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LES And URANS simulations of the swirling flow in a dynamic model of a uniflow-scavenged cylinder

机译:LES和URANS在单流扫气气缸动力学模型中的旋流模拟

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The turbulent swirling flow in a uniflow-scavenged two-stroke engine cylinder is investigated using computational fluid dynamics. The investigation is based on the flow in a scale model with a moving piston. Two numerical approaches are tested; a large eddy simulation (LES) approach with the wall-adaptive local eddy-viscosity (WALE) model and a Reynolds-Averaged Navier-Stokes approach using the k - omega Shear-Stress Transport model. Combustion and compression are neglected. The simulations are verified by a sensitivity study and the performance of the turbulence models are evaluated by comparison with experimental results. Both turbulence models produce results in good agreement with experimental data. The agreement is particularly good for the LES, immediately after the piston passes the bottom dead center. Furthermore, in the piston standstill period, the LES predicts a tangential profile in agreement with the measurements, whereas the k - omega SST model predicts a solid body rotation. Several instabilities are identified during the scavenging process. The formation of a vortex breakdown with multiple helical vortex structures are observed after the scavenge port opening, along with the shedding of vortex rings with superimposed swirl. The turbulence models predict several flow reversals in the vortex breakdown region through the scavenge process. Flow separations in the scavenge ports lead to a secondary axial flow, in the separated region. The secondary flow exits in the top of the scavenge ports, resulting in large velocity gradients near the cylinder liner above the scavenge ports. (C) 2016 Elsevier Inc. All rights reserved.
机译:利用计算流体力学研究了单流扫气二冲程发动机气缸中的湍流涡流。该研究基于带有活动活塞的比例模型中的流量。测试了两种数值方法;大型涡模拟(LES)方法和壁面自适应局部涡粘性(WALE)模型,以及使用k-omega剪切-应力传输模型的雷诺平均Navier-Stokes方法。燃烧和压缩被忽略。通过敏感性研究验证了仿真,并通过与实验结果进行比较来评估湍流模型的性能。两种湍流模型产生的结果均与实验数据吻合良好。活塞经过下止点后,该协议对LES特别有利。此外,在活塞静止期间,LES预测与测量值相符的切线轮廓,而k-ΩSST模型则预测固体旋转。在清除过程中发现了一些不稳定性。在扫气口打开后,观察到具有多个螺旋形涡旋结构的涡旋破裂的形成,以及涡旋环的叠加涡流脱落。湍流模型通过清除过程预测了涡旋破裂区域中的几种流动逆转。扫气口中的流分离导致在分离区域中产生二次轴向流。二次流从扫气口的顶部流出,导致扫气口上方的气缸套附近出现较大的速度梯度。 (C)2016 Elsevier Inc.保留所有权利。

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