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 |
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creator | Kessler, Martin P. 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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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. 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Copyright © 2004 John Wiley & Sons, Ltd.</description><subject>Compressible flows; shock and detonation phenomena</subject><subject>Computational methods in fluid dynamics</subject><subject>Exact sciences and technology</subject><subject>finite elements</subject><subject>Fluid dynamics</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>hypersonic flow</subject><subject>Nonequilibrium gas dynamics</subject><subject>numerical simulation</subject><subject>Physics</subject><subject>Reactive, radiative, or nonequilibrium flows</subject><subject>Supersonic and hypersonic flows</subject><subject>thermochemical non-equilibrium</subject><issn>0271-2091</issn><issn>1097-0363</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2004</creationdate><recordtype>article</recordtype><recordid>eNp10E1PGzEQBmALUYmQov4FX6CHalOvvR_eI6JNqJRCS1IhcbEc75i4OLupZ6Ow_x5XG8GJy8xhHr0avYR8StkkZYx_tb6eFFV-REYpq8qEiUIckxHjZZpwVqUn5BTxL2Os4lKMyM1lo32PDmlr6brfQsC2cYZa3-6R7tA1j9S6xnVAwcMGmg7p3nVrutS9b0My0x7Ck2somnU8fyQfrPYIZ4c9Jn-m35dX18n8dvbj6nKeGFGJPJE5CC6MLFlWmFWdgdagM225LGUKclXwemVsKeIqctC51EUWZ51ZKznIWozJxZC7De2_HWCnNg4NeK8baHeouOQ550JG-HmAJrSIAazaBrfRoVcpU__7UrEvFfuK8vwQqdFob4NujMM3nhdZfCiL7svg9s5D_16cms6_DanJoB128PyqdXhSRSnKXN3fzBR_-Jn-Wizu1G_xAinkiOs</recordid><startdate>20040430</startdate><enddate>20040430</enddate><creator>Kessler, Martin P.</creator><creator>Awruch, Armando M.</creator><general>John Wiley & Sons, Ltd</general><general>Wiley</general><scope>BSCLL</scope><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20040430</creationdate><title>Analysis of hypersonic flows using finite elements with Taylor-Galerkin scheme</title><author>Kessler, Martin P. ; Awruch, Armando M.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c3935-85e323c87046cbd4eaaea4af28781e8b62dbcf732db65ea58a64a58d4ff82e8d3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2004</creationdate><topic>Compressible flows; shock and detonation phenomena</topic><topic>Computational methods in fluid dynamics</topic><topic>Exact sciences and technology</topic><topic>finite elements</topic><topic>Fluid dynamics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>hypersonic flow</topic><topic>Nonequilibrium gas dynamics</topic><topic>numerical simulation</topic><topic>Physics</topic><topic>Reactive, radiative, or nonequilibrium flows</topic><topic>Supersonic and hypersonic flows</topic><topic>thermochemical non-equilibrium</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Kessler, Martin P.</creatorcontrib><creatorcontrib>Awruch, Armando M.</creatorcontrib><collection>Istex</collection><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>International journal for numerical methods in fluids</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Kessler, Martin P.</au><au>Awruch, Armando M.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Analysis of hypersonic flows using finite elements with Taylor-Galerkin scheme</atitle><jtitle>International journal for numerical methods in fluids</jtitle><addtitle>Int. 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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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