Ravichandran, KS (1996) Flux split, higher order compact upwind difference schemes. In: Proceedings of the 3rd International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, 1-6 sept 1996, Beijing, China.
Full text not available from this repository.Abstract
A family of compact upwind schemes with formal orders of accuracy 3 to 5 have been developed. Flux limiters are introduced to render the schemes TVD and suitable for high-speed gasdynamic computations. Upwinding is introduced through the peculiar velocity upwind (PVU2) split fluxes. The schemes are applied to the computation of the flow fields due to a 2D sonic jet impinging on a flat plate.
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| Uncontrolled Keywords: | Compact upwind schemes;Gasdynamic computations |
| Subjects: | ASTRONAUTICS > Spacecraft Design, Testing and Performance |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 19 Sep 2006 |
| Last Modified: | 24 May 2010 04:20 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2763 |
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