Suppr超能文献

用于可压缩均匀湍流直接数值模拟的气体动力学格式。

Gas-kinetic schemes for direct numerical simulations of compressible homogeneous turbulence.

作者信息

Liao Wei, Peng Yan, Luo Li-Shi

机构信息

Department of Mathematics and Statistics, Old Dominion University, Norfolk, Virginia 23529, USA.

出版信息

Phys Rev E Stat Nonlin Soft Matter Phys. 2009 Oct;80(4 Pt 2):046702. doi: 10.1103/PhysRevE.80.046702. Epub 2009 Oct 14.

Abstract

We apply the gas-kinetic scheme (GKS) for the direct numerical simulations (DNSs) of compressible decaying homogeneous isotropic turbulence (DHIT). We intend to study the accuracy, stability, and efficiency of the gas-kinetic scheme for DNS of compressible homogeneous turbulence depending on both flow conditions and numerics. In particular, we study the GKS with multidimensional, quasi-one-dimensional, dimensional-splitting, and smooth-flow approximations. We simulate the compressible DHIT with the Taylor microscale Reynolds number Re(lambda)=72.0 and the turbulence Mach number Ma(t) between 0.1 and 0.6. We compute the low-order statistical quantities including the total kinetic energy K(t), the dissipation rate epsilon(t), the skewness S(u)(t), and the flatness F(u)(t) of the velocity field u(x,t). We assess the effects on the turbulence statistics due to the approximations made in the treatment of fluxes, the flux limiter, the accuracy of the interpolation, and the bulk viscosity. Our results show that the GKS is adequate for DNS of compressible homogeneous turbulence as far as the low-order turbulence statistics are concerned.

摘要

我们将气体动力学格式(GKS)应用于可压缩衰减均匀各向同性湍流(DHIT)的直接数值模拟(DNS)。我们旨在研究气体动力学格式用于可压缩均匀湍流DNS的精度、稳定性和效率,这取决于流动条件和数值方法。特别地,我们研究了具有多维、准一维、维数分裂和平滑流近似的GKS。我们模拟了泰勒微尺度雷诺数Re(λ)=72.0且湍流马赫数Ma(t)在0.1到0.6之间的可压缩DHIT。我们计算了包括总动能K(t)、耗散率ε(t)、速度场u(x,t)的偏度S(u)(t)和峰度F(u)(t)在内的低阶统计量。我们评估了在通量处理、通量限制器、插值精度和体黏性方面所做近似对湍流统计量的影响。我们的结果表明,就低阶湍流统计量而言,GKS适用于可压缩均匀湍流的DNS。

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验