Similarity in the Far Swirling Momentumless TurbulentWake

A. V. Shmidt, Алексей В. Шмидт
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Abstract

Turbulent swirling wakes are usually generated during flow past around a body. Swirls are inserted into the flow by propulsors and they can be formed in various technological devices. An overview of papers devoted to experimental and numerical investigations of the swirling turbulent wakes is presented in [1, 2]. The similarity laws of the swirling turbulent flow decay are investigated [3]. Asymptotic and numerical analysis of the swirling turbulent wakes was performed [4–6]. The classical k− ε model of turbulence was used in these studies. It was shown that even if the tangential component of the mean velocity is small it significantly affects the flow pattern in the turbulent wake and this influence can be traced at sufficiently large distances behind a body. The streamwise component of the excess momentum J and angular momentum M are important integral characteristics of the swirling turbulent wake. The case J = 0, M = 0 corresponds to the swirling turbulent wake behind a self–propelled body. This configuration can be implemented in a wake behind the self–propelled body of revolution (the thrust of a body propulsor compensates the hydrodynamic drag force) with compensation of the swirl introduced by a propulsor. Numerical modelling of the swirling momentumless turbulent wake (J = 0) with nonzero angular momentum was carried out on the basis of the second–order semi–empirical models of turbulence [7–9]. Furthermore, a comparison with experimental data [7] obtained in a wind tunnel in the wake past an ellipsoid of revolution was performed. The drag was compensated by momentum of a swirling jet exhausted from its trailing part and the swirl introduced by the jet was balanced out by the rotation of the body part in the opposite direction. Experimental results on the swirling turbulent wake for M ̸= 0 were presented [10–14]. It should be noted that there is a discrepancy in the results obtained by different authors.
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远旋无动量湍流尾迹的相似性
湍流旋涡尾迹通常是在流过物体时产生的。旋涡是由推进器插入流中的,它们可以在各种工艺装置中形成。关于旋涡湍流尾迹的实验和数值研究的论文综述见[1,2]。研究了旋涡湍流衰减的相似规律[3]。对旋涡湍流尾迹进行了渐近分析和数值分析[4-6]。在这些研究中使用了经典的k−ε湍流模型。结果表明,即使平均速度的切向分量很小,它也会显著影响湍流尾迹中的流型,而且这种影响可以在物体后面足够大的距离上被追踪到。过剩动量J和角动量M的向流分量是旋涡湍流尾流的重要积分特征。J = 0, M = 0的情况对应于自走体后的旋涡湍流尾迹。这种结构可以在自推进旋转体后面的尾流中实现(体推进器的推力补偿流体动力阻力),并补偿由推进器引入的涡流。基于湍流的二阶半经验模型[7-9],对非零角动量的无动量旋涡尾迹(J = 0)进行了数值模拟。此外,还与经过旋转椭球的尾迹风洞实验数据[7]进行了比较。阻力由尾部排出的旋涡射流的动量来补偿,而射流引入的涡流则由身体部分的反方向旋转来平衡。给出了M = 0时的旋涡湍流尾迹的实验结果[10-14]。应该指出的是,不同作者得出的结果存在差异。
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