Parallel implementation of a gas-kinetic BGK method on unstructured grids for 3-D inviscid missile flows

Date

2009-10-12

Author

Ilgaz, Murat
Tuncer, İsmail Hakkı

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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.

Subject Keywords

Parallel Implementation, Unstructured Grid, Aerodynamic Load, Cell Interface, Equilibrium Distribution Function

URI

https://hdl.handle.net/11511/57703

DOI

https://doi.org/10.1007/978-3-540-92744-0_56

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

M. Ilgaz and İ. H. Tuncer, “Parallel implementation of a gas-kinetic BGK method on unstructured grids for 3-D inviscid missile flows,” 2009, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/57703.