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Large-eddy simulations of gas-turbine swirl injector flow dynamics

机译:燃气轮机旋流喷油器流动动力学的大涡模拟

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摘要

A comprehensive study on confined swirling flows in an operational gas-turbine injector was performed by means of large-eddy simulations. The formulation was based on the Favre-filtered conservation equations and a modified Smagorinsky treatment of subgrid-scale motions. The model was then numerically solved by means of a preconditioned density-based finite-volume approach. Calculated mean velocities and turbulence properties show good agreement with experimental data obtained from the laser-Doppler velocimetry measurements. Various aspects of the swirling flow development (such as the central recirculating flow, precessing vortex core and Kelvin-Helmholtz instability) were explored in detail. Both co- and counter-rotating configurations were considered, and the effects of swirl direction on flow characteristics were examined. The flow evolution inside the injector is dictated mainly by the air delivered through the primary swirler. The impact of the secondary swirler appears to be limited.
机译:通过大涡模拟,对燃气轮机喷油器中的受限旋流进行了综合研究。该公式基于Favre滤波的守恒方程和子网格规模运动的改良Smagorinsky处理。然后通过基于密度的预处理有限体积方法对模型进行数值求解。计算出的平均速度和湍流特性与从激光多普勒测速仪测量获得的实验数据显示出良好的一致性。详细探讨了回旋流发展的各个方面(例如中央循环流,旋进旋涡芯和开尔文-亥姆霍兹不稳定性)。同时考虑了同向和反向旋转构型,并研究了旋流方向对流动特性的影响。喷油器内部的流动演变主要由通过主旋流器输送的空气决定。二级旋流器的冲击似乎是有限的。

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