A dispersion relation preserving optimized upwind compact difference scheme for high accuracy flow simulations
In this work, we have derived an optimized upwind compact difference scheme for achieving excellent spatial resolution. The derived numerical scheme adds numerical diffusion which is strictly restricted to a high wavenumber region in order to control numerical instabilities, as well as to achieve de...
Gespeichert in:
Veröffentlicht in: | Journal of computational physics 2014-12, Vol.278, p.378-399 |
---|---|
Hauptverfasser: | , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 399 |
---|---|
container_issue | |
container_start_page | 378 |
container_title | Journal of computational physics |
container_volume | 278 |
creator | Bhumkar, Yogesh G. Sheu, Tony W. H. Sengupta, Tapan K. |
description | In this work, we have derived an optimized upwind compact difference scheme for achieving excellent spatial resolution. The derived numerical scheme adds numerical diffusion which is strictly restricted to a high wavenumber region in order to control numerical instabilities, as well as to achieve de-aliasing ability. More importantly, the derived numerical scheme has excellent dispersion relation preserving (DRP) property. The applicability of the proposed scheme in simulating real flow problems has been demonstrated by solving flow inside a lid driven cavity, a transitional flow past AG24 aerofoil and a two-dimensional decaying turbulence flow. |
doi_str_mv | 10.1016/j.jcp.2014.08.040 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_1642324161</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0021999114006081</els_id><sourcerecordid>1642324161</sourcerecordid><originalsourceid>FETCH-LOGICAL-c396t-6b564cb72a69a59af3c65d9af40d141360a9bf1f7715cf9e3c9639c16af82d603</originalsourceid><addsrcrecordid>eNp9kMtu2zAQRYmiAeq6-YDsuOxG6owetIiuDKOPAAGySdcEPRrGNCRRJSUb7tdHhrvO6s7ingvMEeIBIUdA9e2YH2nMC8AqhyaHCj6IFYKGrNig-ihWAAVmWmv8JD6ndASApq6alRi2svVp5Jh8GGTkzk7XY4ycOJ788CrDOPne_-NWzuPZD62k0I-WpoVzjiMPxDLRgXuWLkR58K8HaYnmaOkiXRfOMvl-vu2mL-LO2S7x_f9ciz8_f7zsfmdPz78ed9unjEqtpkzta1XRflNYpW2trStJ1e2SFbRYYanA6r1Dt9lgTU5zSVqVmlBZ1xStgnItvt52xxj-zpwm0_tE3HV24DAng6oqyqJChUsVb1WKIaXIzozR9zZeDIK5ujVHs7g1V7cGGrO4XZjvN4aXH06eo0nkryZaH5km0wb_Dv0GS8SEQA</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1642324161</pqid></control><display><type>article</type><title>A dispersion relation preserving optimized upwind compact difference scheme for high accuracy flow simulations</title><source>Elsevier ScienceDirect Journals</source><creator>Bhumkar, Yogesh G. ; Sheu, Tony W. H. ; Sengupta, Tapan K.</creator><creatorcontrib>Bhumkar, Yogesh G. ; Sheu, Tony W. H. ; Sengupta, Tapan K.</creatorcontrib><description>In this work, we have derived an optimized upwind compact difference scheme for achieving excellent spatial resolution. The derived numerical scheme adds numerical diffusion which is strictly restricted to a high wavenumber region in order to control numerical instabilities, as well as to achieve de-aliasing ability. More importantly, the derived numerical scheme has excellent dispersion relation preserving (DRP) property. The applicability of the proposed scheme in simulating real flow problems has been demonstrated by solving flow inside a lid driven cavity, a transitional flow past AG24 aerofoil and a two-dimensional decaying turbulence flow.</description><identifier>ISSN: 0021-9991</identifier><identifier>EISSN: 1090-2716</identifier><identifier>DOI: 10.1016/j.jcp.2014.08.040</identifier><language>eng</language><publisher>Elsevier Inc</publisher><subject>Aliasing error ; Compact difference scheme ; Computer simulation ; Decay ; Dispersions ; DRP scheme ; Flow past an aerofoil ; Instability ; Preserving ; q-Waves ; Spatial resolution ; Turbulent flow ; Wavenumber</subject><ispartof>Journal of computational physics, 2014-12, Vol.278, p.378-399</ispartof><rights>2014 Elsevier Inc.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c396t-6b564cb72a69a59af3c65d9af40d141360a9bf1f7715cf9e3c9639c16af82d603</citedby><cites>FETCH-LOGICAL-c396t-6b564cb72a69a59af3c65d9af40d141360a9bf1f7715cf9e3c9639c16af82d603</cites><orcidid>0000-0002-4046-7890</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S0021999114006081$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,776,780,3537,27901,27902,65306</link.rule.ids></links><search><creatorcontrib>Bhumkar, Yogesh G.</creatorcontrib><creatorcontrib>Sheu, Tony W. H.</creatorcontrib><creatorcontrib>Sengupta, Tapan K.</creatorcontrib><title>A dispersion relation preserving optimized upwind compact difference scheme for high accuracy flow simulations</title><title>Journal of computational physics</title><description>In this work, we have derived an optimized upwind compact difference scheme for achieving excellent spatial resolution. The derived numerical scheme adds numerical diffusion which is strictly restricted to a high wavenumber region in order to control numerical instabilities, as well as to achieve de-aliasing ability. More importantly, the derived numerical scheme has excellent dispersion relation preserving (DRP) property. The applicability of the proposed scheme in simulating real flow problems has been demonstrated by solving flow inside a lid driven cavity, a transitional flow past AG24 aerofoil and a two-dimensional decaying turbulence flow.</description><subject>Aliasing error</subject><subject>Compact difference scheme</subject><subject>Computer simulation</subject><subject>Decay</subject><subject>Dispersions</subject><subject>DRP scheme</subject><subject>Flow past an aerofoil</subject><subject>Instability</subject><subject>Preserving</subject><subject>q-Waves</subject><subject>Spatial resolution</subject><subject>Turbulent flow</subject><subject>Wavenumber</subject><issn>0021-9991</issn><issn>1090-2716</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2014</creationdate><recordtype>article</recordtype><recordid>eNp9kMtu2zAQRYmiAeq6-YDsuOxG6owetIiuDKOPAAGySdcEPRrGNCRRJSUb7tdHhrvO6s7ingvMEeIBIUdA9e2YH2nMC8AqhyaHCj6IFYKGrNig-ihWAAVmWmv8JD6ndASApq6alRi2svVp5Jh8GGTkzk7XY4ycOJ788CrDOPne_-NWzuPZD62k0I-WpoVzjiMPxDLRgXuWLkR58K8HaYnmaOkiXRfOMvl-vu2mL-LO2S7x_f9ciz8_f7zsfmdPz78ed9unjEqtpkzta1XRflNYpW2trStJ1e2SFbRYYanA6r1Dt9lgTU5zSVqVmlBZ1xStgnItvt52xxj-zpwm0_tE3HV24DAng6oqyqJChUsVb1WKIaXIzozR9zZeDIK5ujVHs7g1V7cGGrO4XZjvN4aXH06eo0nkryZaH5km0wb_Dv0GS8SEQA</recordid><startdate>20141201</startdate><enddate>20141201</enddate><creator>Bhumkar, Yogesh G.</creator><creator>Sheu, Tony W. H.</creator><creator>Sengupta, Tapan K.</creator><general>Elsevier Inc</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>7U5</scope><scope>8FD</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><orcidid>https://orcid.org/0000-0002-4046-7890</orcidid></search><sort><creationdate>20141201</creationdate><title>A dispersion relation preserving optimized upwind compact difference scheme for high accuracy flow simulations</title><author>Bhumkar, Yogesh G. ; Sheu, Tony W. H. ; Sengupta, Tapan K.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c396t-6b564cb72a69a59af3c65d9af40d141360a9bf1f7715cf9e3c9639c16af82d603</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2014</creationdate><topic>Aliasing error</topic><topic>Compact difference scheme</topic><topic>Computer simulation</topic><topic>Decay</topic><topic>Dispersions</topic><topic>DRP scheme</topic><topic>Flow past an aerofoil</topic><topic>Instability</topic><topic>Preserving</topic><topic>q-Waves</topic><topic>Spatial resolution</topic><topic>Turbulent flow</topic><topic>Wavenumber</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Bhumkar, Yogesh G.</creatorcontrib><creatorcontrib>Sheu, Tony W. H.</creatorcontrib><creatorcontrib>Sengupta, Tapan K.</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>Technology Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>Journal of computational physics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Bhumkar, Yogesh G.</au><au>Sheu, Tony W. H.</au><au>Sengupta, Tapan K.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A dispersion relation preserving optimized upwind compact difference scheme for high accuracy flow simulations</atitle><jtitle>Journal of computational physics</jtitle><date>2014-12-01</date><risdate>2014</risdate><volume>278</volume><spage>378</spage><epage>399</epage><pages>378-399</pages><issn>0021-9991</issn><eissn>1090-2716</eissn><abstract>In this work, we have derived an optimized upwind compact difference scheme for achieving excellent spatial resolution. The derived numerical scheme adds numerical diffusion which is strictly restricted to a high wavenumber region in order to control numerical instabilities, as well as to achieve de-aliasing ability. More importantly, the derived numerical scheme has excellent dispersion relation preserving (DRP) property. The applicability of the proposed scheme in simulating real flow problems has been demonstrated by solving flow inside a lid driven cavity, a transitional flow past AG24 aerofoil and a two-dimensional decaying turbulence flow.</abstract><pub>Elsevier Inc</pub><doi>10.1016/j.jcp.2014.08.040</doi><tpages>22</tpages><orcidid>https://orcid.org/0000-0002-4046-7890</orcidid></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0021-9991 |
ispartof | Journal of computational physics, 2014-12, Vol.278, p.378-399 |
issn | 0021-9991 1090-2716 |
language | eng |
recordid | cdi_proquest_miscellaneous_1642324161 |
source | Elsevier ScienceDirect Journals |
subjects | Aliasing error Compact difference scheme Computer simulation Decay Dispersions DRP scheme Flow past an aerofoil Instability Preserving q-Waves Spatial resolution Turbulent flow Wavenumber |
title | A dispersion relation preserving optimized upwind compact difference scheme for high accuracy flow simulations |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-03T09%3A19%3A28IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=A%20dispersion%20relation%20preserving%20optimized%20upwind%20compact%20difference%20scheme%20for%20high%20accuracy%20flow%20simulations&rft.jtitle=Journal%20of%20computational%20physics&rft.au=Bhumkar,%20Yogesh%20G.&rft.date=2014-12-01&rft.volume=278&rft.spage=378&rft.epage=399&rft.pages=378-399&rft.issn=0021-9991&rft.eissn=1090-2716&rft_id=info:doi/10.1016/j.jcp.2014.08.040&rft_dat=%3Cproquest_cross%3E1642324161%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=1642324161&rft_id=info:pmid/&rft_els_id=S0021999114006081&rfr_iscdi=true |