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Three Dimensional DSMC Calculation for Plume-Plume Interaction of Parallel Supersonic Jets

机译:平行超声速射流羽流相互作用的三维DSMC计算

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摘要

Three dimensional interacting flowfield of two parallel axisymmetric jets is calculated by the DSMC method. Under limited computer resource it is not easy to simulate the three dimensional fiowfield using the method, because every volume of cell is very small and the number of molecules within the cell becomes also very small. In the present calculation the upstream flowfield of each orifice is assumed to be axisymmetric and only the downstream of the orifice is managed to be three dimensional although the downstream flowfield is restricted within one fourth of the full fiowfield. The secondary jet-cell that is formed with two barrel shocks of the two primary jets can be seen clearly in the middle between the jets. The fundamental flow structure calculated by the DSMC method is compared with the experimental result of flow visualization by the laser induced fluorescen- ce technique.
机译:用DSMC方法计算了两个平行轴对称射流的三维相互作用流场。在有限的计算机资源下,使用这种方法模拟三维流场并不容易,因为每个单元的体积都非常小,并且单元内的分子数量也变得非常小。在本计算中,假定每个孔口的上游流场是轴对称的,并且尽管下游流场被限制在全流场的四分之一以内,但只有孔口的下游被管理为三维。在两个喷流之间的中间可以清楚地看到由两个主喷流的两次桶形冲击形成的第二个喷流池。将DSMC方法计算出的基本流动结构与激光诱导荧光技术进行流动可视化的实验结果进行了比较。

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