Steady relaxation methods for unstructured multigrid Euler and Navier-Stokes solutions

被引:3
|
作者
Morano, E [1 ]
Dervieux, A [1 ]
机构
[1] INRIA, F-06902 SOPHIA ANTIPOLIS, FRANCE
基金
美国国家航空航天局;
关键词
Euler equations; Navier-Stokes equations transonic; laminar; unstructured grids; multigrid method; steady relaxation method;
D O I
10.1080/10618569508940740
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This study focuses on the unstructured-mesh multi-grid computation of two-dimensional, steady, transonic hows governed by the Euler or Navier-Stokes equations (in the laminar, low-Reynolds number regime). The central question is the construction of an algorithm of truly O(N) complexity for second-order accurate schemes. This is achieved either by the ''first-order/second-order'' Defect-Correction process, or directly by a fully ''second-order'' approach. Relations between levels are controlled by a coarsening method introduced by Guillard. This work attempts to follow the available theoretical facts to build several strategies that are then evaluated for a set of airfoil flows.
引用
收藏
页码:137 / 167
页数:31
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