Modeling hypersonic entry with the fully-implicit Navier-Stokes (FIN-S) stabilized finite element flow solver
type: Item
instance of: scholarly article
title: Modeling hypersonic entry with the fully-implicit Navier-Stokes (FIN-S) stabilized finite element flow solver
zbMATH Open document ID: 1391.76340
author: Benjamin S. Kirk
author: Roy H. Stogner
author: Paul T. Bauman
author: Todd A. Oliver
published in: Computers and Fluids
publication date: 2018-06-19T00:00:00Z
Mathematics Subject Classification ID: 76M10
Mathematics Subject Classification ID: 76K05
Mathematics Subject Classification ID: 76D05
zbMATH DE Number: 6891123
zbMATH Keywords: stabilized finite elements
zbMATH Keywords: compressible flow
zbMATH Keywords: hypersonic flow
zbMATH Keywords: reentry
zbMATH Keywords: surface ablation
describes a project that uses: PETSc
describes a project that uses: MASA
describes a project that uses: libMesh
describes a project that uses: Spalart-Allmaras
MaRDI profile type: Publication
full work available at URL: j.compfluid.2013.10.003
OpenAlex ID: W2003884583
cites work: Parallel fluid dynamics computations in aerospace applications
cites work: A new finite element formulation for computational fluid dynamics. IV: A discontinuity-capturing operator for multidimensional advective-diffusive systems
cites work: Q5689624
DOI: 10.1016/J.COMPFLUID.2013.10.003
description: scientific article; zbMATH DE number 6891123