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The interaction of near-critical swirling flows in a pipe with inlet azimuthal vorticity perturbations

机译:管道中近临界旋流与入口方位涡度扰动的相互作用

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The interaction of a near-critical axisymmetric incompressible swirling flow in a straight pipe with small inlet azimuthal vorticity perturbations is studied. Certain flow conditions that may reflect the physical situation are prescribed along the pipe inlet and outlet. It is first demonstrated that under these conditions a regular-expansion solution in terms of the small azimuthal vorticity perturbations has a singular behavior around the critical swirl. This singularity infers that large-amplitude disturbances may be induced by the small perturbations when the incoming flow to the pipe has a swirl level around the critical swirl. In order to understand the nature of flows in this swirl range, a small-disturbance analysis is developed. It shows that under the prescribed inlet/outlet conditions, a small but finite inlet azimuthal vorticity perturbation breaks the transcritical bifurcation of solutions of the Euler equations at the critical swirl into two branches of perturbed solutions. When the azimuthal vorticity perturbations are positive these branches show a regular behavior. However, when they are negative, the perturbed branches fold at limit points near the critical swirl, with a finite gap between the two branches, and no near-columnar equilibrium state can exist for an incoming flow with swirl close to the critical level. The flow must develop large disturbances in this swirl range. Beyond this range, two equilibrium states may exist under the same inlet/outlet conditions. When the negative inlet vorticity perturbations become larger in their size, this special behavior uniformly changes into a branch of single equilibrium state for each incoming swirl. The relevance of the results to the appearance of the axisymmetric vortex breakdown in a pipe and the control of this phenomenon using inlet vorticity perturbations is also discussed. The results suggest that, in general, positive inlet azimuthal vorticity perturbations may be used to delay vortex breakdown to higher swirl levels whereas negative perturbations induce the appearance of vertex breakdown at levels below the critical swirl. (C) 1998 American Institute of Physics. [References: 27]
机译:研究了具有较小入口方位涡旋扰动的直管中近临界轴对称不可压缩旋流的相互作用。沿管道入口和出口规定了可能反映物理情况的某些流动条件。首先证明,在这些条件下,关于小方位涡旋扰动的正则展开解在临界涡旋周围具有奇异的行为。这种奇异性推断,当流入管道的气流在临界旋涡周围具有旋涡水平时,较小的扰动可能会引起大振幅干扰。为了理解该旋流范围内的流动的性质,开发了小扰动分析。它表明,在规定的进出口条件下,很小但有限的入口方位涡度扰动将临界涡旋下的Euler方程解的跨临界分叉分解为扰动解的两个分支。当方位涡度扰动为正时,这些分支显示规律的行为。但是,当它们为负时,扰动的分支在临界旋涡附近的极限点处折叠,两个分支之间有有限的间隙,并且对于旋流接近临界水平的进入流,无法存在近列的平衡状态。流量必须在此旋流范围内产生较大的扰动。超出此范围,在相同的进出口条件下可能存在两个平衡状态。当负入口涡旋扰动的大小变大时,此特殊行为会针对每个传入漩涡均匀地变为单一平衡状态的分支。还讨论了结果与管道中轴对称涡旋破裂的出现的相关性,以及使用入口涡旋扰动控制此现象的方法。结果表明,一般而言,可使用正入口方位涡旋扰动将涡旋分解延迟到更高的涡旋水平,而负扰动会在临界涡旋以下的水平诱发顶点分解的出现。 (C)1998美国物理研究所。 [参考:27]

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