Parallel implementation of a gas-kinetic BGK method on unstructured grids for 3-D inviscid missile flows
Parallel Computational Fluid Dynamics, Parallel CFD 2007, Antalya, Turkey, 21 - 24 May 2007, pp.449-456, (Full Text)
- Publication Type: Conference Paper / Full Text
- Volume:
- Doi Number: 10.1007/978-3-540-92744-0_56
- City: Antalya
- Country: Turkey
- Page Numbers: pp.449-456
- Middle East Technical University Affiliated: Yes
Abstract
A 3-D gas-kinetic BGK method and its parallel solution algorithm are developed for the computation of inviscid missile flows on unstructured grids. Flow solutions over a supersonic missile are presented to validate the accuracy and robustness of the method. It is shown that the computation time, which is an important deficiency of gas-kinetic BGK methods, may significantly be reduced by performing computations in parallel. © 2009 Springer-Verlag Berlin Heidelberg.