Analytical method of nonlinear coupled constitutive relations for rarefied non-equilibrium flows
It is well known that Navier-Stokes equations are not valid for those high-Knudsen and high-Mach flows, in which the local thermodynamically non-equilibrium effects are dominant. To extend the non-equilibrium describing the ability of macroscopic equations, Nonlinear Coupled Constitutive Relation (N...
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Veröffentlicht in: | Chinese journal of aeronautics 2021-02, Vol.34 (2), p.136-153 |
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creator | HE, Zhiqiang JIANG, Zhongzheng ZHANG, Huangwei CHEN, Weifang |
description | It is well known that Navier-Stokes equations are not valid for those high-Knudsen and high-Mach flows, in which the local thermodynamically non-equilibrium effects are dominant. To extend the non-equilibrium describing the ability of macroscopic equations, Nonlinear Coupled Constitutive Relation (NCCR) model was developed from Eu’s generalized hydrodynamic equations to substitute linear Newton’s law of viscosity and Fourier’s law of heat conduction in conservation laws. In the NCCR model, how to solve the decomposed constitutive equations with reasonable computational cost is a key ingredient of this scheme. In this paper, an analytic method is proposed firstly. Compared to the iterative procedure in the conventional NCCR model, the analytic method not only obtains exact roots of the decomposed constitutive polynomials, but also preserves the nonlinear constitutive relations in the original framework of NCCR methods. Numerical tests to assess the efficiency and accuracy of the proposed method are conducted for argon shock structures, Couette flows, two-dimensional hypersonic flows over a cylinder and three-dimensional supersonic flows over a three-dimensional sphere. These superior advantages of the current method are expected to render itself a powerful tool for simulating the hypersonic rarefied flows and microscale flows of high Knudsen number for engineering applications. |
doi_str_mv | 10.1016/j.cja.2020.06.023 |
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To extend the non-equilibrium describing the ability of macroscopic equations, Nonlinear Coupled Constitutive Relation (NCCR) model was developed from Eu’s generalized hydrodynamic equations to substitute linear Newton’s law of viscosity and Fourier’s law of heat conduction in conservation laws. In the NCCR model, how to solve the decomposed constitutive equations with reasonable computational cost is a key ingredient of this scheme. In this paper, an analytic method is proposed firstly. Compared to the iterative procedure in the conventional NCCR model, the analytic method not only obtains exact roots of the decomposed constitutive polynomials, but also preserves the nonlinear constitutive relations in the original framework of NCCR methods. Numerical tests to assess the efficiency and accuracy of the proposed method are conducted for argon shock structures, Couette flows, two-dimensional hypersonic flows over a cylinder and three-dimensional supersonic flows over a three-dimensional sphere. These superior advantages of the current method are expected to render itself a powerful tool for simulating the hypersonic rarefied flows and microscale flows of high Knudsen number for engineering applications.</description><identifier>ISSN: 1000-9361</identifier><identifier>DOI: 10.1016/j.cja.2020.06.023</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>Knudsen number ; Microscale flow ; Non-equilibrium ; Nonlinear constitutive relations ; Rarefied gas</subject><ispartof>Chinese journal of aeronautics, 2021-02, Vol.34 (2), p.136-153</ispartof><rights>2020 Chinese Society of Aeronautics and Astronautics</rights><rights>Copyright © Wanfang Data Co. Ltd. All Rights Reserved.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c372t-24e1b8f33287a8d8ef5df40269f8d17100392376f5fb7c495a23931be1fc71283</citedby><cites>FETCH-LOGICAL-c372t-24e1b8f33287a8d8ef5df40269f8d17100392376f5fb7c495a23931be1fc71283</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttp://www.wanfangdata.com.cn/images/PeriodicalImages/hkxb-e/hkxb-e.jpg</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S1000936120303125$$EHTML$$P50$$Gelsevier$$Hfree_for_read</linktohtml><link.rule.ids>314,776,780,3537,27901,27902,65306</link.rule.ids></links><search><creatorcontrib>HE, Zhiqiang</creatorcontrib><creatorcontrib>JIANG, Zhongzheng</creatorcontrib><creatorcontrib>ZHANG, Huangwei</creatorcontrib><creatorcontrib>CHEN, Weifang</creatorcontrib><title>Analytical method of nonlinear coupled constitutive relations for rarefied non-equilibrium flows</title><title>Chinese journal of aeronautics</title><description>It is well known that Navier-Stokes equations are not valid for those high-Knudsen and high-Mach flows, in which the local thermodynamically non-equilibrium effects are dominant. To extend the non-equilibrium describing the ability of macroscopic equations, Nonlinear Coupled Constitutive Relation (NCCR) model was developed from Eu’s generalized hydrodynamic equations to substitute linear Newton’s law of viscosity and Fourier’s law of heat conduction in conservation laws. In the NCCR model, how to solve the decomposed constitutive equations with reasonable computational cost is a key ingredient of this scheme. In this paper, an analytic method is proposed firstly. Compared to the iterative procedure in the conventional NCCR model, the analytic method not only obtains exact roots of the decomposed constitutive polynomials, but also preserves the nonlinear constitutive relations in the original framework of NCCR methods. Numerical tests to assess the efficiency and accuracy of the proposed method are conducted for argon shock structures, Couette flows, two-dimensional hypersonic flows over a cylinder and three-dimensional supersonic flows over a three-dimensional sphere. These superior advantages of the current method are expected to render itself a powerful tool for simulating the hypersonic rarefied flows and microscale flows of high Knudsen number for engineering applications.</description><subject>Knudsen number</subject><subject>Microscale flow</subject><subject>Non-equilibrium</subject><subject>Nonlinear constitutive relations</subject><subject>Rarefied gas</subject><issn>1000-9361</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><recordid>eNp9kLtOAzEURF2ARAh8AJ07ql38SPYhqijiJUWigdp4vdfEi2MH25uQv8dRqKlGupq5mjkI3VBSUkKru6FUgywZYaQkVUkYP0MTSggpWl7RC3QZ40AIb2tKJuhj4aQ9JKOkxRtIa99jr7HzzhoHMmDlx62FPquLyaQxmR3gAFYmky9Y-4CDDKBN9uRUAd-jsaYLZtxgbf0-XqFzLW2E6z-dovfHh7flc7F6fXpZLlaF4jVLBZsB7RrNOWtq2fQN6HmvZ4RVrW56mqvmwozXlZ7rrlazdi4ZbzntgGpVU9bwKbo9_d1Lp6X7FIMfQ94WxfrrpxOQcdBMhNTZSU9OFXyMubvYBrOR4SAoEUeAYhAZoDgCFKQSGWDO3J8ykCfsDAQRlQGnoDcBVBK9N_-kfwHCiHvF</recordid><startdate>20210201</startdate><enddate>20210201</enddate><creator>HE, Zhiqiang</creator><creator>JIANG, Zhongzheng</creator><creator>ZHANG, Huangwei</creator><creator>CHEN, Weifang</creator><general>Elsevier Ltd</general><general>Department of Mechanical Engineering,National University of Singapore,Singapore 117576,Singapore%School of Aeronautics and Astronautics,Zhejiang University,Hangzhou 310027,China%Department of Mechanical Engineering,National University of Singapore,Singapore 117576,Singapore</general><general>School of Aeronautics and Astronautics,Zhejiang University,Hangzhou 310027,China</general><scope>6I.</scope><scope>AAFTH</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>2B.</scope><scope>4A8</scope><scope>92I</scope><scope>93N</scope><scope>PSX</scope><scope>TCJ</scope></search><sort><creationdate>20210201</creationdate><title>Analytical method of nonlinear coupled constitutive relations for rarefied non-equilibrium flows</title><author>HE, Zhiqiang ; JIANG, Zhongzheng ; ZHANG, Huangwei ; CHEN, Weifang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c372t-24e1b8f33287a8d8ef5df40269f8d17100392376f5fb7c495a23931be1fc71283</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Knudsen number</topic><topic>Microscale flow</topic><topic>Non-equilibrium</topic><topic>Nonlinear constitutive relations</topic><topic>Rarefied gas</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>HE, Zhiqiang</creatorcontrib><creatorcontrib>JIANG, Zhongzheng</creatorcontrib><creatorcontrib>ZHANG, Huangwei</creatorcontrib><creatorcontrib>CHEN, Weifang</creatorcontrib><collection>ScienceDirect Open Access Titles</collection><collection>Elsevier:ScienceDirect:Open Access</collection><collection>CrossRef</collection><collection>Wanfang Data Journals - Hong Kong</collection><collection>WANFANG Data Centre</collection><collection>Wanfang Data Journals</collection><collection>万方数据期刊 - 香港版</collection><collection>China Online Journals (COJ)</collection><collection>China Online Journals (COJ)</collection><jtitle>Chinese journal of aeronautics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>HE, Zhiqiang</au><au>JIANG, Zhongzheng</au><au>ZHANG, Huangwei</au><au>CHEN, Weifang</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Analytical method of nonlinear coupled constitutive relations for rarefied non-equilibrium flows</atitle><jtitle>Chinese journal of aeronautics</jtitle><date>2021-02-01</date><risdate>2021</risdate><volume>34</volume><issue>2</issue><spage>136</spage><epage>153</epage><pages>136-153</pages><issn>1000-9361</issn><abstract>It is well known that Navier-Stokes equations are not valid for those high-Knudsen and high-Mach flows, in which the local thermodynamically non-equilibrium effects are dominant. To extend the non-equilibrium describing the ability of macroscopic equations, Nonlinear Coupled Constitutive Relation (NCCR) model was developed from Eu’s generalized hydrodynamic equations to substitute linear Newton’s law of viscosity and Fourier’s law of heat conduction in conservation laws. In the NCCR model, how to solve the decomposed constitutive equations with reasonable computational cost is a key ingredient of this scheme. In this paper, an analytic method is proposed firstly. Compared to the iterative procedure in the conventional NCCR model, the analytic method not only obtains exact roots of the decomposed constitutive polynomials, but also preserves the nonlinear constitutive relations in the original framework of NCCR methods. Numerical tests to assess the efficiency and accuracy of the proposed method are conducted for argon shock structures, Couette flows, two-dimensional hypersonic flows over a cylinder and three-dimensional supersonic flows over a three-dimensional sphere. These superior advantages of the current method are expected to render itself a powerful tool for simulating the hypersonic rarefied flows and microscale flows of high Knudsen number for engineering applications.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.cja.2020.06.023</doi><tpages>18</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Knudsen number Microscale flow Non-equilibrium Nonlinear constitutive relations Rarefied gas |
title | Analytical method of nonlinear coupled constitutive relations for rarefied non-equilibrium flows |
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