An improved diffuse interface method for three-dimensional multiphase flows with complex interface deformation

被引:7
|
作者
Zhang, Tongwei [1 ,2 ]
Wu, Jie [1 ,2 ,3 ]
Lin, Xingjian [1 ,2 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Jiangsu, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Dept Aerodynam, Nanjing, Peoples R China
[3] Nanjing Univ Aeronaut & Astronaut, Key Lab Unsteady Aerodynam & Flow Control, Minist Ind & Informat Technol, Nanjing, Peoples R China
基金
中国国家自然科学基金;
关键词
diffuse interface method; interface compression; multiphase flow; tiny interfacial structure; LATTICE BOLTZMANN MODEL; INCOMPRESSIBLE 2-PHASE FLOWS; LEVEL-SET; BENCHMARK COMPUTATIONS; FREE-ENERGY; FLUX SOLVER; VOLUME; SIMULATION;
D O I
10.1002/fld.4814
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
An improved diffuse interface (DI) method is proposed for accurately capturing complex interface deformation in simulations of three-dimensional (3D) multiphase flows. In original DI methods, the unphysical phenomenon of interface thickening or blurring can affect the accuracy of numerical simulations, especially for flows with large density ratio and high Reynolds number. To remove this drawback, in this article, an interface-compression term is introduced into the Cahn-Hilliard equation to suppress the interface dispersion. The additional term only takes effect in the interface region and works normal to the interface. The difference of the current method from the previous work is that the compression rate can be adjusted synchronously according to the magnitude of local vorticity, which is strongly correlated to the interface dispersion and changes with the computational time and interface position. Numerical validations of the proposed method are implemented by simulating problems of Laplace law, Rayleigh-Taylor instability, bubble rising in a channel, and binary droplet collision. The obtained results agree well with the analytical solutions and published data. The numerical results show that the phenomenon of interface dispersion is suppressed effectively and the tiny interfacial structures in flow field can be captured accurately.
引用
收藏
页码:976 / 991
页数:16
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