Computation of steady supersonic flows by a flux-difference/splitting method
type: Item
instance of: scholarly article
title: Computation of steady supersonic flows by a flux-difference/splitting method
zbMATH Open document ID: 0583.76068
DOI: 10.1016/0045-7930(85)90031-3
author: Maurizio Pandolfi
published in: Computers and Fluids
publication date: 1985-01-01T00:00:00Z
review text: A flux-difference splitting method has been conceived for the numerical solution of hyperbolic problems and successfully implemented for unsteady flows. It aims to describe the propagation of waves and to respect the domains of dependence. Shock waves are captured numerically very neatly. Here an extension is proposed for the prediction of two-dimensional or axisymmetric steady supersonic flows. Numerical examples are shown to validate the capabilities of the method.
Mathematics Subject Classification ID: 76J20
Mathematics Subject Classification ID: 76B47
zbMATH DE Number: 3934633
zbMATH Keywords: flux-difference splitting method
zbMATH Keywords: hyperbolic problems
zbMATH Keywords: unsteady flows
zbMATH Keywords: propagation of waves
zbMATH Keywords: axisymmetric steady supersonic flows
MaRDI profile type: Publication
full work available at URL: 0045-7930(85)90031-3
OpenAlex ID: W2021174658
cites work: Approximate Riemann solvers, parameter vectors, and difference schemes
cites work: Upwind Difference Schemes for Hyperbolic Systems of Conservation Laws
cites work: A Contribution to the Numerical Prediction of Unsteady Flows
cites work: Shock fitting for everybody
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description: scientific article; zbMATH DE number 3934633