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Hybrid Large-Eddy Simulation / Reynolds-Averaged Navier-Stokes Simulations of Sonic Injection into Mach 2 Crossflow

机译:混合声波注入2马赫错流的大涡模拟/雷诺平均Navier-Stokes模拟

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This paper presents numerical simulations of sonic injection of ethylene into a Mach 2 crossflow of air. Experimental Raman scattering imagery, pressure-sensitive paint data and NO-PLIF images are compared with hybrid LES/RANS simulations. The impact of a low-diffusion method on the hybrid LES/RANS solutions is investigated. The effect of grid coarsening is also investigated. The low-dissipation approximation (LD-PPM) is shown to be less impacted by the grid coarsening, but it is numerically unstable at high injection pressures. A three-dimensional visualization of velocity tensor discriminant is used to show the differences between the vortical structures of PPM and LD-PPM as well as the impact of grid coarsening on these structures. The implications of these findings on future research is also presented.
机译:本文介绍了声波注入空气到空气的Mach 2横流中的乙烯的数值模拟。将实验拉曼散射图像,压敏涂料数据和NO-PLIF图像与LES / RANS混合模拟进行了比较。研究了低扩散方法对混合LES / RANS解决方案的影响。还研究了网格粗化的影响。低耗散近似值(LD-PPM)受网格粗化的影响较小,但在高注入压力下在数值上不稳定。速度张量判别式的三维可视化用于显示PPM和LD-PPM涡旋结构之间的差异以及网格粗化对这些结构的影响。还介绍了这些发现对未来研究的影响。

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