Newton-Krylov methods for low-Mach-number compressible combustion

被引:29
|
作者
Knoll, DA
McHugh, PR
Keyes, DE
机构
[1] OLD DOMINION UNIV,DEPT COMP SCI,NORFOLK,VA 23529
[2] NASA,LANGLEY RES CTR,INST COMP APPLICAT SCI & ENGN,HAMPTON,VA 23681
关键词
D O I
10.2514/3.13174
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Fully coupled numerical techniques are used to compute steady-state solutions to a combusting, low-Mach-number compressible flow through a channel. The nonlinear governing equations are discretized on a staggered mesh via integration over discrete finite volumes. The resulting nonlinear algebraic equations are linearized with Newton's method and solved with a preconditioned Krylov algorithm. The selected Krylov solver is the generalized minimum residual algorithm. A matrix-free Newton-Krylov method and a modified Newton-Krylov method are employed as a means of reducing the required number of expensive Jacobian evaluations. The matrix-free implementation is shown to be superior to the modified Newton-Krylov method when starting from a poor initial guess. The technique of mesh sequencing is shown to provide significant CPU savings for fine grid calculations. Additionally, the domain-based multiplicative Schwarz preconditioning strategy was found to be more effective than incomplete lower-upper factorization type preconditioning at lower Mach numbers.
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页码:961 / 967
页数:7
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