ACCURATE SOLUTIONS OF THE NAVIER-STOKES EQUATIONS DESPITE UNKNOWN OUTFLOW BOUNDARY DATA

被引:21
作者
NORDSTROM, J
机构
[1] FFA, Aeronautical Research Institute of Sweden, S-161 11 Bromma
关键词
D O I
10.1006/jcph.1995.1158
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
A very common procedure when constructing boundary conditions for the time-dependent Navier-Stokes equations at artificial boundaries is to extrapolate the solution from grid points near the boundary to the boundary itself. For supersonic outflow, where all the characteristic variables leave the computational domain, this leads to accurate results. In the case of subsonic outflow, where one characteristic variable enters the computational domain, one cannot in general expect accurate solutions by this procedure, The problem with outflow boundary operators of extrapolation type at artificial boundaries with errors in the boundary data of order one will be investigated. Both the problem when the artificial outflow boundary is located in essentially uniform flow and the situation when the artificial outflow boundary is located in a flow field with large gradients are discussed. It will be shown, that in the special case when there are large gradients tangential to the boundary, extrapolation methods can be used even in the subsonic case. (C) 1995 Academic Press, Inc.
引用
收藏
页码:184 / 205
页数:22
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