首页> 外文期刊>International Journal of Heat and Fluid Flow >Investigation of large-scale structures of annular swirling jet in a non-premixed burner using delayed detached eddy simulation
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Investigation of large-scale structures of annular swirling jet in a non-premixed burner using delayed detached eddy simulation

机译:使用延迟分离涡流模拟对非预混燃烧器环形旋转射流大规模结构的研究

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Delayed detached eddy simulation (DDES) is accompanied with Stereo-PIV measurements to study the non-reacting flow field of a non-premixed swirl burner in this paper. Comparisons of experimental and numerical data show that the DDES results are capable of predicting the mean swirling flow features adequately. The instantaneous flow field is found to be strongly affected by the Kelvin-Helmholtz instability. The flow near the injector involves a complex behavior including a recirculation zone. The 3D flow structure at the burner exit, visualized by the iso-surface of Q-criterion, displays four instability types. The dominant instabilities are vortex ring structures induced by the Kelvin-Helmholtz instability, and finger structures induced by the swirling instability. Pressure fluctuation signal recorded in the swirling jet region show that the computational flow passes through transition instants from RANS to DDES equations. After that, the swirling jet becomes fully developed with an oscillation frequency of 222 Hz.
机译:延迟分离涡流模拟(DDES)伴随着立体PIV测量,以研究本文的非预混旋流燃烧器的非反应流场。实验和数值数据的比较表明,DDES结果能够预测平均旋流的流量特征。发现瞬时流场受到Kelvin-Helmholtz不稳定的强烈影响。喷射器附近的流动涉及包括再循环区的复杂行为。燃烧器出口的3D流结构,由Q标准的ISO-Surse可视化,显示了四种不稳定类型。主导稳定性是由旋转亥姆霍兹不稳定性引起的涡旋环结构,以及由旋流不稳定性引起的手指结构。记录在旋转喷射区域中的压力波动信号表明计算流程通过从RAN到DDES方程的转换时刻通过。之后,旋转射流通过222Hz的振荡频率完全开发。

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