Computation of steady supersonic flows by a flux-difference/splitting method

DOI10.1016/0045-7930(85)90031-3zbMath0583.76068OpenAlexW2021174658MaRDI QIDQ1069378

Maurizio Pandolfi

Publication date: 1985

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7930(85)90031-3

zbMATH Keywords

hyperbolic problemsunsteady flowsflux-difference splitting methodpropagation of wavesaxisymmetric steady supersonic flows

Mathematics Subject Classification ID

Vortex flows for incompressible inviscid fluids (76B47) Supersonic flows (76J20)

Related Items (4)

A numerical method for solving the three-dimensional parabolized Navier-Stokes equations ⋮ A second-order finite-volume scheme for Euler equations: kinetic energy preserving and staggering effects ⋮ Numerical experiments with nonoscillatory schemes using Eulerian and new Lagrangian formulations ⋮ A high-order streamline Godunov scheme for steady supersonic flow computation.

Cites Work

• Shock fitting for everybody
• Approximate Riemann solvers, parameter vectors, and difference schemes
• A Contribution to the Numerical Prediction of Unsteady Flows
• Upwind Difference Schemes for Hyperbolic Systems of Conservation Laws

This page was built for publication: Computation of steady supersonic flows by a flux-difference/splitting method