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LES OF TURBULENT SWIRLING JETS: STUDY OF JET PRECESSION, RECIRCULATION AND VORTEX BREAKDOWN

机译:湍流涡流的LES:射流前移,回旋和涡流破坏的研究

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Large eddy simulations (LES) of turbulent isothermal swirling flows have been investigated. The Sydney swirl burner configuration has been used for all simulated test cases from a low to a high swirl and Reynolds numbers. Four test cases based on different swirl numbers have been considered and the influence of the swirl number for producing recirculation, vortex breakdown, precession vortex core and the precession frequencies have been investigated. The governing equations for the continuity and momentum are solved on a structured Cartesian grid, and a Smagorinsky eddy viscosity model with the localised dynamic procedure is used as the subgrid scale turbulence model. The results show that the LES successfully predicts both the upstream first recirculation zone generated by the bluff body and the downstream vortex breakdown bubble (VBB) induced by swirl. The plots reveal that the expansion of the upstream recirculation zone is almost similar for each test case. LES results revealed that the increasing swirl number affect to form the VBB in the downstream region, however it promotes the shear layer instability in the recirculation zones. The frequency spectrums indicate the presence of low frequency oscillations and the existence of a central jet precession. Results demonstrated distinct precession frequencies at the considered spatial jet locator and agreed well with the experimental values. The results also highlight the formation of a precessing vortex core (PVC).
机译:研究了湍流等温涡旋流动的大涡模拟(LES)。悉尼旋流燃烧器配置已用于从低到高旋流和雷诺数的所有模拟测试案例。考虑了四个基于不同旋流数的测试案例,并研究了旋流数对产生再循环,涡旋破坏,旋进旋涡芯和旋进频率的影响。在结构化的笛卡尔网格上求解连续性和动量的控制方程,并将具有局部动态过程的Smagorinsky涡流粘度模型用作子网格尺度湍流模型。结果表明,LES成功地预测了阻流体产生的上游第一再循环区和涡旋引起的下游涡流破裂气泡(VBB)。这些图表明,对于每个测试案例,上游再循环区的扩展几乎相似。 LES结果表明,增加的旋流数会影响在下游区域形成VBB,但它会促进再循环区的剪切层失稳。频谱表明存在低频振荡和中央射流进动。结果表明,在考虑的空间射流定位器上,进动频率明显不同,并且与实验值非常吻合。结果还突出了进动旋涡芯(PVC)的形成。

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