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Implementation of a transient adaptive sub-cell module for the parallel-DSMC code using unstructured grids

机译:使用非结构化网格为并行DSMC代码实现瞬态自适应子单元模块

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摘要

A method of transient adaptive sub-cells (TAS) suitable for unstructured grids that is modified from the existing one for the structured grids of DSMC is introduced. The TAS algorithm is implemented within the framework of a parallelized DSMC code (PDSC). Benchmarking tests are conducted for steady driven cavity flow, steady hypersonic flow over a two-dimensional cylinder, steady hypersonic flow over a cylinder/flare and the unsteady vortex shedding behind a two-dimensional cylinder. The use of TAS enables a reduction in the computational expense of the simulation since larger sampling cells and less simulation particles can be employed. Furthermore, the collision quality of the simulation is maintained or improved and the preservation of property gradients and vorticity at the scale of the sub-cells enables correct unsteady vortex shedding frequencies to be predicted. The use of TAS in a parallel-DSMC code allows simulations of unsteady processes at a level to be carried out efficiently, accurately and with acceptable computational time.
机译:介绍了一种适用于非结构化网格的瞬态自适应子单元(TAS)的方法,该方法从DSMC的结构化网格的现有临时子单元进行了修改。 TAS算法是在并行DSMC代码(PDSC)的框架内实现的。进行基准测试,包括:稳定的驱动腔流,二维圆柱体上的稳定高超音速流,圆柱体/喇叭口上的稳定高超音速流以及二维圆柱体后方的不稳定涡流。由于可以采用更大的采样单元和更少的仿真粒子,因此使用TAS可以减少仿真的计算量。此外,可以保持或改善模拟的碰撞质量,并且在子单元的尺度上保留特性梯度和涡度可以预测正确的不稳定涡脱落频率。在并行DSMC代码中使用TAS可以高效,准确且以可接受的计算时间对不稳定过程进行仿真。

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