Computation of three dimensional supersonic and hypersonic blunt body flows using high resolution TVD schemes based on Roe's Approximate Riemann Solver

Saxena, SK and Ravi, K (1995) Computation of three dimensional supersonic and hypersonic blunt body flows using high resolution TVD schemes based on Roe's Approximate Riemann Solver. Lecture Notes in Physics (453). pp. 520-524.

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Abstract

An explicit finite volume TVD (MUSCL) formulation of the Roe's Approximate Riemann Solver is presented for the solution of three-dimensional Euler and Navier-Stokes equations. It is shown to provide accurate solutions of 3D inviscid and viscous high speed flows past blunt body configurations of practical interest.

Item Type: Journal Article
Uncontrolled Keywords: Approximation theory; Boundary conditions; Computer simulation; Convergence of numerical methods; Finite volume method; Hypersonic flow; Laminar flow; Navier Stokes equations; Parallel processing systems; Supersonic flow; Three dimensional; Viscous flow; Blunt body flows; Euler equation; Local time stepping technique; Parallelization technique; Roe Approximate Riemann Solver; Stanton number; Streamwise domain decomposition techniques; Flow of fluids;
Subjects: AERONAUTICS > Aerodynamics
Division/Department: Computational and Theoretical Fluid Dynamics Division, Other
Depositing User: Mr Vijaianand SK
Date Deposited: 07 Jan 2005
Last Modified: 24 May 2010 09:38
URI: http://nal-ir.nal.res.in/id/eprint/299

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