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Flux difference splitting for the Euler equations with axial symmetry

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Publication:1115277
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DOI10.1007/BF02383596zbMath0663.76070OpenAlexW2051325607MaRDI QIDQ1115277

P. Glaister

Publication date: 1988

Published in: Journal of Engineering Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf02383596

zbMATH Keywords

Euler equationsaxially symmetric flowsapproximate (linearised) Riemann solverconverging spherical shockRoe's flux difference splitting


Mathematics Subject Classification ID

Gas dynamics (general theory) (76N15)


Related Items

Unsteady compressible flow in ducts with varying cross-section: comparison between the nonconservative Euler system and the axisymmetric flow model, Prediction of steady, supercritical, free-surface flow, Approximate Riemann solutions of the two-dimensional shallow-water equations, A multislope MUSCL method on unstructured meshes applied to compressible Euler equations for axisymmetric swirling flows, Hybrid Finite-Volume-Particle Method for Dusty Gas Flows, A non-uniform mesh scheme for compressible flow, A shock capturing scheme for steady, supercritical, free-surface flow



Cites Work

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  • Approximate Riemann solvers, parameter vectors, and difference schemes
  • High Resolution Schemes Using Flux Limiters for Hyperbolic Conservation Laws
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