数值结果与以高雷诺数获得的渐近可压缩数据进行比较之后,这项工作的发现也得到了充分支持。

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