Analysis of hypersonic flows using finite elements with Taylor-Galerkin scheme

The aim of the present work is to introduce a formulation for the numerical analysis of three‐dimensional thermochemical non‐equilibrium hypersonic flows, using the finite element method and the Taylor–Galerkin scheme and adopting Park's 2‐temperature, 5‐species (N2, O2, NO, N and O) and 17‐rea...

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Veröffentlicht in:International journal for numerical methods in fluids 2004-04, Vol.44 (12), p.1355-1376
Hauptverfasser: Kessler, Martin P., Awruch, Armando M.
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Awruch, Armando M.
description The aim of the present work is to introduce a formulation for the numerical analysis of three‐dimensional thermochemical non‐equilibrium hypersonic flows, using the finite element method and the Taylor–Galerkin scheme and adopting Park's 2‐temperature, 5‐species (N2, O2, NO, N and O) and 17‐reaction model. Examples using Euler and Navier–Stokes equations are included and compared with experimental and numerical works presented by other authors. The results are close to those analysed by other researches and a good computational performance was obtained. Copyright © 2004 John Wiley & Sons, Ltd.
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source Wiley Online Library Journals Frontfile Complete
subjects Compressible flows
shock and detonation phenomena
Computational methods in fluid dynamics
Exact sciences and technology
finite elements
Fluid dynamics
Fundamental areas of phenomenology (including applications)
hypersonic flow
Nonequilibrium gas dynamics
numerical simulation
Physics
Reactive, radiative, or nonequilibrium flows
Supersonic and hypersonic flows
thermochemical non-equilibrium
title Analysis of hypersonic flows using finite elements with Taylor-Galerkin scheme
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