Implicit upwind residual-distribution Euler and Navier-Stokes solver on unstructured meshes

被引:12
|
作者
Issman, E
Degrez, G
Deconinck, H
机构
[1] Von Karman Inst. for Fluid Dynam.
关键词
D O I
10.2514/3.13348
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Implicit iterative solution techniques are considered for application to a compressible Euler and Navier-Stokes solver using upwind residual-distribution schemes on unstructured meshes. Numerical evaluation of the complete Jacobian matrix needed for the linearization process is achieved at low cost, either by finite difference approximation or by Broyden's update. It enables nonlinear solution strategies such as Newton iterative methods where linear systems are solved approximately using an accelerated iterative scheme. The linearized backward Euler scheme is used to integrate the discretized equations in time, together with a simple time-step evolution strategy. Alternatively, when this strategy fails, it is possible to use a Bred-point acceleration method that has proven quite robust, Numerical applications show the efficiency of the iterative strategy for various Bow conditions.
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页码:2021 / 2028
页数:8
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