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.
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|
|Division/Department:||Computational and Theoretical Fluid Dynamics Division|
|Depositing User:||M/S ICAST NAL|
|Date Deposited:||19 Sep 2006|
|Last Modified:||24 May 2010 09:50|
Actions (login required)