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...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:AIAA journal 2009-02, Vol.47 (2), p.331-344
Hauptverfasser: Shen, Yiqing, Zha, Gecheng, Wang, Baoyuan
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 344
container_issue 2
container_start_page 331
container_title AIAA journal
container_volume 47
creator Shen, Yiqing
Zha, Gecheng
Wang, Baoyuan
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
format Article
fullrecord <record><control><sourceid>proquest_aiaa_</sourceid><recordid>TN_cdi_aiaa_journals_10_2514_1_37697</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>1634190251</sourcerecordid><originalsourceid>FETCH-LOGICAL-a442t-8b9b36f9ed0fe848bf7fb177ee9b3537567cb463ae962d6bbd2b6ba10cbd6bbc3</originalsourceid><addsrcrecordid>eNptkF9LHDEUxUNR6KqlXyGIVXyYbf5NMvsoYlWQ9mEt7VtIMkmNZCfbJCPOt2-2Kwrq0-Xe--Pccw8AnzGakxazr3hOBV-ID2CGW0ob2rW_d8AMIYQbzFryEezlfF87Ijo8A7fXq3WKD3ZlhwKjg8uitA--TFANPTwzZkzKTNDFBH9Z_-eu2B5e5Fxpr0KY4Pc4xGx8CKrENMGluatSB2DXqZDtp6e6D35-u7g9v2puflxen5_dNIoxUppOLzTlbmF75GzHOu2E01gIa-u8paLlwmjGqbILTnqudU801wojozedofvgeKtbX_g72lzkymdjq5nBxjFLyhHhiHYVPHwF3scxDdWbJDUlwjrGKnSyhUyKOSfr5Dr5lUqTxEhuopVY_o-2kl-e5FQ2KrikBuPzM04wFpy3m7NHW055pV5OvpU7fRfbruW6d9KNIRT7WOg_pTSS_w</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>215324844</pqid></control><display><type>article</type><title>Improvement of Stability and Accuracy for Weighted Essentially Nonoscillatory Scheme</title><source>Alma/SFX Local Collection</source><creator>Shen, Yiqing ; Zha, Gecheng ; Wang, Baoyuan</creator><creatorcontrib>Shen, Yiqing ; Zha, Gecheng ; Wang, Baoyuan</creatorcontrib><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.)</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.37697</identifier><identifier>CODEN: AIAJAH</identifier><language>eng</language><publisher>Reston, VA: American Institute of Aeronautics and Astronautics</publisher><subject>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</subject><ispartof>AIAA journal, 2009-02, Vol.47 (2), p.331-344</ispartof><rights>2009 INIST-CNRS</rights><rights>Copyright American Institute of Aeronautics and Astronautics Feb 2009</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a442t-8b9b36f9ed0fe848bf7fb177ee9b3537567cb463ae962d6bbd2b6ba10cbd6bbc3</citedby><cites>FETCH-LOGICAL-a442t-8b9b36f9ed0fe848bf7fb177ee9b3537567cb463ae962d6bbd2b6ba10cbd6bbc3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&amp;idt=21176658$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Shen, Yiqing</creatorcontrib><creatorcontrib>Zha, Gecheng</creatorcontrib><creatorcontrib>Wang, Baoyuan</creatorcontrib><title>Improvement of Stability and Accuracy for Weighted Essentially Nonoscillatory Scheme</title><title>AIAA journal</title><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.)</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 &amp; 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>
fulltext fulltext
identifier ISSN: 0001-1452
ispartof AIAA journal, 2009-02, Vol.47 (2), p.331-344
issn 0001-1452
1533-385X
language eng
recordid cdi_aiaa_journals_10_2514_1_37697
source Alma/SFX Local Collection
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
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-07T16%3A32%3A38IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_aiaa_&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Improvement%20of%20Stability%20and%20Accuracy%20for%20Weighted%20Essentially%20Nonoscillatory%20Scheme&rft.jtitle=AIAA%20journal&rft.au=Shen,%20Yiqing&rft.date=2009-02-01&rft.volume=47&rft.issue=2&rft.spage=331&rft.epage=344&rft.pages=331-344&rft.issn=0001-1452&rft.eissn=1533-385X&rft.coden=AIAJAH&rft_id=info:doi/10.2514/1.37697&rft_dat=%3Cproquest_aiaa_%3E1634190251%3C/proquest_aiaa_%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=215324844&rft_id=info:pmid/&rfr_iscdi=true