Modeling hypersonic entry with the fully-implicit Navier-Stokes (FIN-S) stabilized finite element flow solver

DOI10.1016/J.COMPFLUID.2013.10.003zbMath1391.76340OpenAlexW2003884583MaRDI QIDQ1641252

Todd A. Oliver, Benjamin S. Kirk, Roy H. Stogner, Paul T. Bauman

Publication date: 19 June 2018

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

Full work available at URL: https://doi.org/10.1016/j.compfluid.2013.10.003

zbMATH Keywords

compressible flowhypersonic flowstabilized finite elementssurface ablationreentry

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) Finite element methods applied to problems in fluid mechanics (76M10) Hypersonic flows (76K05)

Related Items (5)

A Jacobian-free edge-based Galerkin formulation for compressible flows ⋮ A streamline-upwind Petrov-Galerkin formulation for the analysis of hypersonic flows in thermal non-equilibrium ⋮ High order discontinuous Galerkin simulation of hypersonic shock-boundary layer interaction using subcell limiting approach ⋮ Stabilized methods for high-speed compressible flows: toward hypersonic simulations ⋮ Edge-Based Finite Element Formulation of Magnetohydrodynamics at High Mach Numbers

Uses Software

• PETSc
• libMesh
• MASA
• Spalart-Allmaras

Cites Work

• Unnamed Item
• A new finite element formulation for computational fluid dynamics. IV: A discontinuity-capturing operator for multidimensional advective-diffusive systems
• Parallel fluid dynamics computations in aerospace applications

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