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Large eddy simulation of a swirling transverse jet into a crossflow with investigation of scalar transport

机译:涡流横向射流到横流的大涡模拟及标量输运研究

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The flow field of a turbulent jet emerging from a straight round pipe into a laminar crossflow is investigated by means of large eddy simulations. The concentration of a passive scalar, introduced with the jet, is calculated in order to quantify the mixing of the jet and the crossflow. In the jet, swirl is introduced by means of body forces and a range of jet swirl numbers from S=0 up to S=0.6 is studied. The impact of the jet swirl on the flow field, on the coherent structures, and on the mixing efficiency is investigated and quantified by means of various analyses. It is found that for all swirl numbers larger than zero a clear asymmetry appears in all quantities studied. Additional to the two hanging vortices at both sides of the jet a third vortex is introduced by the swirling pipe flow which interacts with the former. This feature is described in detail as it is not mentioned in the literature. For the strongest swirl investigated a recirculation zone near the jet exit is observed. Despite the asymmetry and even with a recirculation zone at the outlet, the counter-rotating vortex pair still exists in all cases in the downstream flow, where it entrains a large amount of crossflow fluid into the jet. The near field, however, is altered by the jet swirl in several respects. The jet more and more approaches the bottom wall with increasing swirl. As a result, the entrainment is gradually attenuated due to the larger blocking of the secondary flow by the wall. Increased swirl increases both the turbulent kinetic energy in the pipe and the vorticity of the average flow field near the jet exit, and thus stimulates the mixing in these regions. However, this stimulating effect is overwhelmed by the closer position of the jet trajectory to the wall of the channel with increasing swirl, which in turn reduces entrainment of fresh crossflow fluid into the jet. As a final result of these two competing effects, the overall mixing efficiency of a jet into a crossflow is merely unchanged with the addition of swirl. Various mixing indices, both spatial and temporal, are used for this analysis. Their respective advantages and disadvantages are discussed and detailed illustrations provide a sound understanding of their behavior.
机译:通过大型涡流模拟研究了从直圆形管进入层流错流的湍流射流的流场。计算随射流引入的无源标量的浓度,以便量化射流和错流的混合。在射流中,借助于体力引入涡流,并且研究了从S = 0到S = 0.6的射流涡流数范围。通过各种分析研究和量化了射流涡流对流场,相干结构以及混合效率的影响。发现对于所有大于零的旋流数,在所有研究的量中都出现明显的不对称性。除射流两侧的两个悬挂涡流外,与涡流相互作用的旋流管流引入了第三涡流。由于没有在文献中提及,因此对该功能进行了详细描述。对于所研究的最强旋流,观察到了射流出口附近的回流区。尽管不对称,甚至在出口处有一个回流区,但在所有情况下,逆流涡流仍然存在于下游流中,在那里,它将大量的错流流体夹带到射流中。然而,近场在几个方面被射流涡旋改变。随着旋流的增加,射流越来越接近底壁。结果,夹带由于壁对次级流的较大阻塞而逐渐减弱。涡旋的增加既增加了管道中的湍动能,又增加了射流出口附近的平均流场的涡度,从而刺激了这些区域的混合。然而,随着涡旋的增加,射流轨迹相对于通道壁的更近位置使这种刺激效果不堪重负,这反过来又减少了新鲜的横流流体进入射流的夹带。作为这两个相互竞争的结果的最终结果,射流进入横流的总混合效率只是在增加旋流的情况下保持不变。各种混合指标,包括空间和时间上的混合指标均用于此分析。讨论了它们各自的优缺点,详细的插图对它们的行为提供了很好的理解。

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