A code optimization package for REDUCE
ISSAC '89 Proceedings of the ACM-SIGSAM 1989 international symposium on Symbolic and algebraic computation
FIDE: a REDUCE package for automation of FInite difference method for solving pDE
ISSAC '90 Proceedings of the international symposium on Symbolic and algebraic computation
A new symbolic-numeric approach to stability analysis of difference schemes
ISSAC '92 Papers from the international symposium on Symbolic and algebraic computation
Symbolic-numerical computation of the stability regions for Jameson's schemes
Selected papers presented at the international IMACS symposium on Symbolic computation, new trends and developments
Hi-index | 0.00 |
The Navier-Stokes equations governing the three-dimensional flows of viscous, compressible, heat-conducting gas and augmented by turbulence modeling present the most realistic model for gas flows around the elements of aircraft configurations. We study the stability of one of the Jameson's schemes of 1981, which approximates the set of five Navier-Stokes equations completed by the turbulence model of Baldwin and Lomax. The analysis procedure implements the check-up of the necessary von Neumann stability criterion. It is shown with the aid of the proposed symbolic-numeric strategy that the physical viscosity terms in the Navier-Stokes equations have a dominant effect on the sizes of the stability region in comparison with the heat conduction terms. It turns out that the consideration of turbulence with the aid of eddy viscosity model of Baldwin and Lomax has an insignificant effect on the size of the necessary stability region.