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...
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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 |
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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). 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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> |
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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 |
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