A natural extension of the conventional finite volume method into polygonal unstructured meshes for CFD application

被引:79
作者
Chow, P
Cross, M
Pericleous, K
机构
[1] Ctr. Numer. Modelling Proc. Anal., Sch. of Comp. and Math. Science, University of Greenwich, London
[2] Sch. of Comp. and Math. Sciences, University of Greenwich, Woolwich, London SE18 6PF, Wellington Street
关键词
finite volume; unstructured mesh; computational fluid dynamics;
D O I
10.1016/0307-904X(95)00156-E
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A new general cell-centered solution procedure based upon the conventional control or finite volume (CV or FV) approach has been developed for numerical heat transfer and fluid flow which encompasses both structured and unstructured meshes for any kind of mixed polygon cell. Unlike conventional FV methods for structured and block structured meshes and both FV and FE methods for unstructured meshes, the irregular control volume (ICV) method does not require the shape of the element or cell to be predefined because it simply exploits the concept of fluxes across cell faces. That is, the ICV method enables meshes employing mixtures of triangular, quadrilateral, and any other higher order polygonal cells to be exploited using a single solution procedure. The ICV approach otherwise preserves all the desirable features of conventional FV procedures for a structured mesh; in the current implementation, collocation of variables at cell centers is used with a Rhie and Chow interpolation (to suppress pressure oscillation in the flow field) in the context of the SIMPLE pressure correction solution procedure. In fact all other FV structured mesh-based methods may be perceived as a subset of the ICV formulation. The new ICV formulation is benchmarked using two standard computational fluid dynamics (CFD) problems, i.e., the moving lid cavity and the natural convection driven cavity. Both cases were solved with a variety of structured and unstructured meshes, the latter exploiting mixed polygonal cell meshes. The polygonal mesh experiments show a higher degree of accuracy for equivalent meshes (in nodal density terms) using triangular or quadrilateral cells; these results may be interpreted in a manner similar to the CUPID scheme used in structured meshes for reducing numerical diffusion for flows with changing direction.
引用
收藏
页码:170 / 183
页数:14
相关论文
共 40 条
[1]  
BAILEY C, 1993, MATH MODELLING MATER, P259
[2]  
Baliga B. R., 1980, Numerical Heat Transfer, V3, P393, DOI 10.1080/01495728008961767
[3]  
BARTH TJ, 1990, MAR P VKI LECT SER 1
[4]  
BATINA J, 1991, J AIRCRAFT
[5]   UNSTEADY EULER AIRFOIL SOLUTIONS USING UNSTRUCTURED DYNAMIC MESHES [J].
BATINA, JT .
AIAA JOURNAL, 1990, 28 (08) :1381-1388
[6]   IMPLICIT FLUX-SPLIT EULER SCHEMES FOR UNSTEADY AERODYNAMIC ANALYSIS INVOLVING UNSTRUCTURED DYNAMIC MESHES [J].
BATINA, JT .
AIAA JOURNAL, 1991, 29 (11) :1836-1843
[7]   UNSTEADY EULER ALGORITHM WITH UNSTRUCTURED DYNAMIC MESH FOR COMPLEX-AIRCRAFT AERODYNAMIC ANALYSIS [J].
BATINA, JT .
AIAA JOURNAL, 1991, 29 (03) :327-333
[8]   ANALYTICAL AND NUMERICAL STUDIES OF STRUCTURE OF STEADY SEPARATED FLOWS [J].
BURGGRAF, OR .
JOURNAL OF FLUID MECHANICS, 1966, 24 :113-&
[9]  
CHEN J, 1991, THESIS U LEEDS UK
[10]  
CHILDS PN, 1992, 1ST EUR COMP FLUID D