A VERTEX-CENTERED FINITE-VOLUME METHOD WITH SHOCK DETECTION

被引:7
|
作者
CRUMPTON, PI
SHAW, GJ
机构
[1] Oxford University Computing Laboratory, Numerical Analysis Group, Oxford, OX1 3QD
关键词
VERTEX-CENTERED; FINITE VOLUME; MULTIGRID; NAVIER-STOKES; SHOCK DETECTION; TURBULENCE;
D O I
10.1002/fld.1650180605
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
This paper introduces a vertex-centred finite volume method for compressible viscous flow incorporating a new shock detection procedure. The discretization is designed to be robust and accurate on the highly stretched and curved meshes necessary for resolving turbulent boundary layers around the leading edge of an aerofoil. Details of the method are described for two-dimensional problems and the natural extension to three-dimensional multiblock meshes is discussed. The shock detection procedure is used to limit the range of the shock-capturing dissipation specifically to regions containing shocks. For transonic turbulent flow this is shown to improve the boundary layer representation significantly.
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页码:605 / 625
页数:21
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