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.Full text not available from this repository.
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|
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