Panel method formulation for oscillating airfoils in supersonic flow
The mathematical model for two-dimensional unsteady supersonic flow based on the reduced potential equation, also known as the hyperbolic Helmholtz equation, is discussed.
Gespeichert in:
| Veröffentlicht in: | AIAA journal 1995-09, Vol.33 (9), p.1659-1666 |
|---|---|
| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 1666 |
|---|---|
| container_issue | 9 |
| container_start_page | 1659 |
| container_title | AIAA journal |
| container_volume | 33 |
| creator | Soviero, Paulo A. O Ribeiro, Renato S |
| description | The mathematical model for two-dimensional unsteady supersonic flow based on the reduced potential equation, also known as the hyperbolic Helmholtz equation, is discussed. |
| doi_str_mv | 10.2514/3.12707 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_aiaa_</sourceid><recordid>TN_cdi_aiaa_journals_10_2514_3_12707</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>6963408</sourcerecordid><originalsourceid>FETCH-LOGICAL-a373t-dacabed870ff16b7ef02d7cbfdb9aa8785ac321374c05a3f5dd0a41d6e8c09673</originalsourceid><addsrcrecordid>eNpd0MtKAzEUBuAgCtYqvsIgoriYmkszSZdSr1DQhYK7cJqLpqSTmsygvr1TWyx2lRz4-M_hR-iY4AHlZHjJBoQKLHZQj3DGSib56y7qYYxJSYac7qODnGfdRIUkPXT9BLUNxdw279EULqZ5G6DxsV7-i5i1D8u5fivAJxd9yIWvi9wubMqx9rpwIX4eoj0HIduj9dtHL7c3z-P7cvJ49zC-mpTABGtKAxqm1kiBnSPVVFiHqRF66sx0BCCF5KAZJUwMNebAHDcGw5CYykqNR5VgfXS2yl2k-NHa3Ki5z9p2F9Y2tllRPmKYS9rBky04i22qu9sUXbZCZTXq0PkK6RRzTtapRfJzSN-KYLWsUjH1W2UnT9dxkDUEl6DWPv9xVnEsCenYxYqBB9hsXKeohXHKtSE09qvZRP6325t_AE_LjNI</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>215332869</pqid></control><display><type>article</type><title>Panel method formulation for oscillating airfoils in supersonic flow</title><source>Alma/SFX Local Collection</source><creator>Soviero, Paulo A. O ; Ribeiro, Renato S</creator><creatorcontrib>Soviero, Paulo A. O ; Ribeiro, Renato S</creatorcontrib><description>The mathematical model for two-dimensional unsteady supersonic flow based on the reduced potential equation, also known as the hyperbolic Helmholtz equation, is discussed.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/3.12707</identifier><identifier>CODEN: AIAJAH</identifier><language>eng</language><publisher>Reston, VA: American Institute of Aeronautics and Astronautics</publisher><subject>Aerodynamics ; Aircraft ; Applied fluid mechanics ; Exact sciences and technology ; Fluid dynamics ; Fundamental areas of phenomenology (including applications) ; Mathematical models ; Physics</subject><ispartof>AIAA journal, 1995-09, Vol.33 (9), p.1659-1666</ispartof><rights>1995 INIST-CNRS</rights><rights>Copyright American Institute of Aeronautics and Astronautics Sep 1995</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a373t-dacabed870ff16b7ef02d7cbfdb9aa8785ac321374c05a3f5dd0a41d6e8c09673</citedby><cites>FETCH-LOGICAL-a373t-dacabed870ff16b7ef02d7cbfdb9aa8785ac321374c05a3f5dd0a41d6e8c09673</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=3650811$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Soviero, Paulo A. O</creatorcontrib><creatorcontrib>Ribeiro, Renato S</creatorcontrib><title>Panel method formulation for oscillating airfoils in supersonic flow</title><title>AIAA journal</title><description>The mathematical model for two-dimensional unsteady supersonic flow based on the reduced potential equation, also known as the hyperbolic Helmholtz equation, is discussed.</description><subject>Aerodynamics</subject><subject>Aircraft</subject><subject>Applied fluid mechanics</subject><subject>Exact sciences and technology</subject><subject>Fluid dynamics</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Mathematical models</subject><subject>Physics</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1995</creationdate><recordtype>article</recordtype><recordid>eNpd0MtKAzEUBuAgCtYqvsIgoriYmkszSZdSr1DQhYK7cJqLpqSTmsygvr1TWyx2lRz4-M_hR-iY4AHlZHjJBoQKLHZQj3DGSib56y7qYYxJSYac7qODnGfdRIUkPXT9BLUNxdw279EULqZ5G6DxsV7-i5i1D8u5fivAJxd9yIWvi9wubMqx9rpwIX4eoj0HIduj9dtHL7c3z-P7cvJ49zC-mpTABGtKAxqm1kiBnSPVVFiHqRF66sx0BCCF5KAZJUwMNebAHDcGw5CYykqNR5VgfXS2yl2k-NHa3Ki5z9p2F9Y2tllRPmKYS9rBky04i22qu9sUXbZCZTXq0PkK6RRzTtapRfJzSN-KYLWsUjH1W2UnT9dxkDUEl6DWPv9xVnEsCenYxYqBB9hsXKeohXHKtSE09qvZRP6325t_AE_LjNI</recordid><startdate>19950901</startdate><enddate>19950901</enddate><creator>Soviero, Paulo A. O</creator><creator>Ribeiro, Renato S</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>19950901</creationdate><title>Panel method formulation for oscillating airfoils in supersonic flow</title><author>Soviero, Paulo A. O ; Ribeiro, Renato S</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a373t-dacabed870ff16b7ef02d7cbfdb9aa8785ac321374c05a3f5dd0a41d6e8c09673</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1995</creationdate><topic>Aerodynamics</topic><topic>Aircraft</topic><topic>Applied fluid mechanics</topic><topic>Exact sciences and technology</topic><topic>Fluid dynamics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Mathematical models</topic><topic>Physics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Soviero, Paulo A. O</creatorcontrib><creatorcontrib>Ribeiro, Renato S</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>Soviero, Paulo A. O</au><au>Ribeiro, Renato S</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Panel method formulation for oscillating airfoils in supersonic flow</atitle><jtitle>AIAA journal</jtitle><date>1995-09-01</date><risdate>1995</risdate><volume>33</volume><issue>9</issue><spage>1659</spage><epage>1666</epage><pages>1659-1666</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><coden>AIAJAH</coden><abstract>The mathematical model for two-dimensional unsteady supersonic flow based on the reduced potential equation, also known as the hyperbolic Helmholtz equation, is discussed.</abstract><cop>Reston, VA</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/3.12707</doi><tpages>8</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0001-1452 |
| ispartof | AIAA journal, 1995-09, Vol.33 (9), p.1659-1666 |
| issn | 0001-1452 1533-385X |
| language | eng |
| recordid | cdi_aiaa_journals_10_2514_3_12707 |
| source | Alma/SFX Local Collection |
| subjects | Aerodynamics Aircraft Applied fluid mechanics Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Mathematical models Physics |
| title | Panel method formulation for oscillating airfoils in supersonic flow |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-03T00%3A26%3A09IST&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=Panel%20method%20formulation%20for%20oscillating%20airfoils%20in%20supersonic%20flow&rft.jtitle=AIAA%20journal&rft.au=Soviero,%20Paulo%20A.%20O&rft.date=1995-09-01&rft.volume=33&rft.issue=9&rft.spage=1659&rft.epage=1666&rft.pages=1659-1666&rft.issn=0001-1452&rft.eissn=1533-385X&rft.coden=AIAJAH&rft_id=info:doi/10.2514/3.12707&rft_dat=%3Cproquest_aiaa_%3E6963408%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=215332869&rft_id=info:pmid/&rfr_iscdi=true |