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基于二维紧凑型四阶格子模型的激波管流动模拟

胡开南 耿少娟 张宏武

胡开南, 耿少娟, 张宏武. 基于二维紧凑型四阶格子模型的激波管流动模拟[J]. 航空动力学报, 2017, 32(11): 2777-2783. doi: 10.13224/j.cnki.jasp.2017.11.027
引用本文: 胡开南, 耿少娟, 张宏武. 基于二维紧凑型四阶格子模型的激波管流动模拟[J]. 航空动力学报, 2017, 32(11): 2777-2783. doi: 10.13224/j.cnki.jasp.2017.11.027
Simulating shocktube flow with a twodimensional compact fourth order lattice model[J]. Journal of Aerospace Power, 2017, 32(11): 2777-2783. doi: 10.13224/j.cnki.jasp.2017.11.027
Citation: Simulating shocktube flow with a twodimensional compact fourth order lattice model[J]. Journal of Aerospace Power, 2017, 32(11): 2777-2783. doi: 10.13224/j.cnki.jasp.2017.11.027

基于二维紧凑型四阶格子模型的激波管流动模拟

doi: 10.13224/j.cnki.jasp.2017.11.027
基金项目: 国家重点基础研究发展计划(2016YFB0200901); 国家自然科学基金(51236001)

Simulating shocktube flow with a twodimensional compact fourth order lattice model

  • 摘要: 为了提高格子的稳定性,使用Hermite展开方法,构建了新的二维四阶紧凑型格子模型,即D2Q37A。比较了D2Q37A和与Philippi给出的紧凑型格子模型(D2Q37B)的稳定性。在相同的碰撞频率下,与D2Q37B相比,D2Q37A可以模拟初始密度比更高的一维激波管流动。这表明D2Q37A与现有格子模型相比,具有更好的稳定性。详细给出了适用于高阶格子模型的边界条件实现方式。此边界条件实现方式保留了体现LBM(lattice Boltmann method)粒子特性的迁移碰撞机制。用以上给出的格子模型和边界条件处理方式模拟激波管流动,得到的模拟结果和解析解吻合得很好。这表明所给出的边界处理方式是可行的。此边界格式同样可以用于其他类型的流动和边界。

     

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出版历程
  • 收稿日期:  2016-03-30
  • 刊出日期:  2017-11-28

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