Ravichandran, KS (1995) Explicit Third Order Compact Upwind Difference Schemes for13; Compressible Flow Calculations. Technical Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
A compact upwind difference operator is used to generate formally third order accurate spatial discretizations for the inviscid flux terms of the Euler equations governing compressible fluid flow. A notable feature of the present work is that currently well known first order upwind fluxes such as that of Murman or Roe have been used interchangeably. A Runge-Kutta time stepping algorithm is combined with the high order spatial discretization to produce effective integration schemes for the Euler equations that may be used for both steady and unsteady computations.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Euler Equations;Compressible Flow;Compact Schemes |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 08 Mar 2006 |
| Last Modified: | 24 May 2010 09:40 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1088 |
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