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首页> 外文期刊>Journal of engineering mathematics >Transition to turbulence in rotating-disk boundary layers-convective and absolute instabilities
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Transition to turbulence in rotating-disk boundary layers-convective and absolute instabilities

机译:转盘边界层的湍流过渡-对流和绝对不稳定性

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This work is an experimental study of mechanisms for transition to turbulence in the boundary layer on a rotating disk. In one case, the focus was on a triad resonance between pairs of traveling cross-flow modes and a stationary cross-flow mode. The other was on the temporal growth of traveling modes through a linear absolute instability mechanism first discovered by Lingwood (1995, J Fluid Mech 314:373-405). Both research directions made use of methods for introducing controlled initial disturbances. One used a distributed array of ink dots placed on the disk surface to enhance a narrow band of azimuthal and radial wave numbers of both stationary and traveling modes. The size of the dots was small so that the disturbances they produce were linear. Another approach introduced temporal disturbances by a short-duration air pulse from a hypodermic tube located above the disk and outside the boundary layer. Hot-wire sensors primarily sensitive to the azimuthal velocity component, were positioned at different spatial (r,θ) locations on the disk to document the growth of disturbances. Spatial correlation measurements were used with two simultaneous sensors to obtain wavenumber vectors. Cross-bicoherence was used to identify three-frequency phase locking. Ensemble averages conditioned on the air pulses revealed wave packets that evolved in time and space. The space-time evolution of the leading and trailing edges of the wave packets were followed past the critical radius for the absolute instability, r_(c/A). With documented linear amplitudes, the spreading of the disturbance wave packets did not continue to grow in time as r_(c/A) was approached. Rather, the spreading of the trailing edge of the wave packet decelerated and asymptotically approached a constant. This result supports the linear DNS simulations of Davies and Carpenter (2003, J Fluid Mech 486:287-329) who concluded that the absolute instability mechanism does not result in a global mode, and that linear-disturbance wave packets are dominated by the convective instability. In contrast, wave-number matching between traveling cross-flow modes confirmed a triad resonance that lead to the growth of a low azimuthal number (n = 4) stationary mode. At transition, this mode had the largest amplitude. Signs of this mechanism can be found in past flow visualization of transition to turbulence in rotating disk flows.
机译:这项工作是对转盘边界层内湍流过渡机制的实验研究。在一种情况下,重点是在成对的错流模式和平稳错流模式之间的三重共振。另一种是通过线性绝对不稳定性机制在行进模态的时间增长上进行的,该机制最初由Lingwood(1995,J Fluid Mech 314:373-405)发现。这两个研究方向都利用了引入受控初始扰动的方法。一种方法是使用分布在磁盘表面上的墨点分布阵列来增强固定模式和行进模式的窄范围的方位角和径向波数。点的大小很小,因此它们产生的干扰是线性的。另一种方法是通过来自磁盘上方且位于边界层外部的皮下注射管的短时空气脉冲引入时间干扰。主要对方位速度分量敏感的热线传感器位于磁盘上的不同空间(r,θ)位置,以记录干扰的增长。空间相关性测量与两个同时使用的传感器一起使用以获得波数矢量。交叉双相干用于识别三相锁相。以空气脉冲为条件的集合平均值揭示了随时间和空间演化的波包。波包的前缘和后缘的时空演化都经过了绝对不稳定性r_(c / A)的临界半径。在记录的线性振幅下,随着接近r_(c / A),干扰波包的扩散不会随时间继续增长。而是,波包的后缘的扩展被减速并且渐近地接近常数。该结果支持Davies和Carpenter(2003,J Fluid Mech 486:287-329)的线性DNS模拟,他们得出结论,绝对不稳定机制不会导致整体模式,并且线性扰动波包受对流控制不稳定。相反,行进的横流模式之间的波数匹配证实了三重共振,从而导致低方位角数(n = 4)平稳模式的增长。在过渡时,该模式具有最大振幅。这种机制的迹象可以在旋转圆盘流中的过渡到湍流的过去流可视化中找到。

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