Adaptive finite element computations of hypersonic inviscid flows around a doubel ellipsoid

This report documents the potential capabilities of adaptive inviscid flow calculations on unstructured meshes in three dimensions using the finite element method. The finite element formulation of the compressible Euler and Navier-Stokes equations is based on a two-step explicit Taylor-Galerkin sch...

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Detalles Bibliográficos
Autores: Fischer, Thomas B., Oñate Ibáñez de Navarra, Eugenio|||0000-0002-0804-7095
Tipo de recurso: informe técnico
Fecha de publicación:1995
País:España
Institución:Universitat Politècnica de Catalunya (UPC)
Repositorio:UPCommons. Portal del coneixement obert de la UPC
Idioma:inglés
OAI Identifier:oai:upcommons.upc.edu:2117/183696
Acceso en línea:https://hdl.handle.net/2117/183696
Access Level:acceso abierto
Palabra clave:Numerical analysis--Simulation methods
Fluid mechanics
Research Report CIMNE
Anàlisi numèrica
Mecànica de fluids
Classificació AMS::65 Numerical analysis::65D Numerical approximation and computational geometry
Classificació AMS::76 Fluid mechanics::76G25 General aerodynamics and subsonic flows
Àrees temàtiques de la UPC::Matemàtiques i estadística::Anàlisi numèrica
Àrees temàtiques de la UPC::Matemàtiques i estadística::Matemàtica aplicada a les ciències
Descripción
Sumario:This report documents the potential capabilities of adaptive inviscid flow calculations on unstructured meshes in three dimensions using the finite element method. The finite element formulation of the compressible Euler and Navier-Stokes equations is based on a two-step explicit Taylor-Galerkin scheme. Adaptive remeshing is applied to enhance the numerical solution in the vicinity the shocks. Particular emphasis is put on the generation of unstructured tetrahedral meshes as well as in the discussion of estimating the error in the numerical solution. Finally, an application to a well-known 3D high speed flow problem is shown where adaptive remeshing techniques become essential to keep the computational cost within reasonable limits. Its results are compared to some seemingly best reference solutions using other algorithms.