General Procedure for Riemann Solver to Eliminate Carbuncle and Shock Instability
A novel procedure for the Riemann solver flux calculation is proposed in this paper. With this simple normal velocity reconstruction procedure, all of the commonly used flux solvers (such as Godunov, Roe, Harten-Lax-van Leer-Contact, Advection-Upstream-Splitting-Method, etc.) turn out to be carbuncl...
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creator | Chen, Zhiqiang Huang, Xudong Ren, Yu-Xin Zhou, Ming |
description | A novel procedure for the Riemann solver flux calculation is proposed in this paper. With this simple normal velocity reconstruction procedure, all of the commonly used flux solvers (such as Godunov, Roe, Harten-Lax-van Leer-Contact, Advection-Upstream-Splitting-Method, etc.) turn out to be carbuncle-free and shock-stable. The normal velocity reconstruction procedure is done by a linear reconstruction of the cell interface normal velocity with the transverse neighbor cells, in consideration of the information transport in the transverse direction, which is neglected in the conventional finite volume/difference method. Some typical cases are performed to show that, when the normal velocity reconstruction procedure is used, various schemes (e.g., Roe) become carbuncle-free and shock-stable. In addition, the normal velocity reconstruction procedure has no influence on the contact-preserving property of the original flux solvers, and it adds very little computational cost. The mechanism of the normal velocity reconstruction procedure also is analyzed by a matrix-based stability method, and the results indicate that the normal velocity reconstruction procedure effectively reduces the system’s positive eigenvalues that are leading to shock instability. |
doi_str_mv | 10.2514/1.J055366 |
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With this simple normal velocity reconstruction procedure, all of the commonly used flux solvers (such as Godunov, Roe, Harten-Lax-van Leer-Contact, Advection-Upstream-Splitting-Method, etc.) turn out to be carbuncle-free and shock-stable. The normal velocity reconstruction procedure is done by a linear reconstruction of the cell interface normal velocity with the transverse neighbor cells, in consideration of the information transport in the transverse direction, which is neglected in the conventional finite volume/difference method. Some typical cases are performed to show that, when the normal velocity reconstruction procedure is used, various schemes (e.g., Roe) become carbuncle-free and shock-stable. In addition, the normal velocity reconstruction procedure has no influence on the contact-preserving property of the original flux solvers, and it adds very little computational cost. The mechanism of the normal velocity reconstruction procedure also is analyzed by a matrix-based stability method, and the results indicate that the normal velocity reconstruction procedure effectively reduces the system’s positive eigenvalues that are leading to shock instability.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.J055366</identifier><language>eng</language><publisher>Virginia: American Institute of Aeronautics and Astronautics</publisher><subject>Cost analysis ; Eigenvalues ; Flux ; Reconstruction ; Riemann solver ; Stability analysis ; Velocity</subject><ispartof>AIAA journal, 2017-06, Vol.55 (6), p.2002-2015</ispartof><rights>Copyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at ; employ the ISSN (print) or (online) to initiate your request. See also AIAA Rights and Permissions .</rights><rights>Copyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0001-1452 (print) or 1533-385X (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a394t-8330e8968b8b1f2aca6d26e7a79e1eff0b647001d3ddc1eee998fd4c2ca77c2d3</citedby><cites>FETCH-LOGICAL-a394t-8330e8968b8b1f2aca6d26e7a79e1eff0b647001d3ddc1eee998fd4c2ca77c2d3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27903,27904</link.rule.ids></links><search><creatorcontrib>Chen, Zhiqiang</creatorcontrib><creatorcontrib>Huang, Xudong</creatorcontrib><creatorcontrib>Ren, Yu-Xin</creatorcontrib><creatorcontrib>Zhou, Ming</creatorcontrib><title>General Procedure for Riemann Solver to Eliminate Carbuncle and Shock Instability</title><title>AIAA journal</title><description>A novel procedure for the Riemann solver flux calculation is proposed in this paper. With this simple normal velocity reconstruction procedure, all of the commonly used flux solvers (such as Godunov, Roe, Harten-Lax-van Leer-Contact, Advection-Upstream-Splitting-Method, etc.) turn out to be carbuncle-free and shock-stable. The normal velocity reconstruction procedure is done by a linear reconstruction of the cell interface normal velocity with the transverse neighbor cells, in consideration of the information transport in the transverse direction, which is neglected in the conventional finite volume/difference method. Some typical cases are performed to show that, when the normal velocity reconstruction procedure is used, various schemes (e.g., Roe) become carbuncle-free and shock-stable. In addition, the normal velocity reconstruction procedure has no influence on the contact-preserving property of the original flux solvers, and it adds very little computational cost. The mechanism of the normal velocity reconstruction procedure also is analyzed by a matrix-based stability method, and the results indicate that the normal velocity reconstruction procedure effectively reduces the system’s positive eigenvalues that are leading to shock instability.</description><subject>Cost analysis</subject><subject>Eigenvalues</subject><subject>Flux</subject><subject>Reconstruction</subject><subject>Riemann solver</subject><subject>Stability analysis</subject><subject>Velocity</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNpl0E1Lw0AQBuBFFKzVg_9gQRA8pO5nsjlKqVUp-FEFb2GyO8HUdLduEqH_3kgLHjwNAw_vDC8h55xNhObqmk8emNYyTQ_IiGspE2n0-yEZMcZ4wpUWx-SkbVfDJjLDR-R5jh4jNPQpBouuj0irEOlLjWvwni5D842RdoHOmnpde-iQTiGWvbcNUvCOLj-C_aT3vu2grJu6256SowqaFs_2c0zebmev07tk8Ti_n94sEpC56hIjJUOTp6Y0Ja8EWEidSDGDLEeOVcXKVGXDm046Zzki5rmpnLLCQpZZ4eSYXOxyNzF89dh2xSr00Q8nC6FyngojlB7U1U7ZGNo2YlVsYr2GuC04K34bK3ixb2ywlzsLNcBf2n_4A3dnaYk</recordid><startdate>20170601</startdate><enddate>20170601</enddate><creator>Chen, Zhiqiang</creator><creator>Huang, Xudong</creator><creator>Ren, Yu-Xin</creator><creator>Zhou, Ming</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20170601</creationdate><title>General Procedure for Riemann Solver to Eliminate Carbuncle and Shock Instability</title><author>Chen, Zhiqiang ; Huang, Xudong ; Ren, Yu-Xin ; Zhou, Ming</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a394t-8330e8968b8b1f2aca6d26e7a79e1eff0b647001d3ddc1eee998fd4c2ca77c2d3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Cost analysis</topic><topic>Eigenvalues</topic><topic>Flux</topic><topic>Reconstruction</topic><topic>Riemann solver</topic><topic>Stability analysis</topic><topic>Velocity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Chen, Zhiqiang</creatorcontrib><creatorcontrib>Huang, Xudong</creatorcontrib><creatorcontrib>Ren, Yu-Xin</creatorcontrib><creatorcontrib>Zhou, Ming</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Chen, Zhiqiang</au><au>Huang, Xudong</au><au>Ren, Yu-Xin</au><au>Zhou, Ming</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>General Procedure for Riemann Solver to Eliminate Carbuncle and Shock Instability</atitle><jtitle>AIAA journal</jtitle><date>2017-06-01</date><risdate>2017</risdate><volume>55</volume><issue>6</issue><spage>2002</spage><epage>2015</epage><pages>2002-2015</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><abstract>A novel procedure for the Riemann solver flux calculation is proposed in this paper. With this simple normal velocity reconstruction procedure, all of the commonly used flux solvers (such as Godunov, Roe, Harten-Lax-van Leer-Contact, Advection-Upstream-Splitting-Method, etc.) turn out to be carbuncle-free and shock-stable. The normal velocity reconstruction procedure is done by a linear reconstruction of the cell interface normal velocity with the transverse neighbor cells, in consideration of the information transport in the transverse direction, which is neglected in the conventional finite volume/difference method. Some typical cases are performed to show that, when the normal velocity reconstruction procedure is used, various schemes (e.g., Roe) become carbuncle-free and shock-stable. In addition, the normal velocity reconstruction procedure has no influence on the contact-preserving property of the original flux solvers, and it adds very little computational cost. The mechanism of the normal velocity reconstruction procedure also is analyzed by a matrix-based stability method, and the results indicate that the normal velocity reconstruction procedure effectively reduces the system’s positive eigenvalues that are leading to shock instability.</abstract><cop>Virginia</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.J055366</doi><tpages>14</tpages></addata></record> |
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subjects | Cost analysis Eigenvalues Flux Reconstruction Riemann solver Stability analysis Velocity |
title | General Procedure for Riemann Solver to Eliminate Carbuncle and Shock Instability |
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