Numerical studies of the flow features and integral aerodynamic characteristics of canard-controlled missiles

The article discusses the flow features of canard-controlled missiles with account to aerodynamic cross- connections conditioned upon the interaction of the spectra of the flow around the canard, tail and body. The results of a numerical analysis of the influence of the relative position of the cana...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Voropaev, S. N., Kalugin, V. T.
Format: Tagungsbericht
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue 1
container_start_page
container_title
container_volume 2318
creator Voropaev, S. N.
Kalugin, V. T.
description The article discusses the flow features of canard-controlled missiles with account to aerodynamic cross- connections conditioned upon the interaction of the spectra of the flow around the canard, tail and body. The results of a numerical analysis of the influence of the relative position of the canard and tail on the integrated aerodynamic characteristics are shown. The possibility of controlling the flow by reducing the intensity of the end vortex generated by the canard is shown.
doi_str_mv 10.1063/5.0037339
format Conference Proceeding
fullrecord <record><control><sourceid>proquest_scita</sourceid><recordid>TN_cdi_proquest_journals_2492102108</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2492102108</sourcerecordid><originalsourceid>FETCH-LOGICAL-p218t-ce2e1642a93657b03da580d6f339a45a7c7d91deba43f2500b488f616086eda13</originalsourceid><addsrcrecordid>eNotkFtLAzEQhYMoWKsP_oOAb8LWSbLZy6MUb1D0RcG3ME2yNmV3U5Ms0n9vtIWBgeE7ZziHkGsGCwaVuJMLAFEL0Z6QGZOSFXXFqlMyA2jLgpfi85xcxLgF4G1dNzMyvE6DDU5jT2OajLOR-o6mjaVd739oZzFNIR9xNNSNyX6FTKIN3uxHHJymeoMBdcoeMTn9r9Y4YjCF9mMKvu-toYOL0fU2XpKzDvtor457Tj4eH96Xz8Xq7elleb8qdpw1qdCWW1aVHFtRyXoNwqBswFRdzoWlxFrXpmXGrrEUHZcA67JpuhwUmsoaZGJObg6-u-C_JxuT2vopjPml4mXLGeRpMnV7oKJ2CZPzo9oFN2DYKwbqr04l1bFO8QtGwmjF</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype><pqid>2492102108</pqid></control><display><type>conference_proceeding</type><title>Numerical studies of the flow features and integral aerodynamic characteristics of canard-controlled missiles</title><source>AIP Journals Complete</source><creator>Voropaev, S. N. ; Kalugin, V. T.</creator><contributor>Mayorova, Vera I ; Fedorov, Igor B ; Rogozin, Dmitry O ; Sadovnichy, Victor A ; Mikrin, Evgeny A ; Aleksandrov, Anatoly A</contributor><creatorcontrib>Voropaev, S. N. ; Kalugin, V. T. ; Mayorova, Vera I ; Fedorov, Igor B ; Rogozin, Dmitry O ; Sadovnichy, Victor A ; Mikrin, Evgeny A ; Aleksandrov, Anatoly A</creatorcontrib><description>The article discusses the flow features of canard-controlled missiles with account to aerodynamic cross- connections conditioned upon the interaction of the spectra of the flow around the canard, tail and body. The results of a numerical analysis of the influence of the relative position of the canard and tail on the integrated aerodynamic characteristics are shown. The possibility of controlling the flow by reducing the intensity of the end vortex generated by the canard is shown.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/5.0037339</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Aerodynamic characteristics ; Aerodynamics ; Computational fluid dynamics ; Missile control ; Missiles ; Numerical analysis</subject><ispartof>AIP conference proceedings, 2021, Vol.2318 (1)</ispartof><rights>Author(s)</rights><rights>2021 Author(s). Published by AIP Publishing.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://pubs.aip.org/acp/article-lookup/doi/10.1063/5.0037339$$EHTML$$P50$$Gscitation$$H</linktohtml><link.rule.ids>310,311,315,781,785,790,791,795,4513,23935,23936,25145,27929,27930,76389</link.rule.ids></links><search><contributor>Mayorova, Vera I</contributor><contributor>Fedorov, Igor B</contributor><contributor>Rogozin, Dmitry O</contributor><contributor>Sadovnichy, Victor A</contributor><contributor>Mikrin, Evgeny A</contributor><contributor>Aleksandrov, Anatoly A</contributor><creatorcontrib>Voropaev, S. N.</creatorcontrib><creatorcontrib>Kalugin, V. T.</creatorcontrib><title>Numerical studies of the flow features and integral aerodynamic characteristics of canard-controlled missiles</title><title>AIP conference proceedings</title><description>The article discusses the flow features of canard-controlled missiles with account to aerodynamic cross- connections conditioned upon the interaction of the spectra of the flow around the canard, tail and body. The results of a numerical analysis of the influence of the relative position of the canard and tail on the integrated aerodynamic characteristics are shown. The possibility of controlling the flow by reducing the intensity of the end vortex generated by the canard is shown.</description><subject>Aerodynamic characteristics</subject><subject>Aerodynamics</subject><subject>Computational fluid dynamics</subject><subject>Missile control</subject><subject>Missiles</subject><subject>Numerical analysis</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2021</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNotkFtLAzEQhYMoWKsP_oOAb8LWSbLZy6MUb1D0RcG3ME2yNmV3U5Ms0n9vtIWBgeE7ZziHkGsGCwaVuJMLAFEL0Z6QGZOSFXXFqlMyA2jLgpfi85xcxLgF4G1dNzMyvE6DDU5jT2OajLOR-o6mjaVd739oZzFNIR9xNNSNyX6FTKIN3uxHHJymeoMBdcoeMTn9r9Y4YjCF9mMKvu-toYOL0fU2XpKzDvtor457Tj4eH96Xz8Xq7elleb8qdpw1qdCWW1aVHFtRyXoNwqBswFRdzoWlxFrXpmXGrrEUHZcA67JpuhwUmsoaZGJObg6-u-C_JxuT2vopjPml4mXLGeRpMnV7oKJ2CZPzo9oFN2DYKwbqr04l1bFO8QtGwmjF</recordid><startdate>20210222</startdate><enddate>20210222</enddate><creator>Voropaev, S. N.</creator><creator>Kalugin, V. T.</creator><general>American Institute of Physics</general><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20210222</creationdate><title>Numerical studies of the flow features and integral aerodynamic characteristics of canard-controlled missiles</title><author>Voropaev, S. N. ; Kalugin, V. T.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p218t-ce2e1642a93657b03da580d6f339a45a7c7d91deba43f2500b488f616086eda13</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Aerodynamic characteristics</topic><topic>Aerodynamics</topic><topic>Computational fluid dynamics</topic><topic>Missile control</topic><topic>Missiles</topic><topic>Numerical analysis</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Voropaev, S. N.</creatorcontrib><creatorcontrib>Kalugin, V. T.</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Voropaev, S. N.</au><au>Kalugin, V. T.</au><au>Mayorova, Vera I</au><au>Fedorov, Igor B</au><au>Rogozin, Dmitry O</au><au>Sadovnichy, Victor A</au><au>Mikrin, Evgeny A</au><au>Aleksandrov, Anatoly A</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Numerical studies of the flow features and integral aerodynamic characteristics of canard-controlled missiles</atitle><btitle>AIP conference proceedings</btitle><date>2021-02-22</date><risdate>2021</risdate><volume>2318</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>The article discusses the flow features of canard-controlled missiles with account to aerodynamic cross- connections conditioned upon the interaction of the spectra of the flow around the canard, tail and body. The results of a numerical analysis of the influence of the relative position of the canard and tail on the integrated aerodynamic characteristics are shown. The possibility of controlling the flow by reducing the intensity of the end vortex generated by the canard is shown.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/5.0037339</doi><tpages>8</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0094-243X
ispartof AIP conference proceedings, 2021, Vol.2318 (1)
issn 0094-243X
1551-7616
language eng
recordid cdi_proquest_journals_2492102108
source AIP Journals Complete
subjects Aerodynamic characteristics
Aerodynamics
Computational fluid dynamics
Missile control
Missiles
Numerical analysis
title Numerical studies of the flow features and integral aerodynamic characteristics of canard-controlled missiles
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-16T03%3A47%3A05IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_scita&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Numerical%20studies%20of%20the%20flow%20features%20and%20integral%20aerodynamic%20characteristics%20of%20canard-controlled%20missiles&rft.btitle=AIP%20conference%20proceedings&rft.au=Voropaev,%20S.%20N.&rft.date=2021-02-22&rft.volume=2318&rft.issue=1&rft.issn=0094-243X&rft.eissn=1551-7616&rft.coden=APCPCS&rft_id=info:doi/10.1063/5.0037339&rft_dat=%3Cproquest_scita%3E2492102108%3C/proquest_scita%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2492102108&rft_id=info:pmid/&rfr_iscdi=true