Adaptive Unstructured Mesh Refinement of Supersonic Channel Flows

DOI10.1080/10618560310001634168zbMath1063.76597OpenAlexW2136637562MaRDI QIDQ4651409

M. Michael Yovanovich, R. C. Ripley, Fue-Sang Lien

Publication date: 21 February 2005

Published in: International Journal of Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/10618560310001634168

zbMATH Keywords

Unstructured Grids, Compressible Flow, Shock Capturing, Mesh Adaption, Euler Equation, Inviscid Supersonic Flow

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Supersonic flows (76J20)

Related Items (9)

Computation of flows with shocks using the spectral difference method with artificial viscosity. I: Basic formulation and application ⋮ Computation of flows with shocks using the spectral difference method with artificial viscosity. II: Modified formulation with local mesh refinement ⋮ On construction of shock-capturing boundary closures for high-order finite difference method ⋮ r-adaptive algorithms for high-speed flows and plasma simulations ⋮ r-adaptive algorithms for supersonic flows with high-order flux reconstruction methods ⋮ Combination of adaptive grid-embedding and equation adaptation methods for compressible viscous flows ⋮ Lyapunov exponents and adaptive mesh refinement for high-speed flows using a discontinuous Galerkin scheme ⋮ An h-adaptive solution of the spherical blast wave problem ⋮ A kinetic flux difference splitting method for compressible flows

Uses Software

• AUSM
• EasyMesh

Cites Work

• Unnamed Item
• A sequel to AUSM: AUSM\(^ +\)
• An adaptively refined Cartesian mesh solver for the Euler equations
• Local mesh refinement within a multi-block structured-grid scheme for general flows
• Selective refinement/derefinement algorithms for sequences of nested triangulations

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