Three dimensional high-order gas-kinetic scheme for supersonic isotropic turbulence I: Criterion for direct numerical simulation

被引:24
作者
Cao, Guiyu [1 ]
Pan, Liang [2 ]
Xu, Kun [1 ,3 ,4 ]
机构
[1] Hong Kong Univ Sci & Technol, Dept Math, Kowloon, Clear Water Bay, Hong Kong, Peoples R China
[2] Beijing Normal Univ, Sch Math Sci, Beijing, Peoples R China
[3] Hong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Clear Water Bay, Hong Kong, Peoples R China
[4] Hong Kong Univ Sci & Technol, Shenzhen Res Inst, Shenzhen, Guangdong, Peoples R China
基金
美国国家科学基金会;
关键词
High-order gas-kinetic scheme; Direct numerical simulation; Compressible isotropic turbulence; Supersonic regime; LARGE-EDDY SIMULATION; COMPRESSIBLE TURBULENCE; BGK SCHEME; REYNOLDS; EULER; TRANSITION; EFFICIENT; MODEL; DECAY;
D O I
10.1016/j.compfluid.2019.104273
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
In this paper, we intend to address the high-order gas-kinetic scheme (HGKS) in the direct numerical simulation (DNS) of compressible isotropic turbulence up to the supersonic regime. To validate the performance of HGKS, the compressible isotropic turbulence with initial turbulent Mach number Ma(t0) = 0.5 and Taylor microscale Reynold number Re-lambda 0 = 72 is simulated as a benchmark. With the consideration of robustness and accuracy, the WENO-Z scheme is adopted for spatial reconstruction in the current higher-order scheme. Statistical quantities are compared with the high-order compact finite difference scheme to determine the spatial and temporal criterion for DNS. According to the grid and time convergence study, it can be concluded that the minimum spatial resolution parameter kappa(max)eta(0) >= 2.71 and the maximum temporal resolution parameter Delta t(ini)/tau(0) <= 27.08/1000 are adequate for HGKS to resolve the compressible isotropic turbulence, where kappa(max) is the maximum resolved wave number, Delta t(ini) is the initial time step, eta(0) and tau(0) are the initial Kolmogorov length scale and time scale, respectively. Guided by such criterion, the compressible isotropic turbulence from subsonic regime Ma(t0) = 0.8 to supersonic one Ma(t0) = 1.2, and the Taylor microscale Reynolds number Re-lambda 0 ranging from 10 to 72 are simulated. With the high initial turbulent Mach number, the strong random shocklets and high expansion regions are identified, as well as the wide range of probability density function over local turbulent Mach number. All those impose great challenge for high-order schemes. In order to construct compressible large eddy simulation models at high turbulent Mach number, the ensemble budget of turbulent kinetic energy is fully analyzed. The solenoidal dissipation rate decreases with the increasing of Ma(t0) and Re lambda(0). Meanwhile, the dilational dissipation rate increases with the increasing of Ma(t0), which cannot be neglected for constructing supersonic turbulence model. The current work shows that HGKS provides a valid tool for the numerical and physical studies of isotropic compressible turbulence in supersonic regime, which is much less reported in the current turbulent flow study. (C) 2019 Elsevier Ltd. All rights reserved.
引用
收藏
页数:14
相关论文
共 59 条