Improvement of Stability and Accuracy for Weighted Essentially Nonoscillatory Scheme
This paper studies the weights stability and accuracy of the implicit fifth-order weighted essentially nonoscillatory finite difference scheme. It is observed that the weights of the Jiang-Shu weighted essentially nonoscillatory scheme oscillate even for smooth flows. An increased " value of 10...
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Veröffentlicht in: | AIAA journal 2009-02, Vol.47 (2), p.331-344 |
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description | This paper studies the weights stability and accuracy of the implicit fifth-order weighted essentially nonoscillatory finite difference scheme. It is observed that the weights of the Jiang-Shu weighted essentially nonoscillatory scheme oscillate even for smooth flows. An increased " value of 10... is suggested for the weighted essentially nonoscillatory smoothness factors, which removes the weights oscillation and significantly improves the accuracy of the weights and solution convergence. With the improved " value, the weights achieve the optimum value with minimum numerical dissipation in smooth regions and maintain the sensitivity to capture nonoscillatory shock profiles for the transonic flows. The theoretical justification of this treatment is given in the paper. The wall surface boundary condition uses a half-point mesh so that the conservative differencing can be enforced. A third-order accurate finite difference scheme is given to treat wall boundary conditions. The implicit time-marching method with unfactored Gauss - Seidel line relaxation is used with the high-order schemes to achieve a high convergence rate. Several transonic cases are calculated to demonstrate the robustness, efficiency, and accuracy of the methodology. (ProQuest: ... denotes formulae/symbols omitted.) |
doi_str_mv | 10.2514/1.37697 |
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It is observed that the weights of the Jiang-Shu weighted essentially nonoscillatory scheme oscillate even for smooth flows. An increased " value of 10... is suggested for the weighted essentially nonoscillatory smoothness factors, which removes the weights oscillation and significantly improves the accuracy of the weights and solution convergence. With the improved " value, the weights achieve the optimum value with minimum numerical dissipation in smooth regions and maintain the sensitivity to capture nonoscillatory shock profiles for the transonic flows. The theoretical justification of this treatment is given in the paper. The wall surface boundary condition uses a half-point mesh so that the conservative differencing can be enforced. A third-order accurate finite difference scheme is given to treat wall boundary conditions. The implicit time-marching method with unfactored Gauss - Seidel line relaxation is used with the high-order schemes to achieve a high convergence rate. Several transonic cases are calculated to demonstrate the robustness, efficiency, and accuracy of the methodology. 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It is observed that the weights of the Jiang-Shu weighted essentially nonoscillatory scheme oscillate even for smooth flows. An increased " value of 10... is suggested for the weighted essentially nonoscillatory smoothness factors, which removes the weights oscillation and significantly improves the accuracy of the weights and solution convergence. With the improved " value, the weights achieve the optimum value with minimum numerical dissipation in smooth regions and maintain the sensitivity to capture nonoscillatory shock profiles for the transonic flows. The theoretical justification of this treatment is given in the paper. The wall surface boundary condition uses a half-point mesh so that the conservative differencing can be enforced. A third-order accurate finite difference scheme is given to treat wall boundary conditions. The implicit time-marching method with unfactored Gauss - Seidel line relaxation is used with the high-order schemes to achieve a high convergence rate. Several transonic cases are calculated to demonstrate the robustness, efficiency, and accuracy of the methodology. (ProQuest: ... denotes formulae/symbols omitted.)</description><subject>Accuracy</subject><subject>Boundary layer</subject><subject>Compressible flows; shock and detonation phenomena</subject><subject>Computational methods in fluid dynamics</subject><subject>Exact sciences and technology</subject><subject>Flow velocity</subject><subject>Fluid dynamics</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Physics</subject><subject>Studies</subject><subject>Systems stability</subject><subject>Transonic flows</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2009</creationdate><recordtype>article</recordtype><recordid>eNptkF9LHDEUxUNR6KqlXyGIVXyYbf5NMvsoYlWQ9mEt7VtIMkmNZCfbJCPOt2-2Kwrq0-Xe--Pccw8AnzGakxazr3hOBV-ID2CGW0ob2rW_d8AMIYQbzFryEezlfF87Ijo8A7fXq3WKD3ZlhwKjg8uitA--TFANPTwzZkzKTNDFBH9Z_-eu2B5e5Fxpr0KY4Pc4xGx8CKrENMGluatSB2DXqZDtp6e6D35-u7g9v2puflxen5_dNIoxUppOLzTlbmF75GzHOu2E01gIa-u8paLlwmjGqbILTnqudU801wojozedofvgeKtbX_g72lzkymdjq5nBxjFLyhHhiHYVPHwF3scxDdWbJDUlwjrGKnSyhUyKOSfr5Dr5lUqTxEhuopVY_o-2kl-e5FQ2KrikBuPzM04wFpy3m7NHW055pV5OvpU7fRfbruW6d9KNIRT7WOg_pTSS_w</recordid><startdate>20090201</startdate><enddate>20090201</enddate><creator>Shen, Yiqing</creator><creator>Zha, Gecheng</creator><creator>Wang, Baoyuan</creator><general>American Institute of Aeronautics and Astronautics</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20090201</creationdate><title>Improvement of Stability and Accuracy for Weighted Essentially Nonoscillatory Scheme</title><author>Shen, Yiqing ; Zha, Gecheng ; Wang, Baoyuan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a442t-8b9b36f9ed0fe848bf7fb177ee9b3537567cb463ae962d6bbd2b6ba10cbd6bbc3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2009</creationdate><topic>Accuracy</topic><topic>Boundary layer</topic><topic>Compressible flows; shock and detonation phenomena</topic><topic>Computational methods in fluid dynamics</topic><topic>Exact sciences and technology</topic><topic>Flow velocity</topic><topic>Fluid dynamics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Physics</topic><topic>Studies</topic><topic>Systems stability</topic><topic>Transonic flows</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Shen, Yiqing</creatorcontrib><creatorcontrib>Zha, Gecheng</creatorcontrib><creatorcontrib>Wang, Baoyuan</creatorcontrib><collection>Pascal-Francis</collection><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>Shen, Yiqing</au><au>Zha, Gecheng</au><au>Wang, Baoyuan</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Improvement of Stability and Accuracy for Weighted Essentially Nonoscillatory Scheme</atitle><jtitle>AIAA journal</jtitle><date>2009-02-01</date><risdate>2009</risdate><volume>47</volume><issue>2</issue><spage>331</spage><epage>344</epage><pages>331-344</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><coden>AIAJAH</coden><abstract>This paper studies the weights stability and accuracy of the implicit fifth-order weighted essentially nonoscillatory finite difference scheme. It is observed that the weights of the Jiang-Shu weighted essentially nonoscillatory scheme oscillate even for smooth flows. An increased " value of 10... is suggested for the weighted essentially nonoscillatory smoothness factors, which removes the weights oscillation and significantly improves the accuracy of the weights and solution convergence. With the improved " value, the weights achieve the optimum value with minimum numerical dissipation in smooth regions and maintain the sensitivity to capture nonoscillatory shock profiles for the transonic flows. The theoretical justification of this treatment is given in the paper. The wall surface boundary condition uses a half-point mesh so that the conservative differencing can be enforced. A third-order accurate finite difference scheme is given to treat wall boundary conditions. The implicit time-marching method with unfactored Gauss - Seidel line relaxation is used with the high-order schemes to achieve a high convergence rate. Several transonic cases are calculated to demonstrate the robustness, efficiency, and accuracy of the methodology. (ProQuest: ... denotes formulae/symbols omitted.)</abstract><cop>Reston, VA</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.37697</doi><tpages>14</tpages></addata></record> |
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subjects | Accuracy Boundary layer Compressible flows shock and detonation phenomena Computational methods in fluid dynamics Exact sciences and technology Flow velocity Fluid dynamics Fundamental areas of phenomenology (including applications) Physics Studies Systems stability Transonic flows |
title | Improvement of Stability and Accuracy for Weighted Essentially Nonoscillatory Scheme |
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