Saxena, SK and Ravi, K (1993) Some aspects of three dimensional supersonic/hypersonic 13; inviscid blunt body flow computations employing high resolution TVD schemes based on Roe's Riemann solver. Technical Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
A Flow Solver for the solutioi of three dimensional filer Equations to compute supersonic/hypersonic blunt body flows has been developed based on an upwind TV-D (N1USCL) formulation of the Roe Riemann Solver within the finite volume frame work . A Tall boundary condition treatment compatible with the explicit Riemann Solver and a special treatment of the singularity line enhances the robustness of the Flow Solver . A comparative study of various limiters and entropy fixes was carried out to identify the lost approriate combination of the limiter and the entropy fix far the Mach number range of interest . Excellent results of computation at supersonic/hypersonic mach numbers for blunt body flows have been obtained with this combination . Local time stepping and parallelization techniques have been employed to accelerate convergence in terms of effective wall clock times
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Supersonic/hypersonic;Inviscid;Blunt body flows;13; High resolution TVD scheme;Euler solution |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | Mr. N A |
| Date Deposited: | 29 Jun 2006 |
| Last Modified: | 24 May 2010 09:42 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1600 |
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