ON CENTRAL-DIFFERENCE AND UPWIND SCHEMES

被引:293
作者
SWANSON, RC
TURKEL, E
机构
[1] TEL AVIV UNIV,IL-69978 TEL AVIV,ISRAEL
[2] INST COMP APPLICAT SCI & ENGN,HAMPTON,VA 23665
关键词
D O I
10.1016/0021-9991(92)90007-L
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
A class of numerical dissipation models for central-difference schemes constructed with second- and fourth-difference terms is considered. The notion of matrix dissipation associated with upwind schemes is used to establish improved shock capturing capability for these models. In addition, conditions are given that guarantee that such dissipation models produce a TVD scheme. Appropriate switches for this type of model to ensure satisfaction of the TVD property are presented. Significant improvements in the accuracy of a central-difference scheme are demonstrated by computing both inviscid and viscous transonic airfoil flows. © 1992.
引用
收藏
页码:292 / 306
页数:15
相关论文
共 27 条
[21]   CONVENIENT TOTAL VARIATION DIMINISHING CONDITIONS FOR NONLINEAR DIFFERENCE-SCHEMES [J].
TADMOR, E .
SIAM JOURNAL ON NUMERICAL ANALYSIS, 1988, 25 (05) :1002-1014
[22]   FAR-FIELD BOUNDARY-CONDITIONS FOR TRANSONIC LIFTING SOLUTIONS TO THE EULER EQUATIONS [J].
THOMAS, JL ;
SALAS, MD .
AIAA JOURNAL, 1986, 24 (07) :1074-1080
[23]   ACCURACY OF SCHEMES WITH NONUNIFORM MESHES FOR COMPRESSIBLE FLUID-FLOWS [J].
TURKEL, E .
APPLIED NUMERICAL MATHEMATICS, 1986, 2 (06) :529-550
[24]  
TURKEL E, 1990, AIAA901445 PAP
[25]  
Turkel E., 1989, LECT NOTE PHYS, V323, P586
[26]   ACCURATE NUMERICAL-SOLUTIONS FOR TRANSONIC VISCOUS-FLOW OVER FINITE WINGS [J].
VATSA, VN .
JOURNAL OF AIRCRAFT, 1987, 24 (06) :377-385
[27]  
YEE HC, 1987, NASA TM89464