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Numerical study of flow asymmetry and self-sustained jet oscillations in geometrically symmetric cavities

机译:几何对称腔中流动不对称性和自持射流振荡的数值研究

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摘要

In this paper we present the results of numerical investigation of self-sustained oscillations of a jet confined in a symmetric cavity. This work represents an attempt to reproduce empirical observations of asymmetric flows in geometrically symmetric systems and to extend the jet flow investigations to more complex possible scenarios. A well-known example of such two-dimensional flow has been reported experimentally and reproduced numerically for simple flow [E. Schreck, M. Schaefer, Numerical study or bifurcation in three-dimensional sudden channel expansions, Comput. Fluids 29 (2000) 583— 593]. It has been found that for some particular control parameter, above its critical value (bifurcation point), the jet can be deflected to either of the two sides of the cavity. In this paper we report a similar behaviour which is, however, characterized by a more complicated flow pattern. While simple flow appears only within small cavity lengths the complex flows develops with increased cavity lengths. Unlike stationary asymmetric solutions accompanied by cavity jet oscillations, as experimentally reported in e.g., [A. Maurel, P. Ern, B.J.A. Zielinska, J.E. Wesfreid, Experimental study of self-sustained oscillations in a confined jet, Phys Rev. E 54 (1996) 3643-3651], in our investigations of both simple and complex asymmetric flow we observed the slow periodical drift of the jet from one to another side of the cavity. The essential control parameters were Reynolds number Re and the ratio length to inlet width L/d. According to experiments of Maurel et al. (1996), the jet is stable and symmetric, when both L/d and Re are below certain critical values, otherwise jet oscillations appear in both experiment and our simulation (cavity oscillations regime). However, further increase of either (or both) L/d and Re leads of so called free jet type oscillations regime. This paper describes complex jet behaviour within the later oscillations regime. We believe that both simple "classical" and "our" complex stationary asymmetric solutions (as well as superimposed cavity-type and free-jet oscillations) can be explained based on physical arguments as already done in previous works. However, the origin of slow drift motion remains still to be resolved. This might be of high importance for clear distinguishing between relevant physical and numerical features in future codes developments.
机译:在本文中,我们介绍了有限对称腔内射流自持振荡的数值研究结果。这项工作代表了对几何对称系统中非对称流的经验观测结果进行重现的尝试,并将射流研究扩展到更复杂的可能情况。已经通过实验报道了这种二维流动的一个众所周知的例子,并通过数值复制了简单流动[E. Schreck,M. Schaefer,三维突然通道扩展中的数值研究或分叉,计算机。流体29(2000)583-593]。已经发现,对于某些特定的控制参数,在其临界值(分叉点)以上,射流可以偏转到空腔的两侧。在本文中,我们报告了类似的行为,但是其特征是更复杂的流模式。虽然简单的流动仅在较小的腔体长度内出现,但复杂的流动却随着腔体长度的增加而发展。与固定的不对称解伴有空腔射流振荡不同,例如在[A. Maurel,P.Ern,B.J.A. Zielinska,JE Wesfreid,密闭射流中自持振荡的实验研究,Phys Rev. E 54(1996)3643-3651],在我们对简单和复杂非对称流动的研究中,我们观察到射流从腔的另一侧。基本的控制参数是雷诺数Re和长度与入口宽度的比L / d。根据Maurel等人的实验。 (1996年),当L / d和Re都低于某些临界值时,射流是稳定且对称的,否则在实验和我们的模拟中都将出现射流振荡(腔振荡机制)。然而,所谓的自由射流型振荡方式的L / d和Re引线中的任一个(或两者)的进一步增加。本文介绍了在随后的振荡范围内的复杂射流行为。我们相信,简单的“经典”和“我们的”复杂的平稳不对称解(以及叠加的腔型和自由射流振荡)都可以根据物理论据进行解释,就像以前的工作一样。但是,缓慢漂移运动的起因仍有待解决。这对于在将来的代码开发中清楚地区分相关的物理和数字特征可能非常重要。

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