Simulation Analysis of Fluid-Structure Interaction of High Velocity Environment Influence on Aircraft Wing Materials under Different Mach Numbers
Aircraft service process is in a state of the composite load of pressure and temperature for a long period of time, which inevitably affects the inherent characteristics of some components in aircraft accordingly. The flow field of aircraft wing materials under different Mach numbers is simulated by...
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| Veröffentlicht in: | Sensors (Basel, Switzerland) Switzerland), 2018-04, Vol.18 (4), p.1248 |
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| creator | Zhang, Lijun Sun, Changyan |
| description | Aircraft service process is in a state of the composite load of pressure and temperature for a long period of time, which inevitably affects the inherent characteristics of some components in aircraft accordingly. The flow field of aircraft wing materials under different Mach numbers is simulated by Fluent in order to extract pressure and temperature on the wing in this paper. To determine the effect of coupling stress on the wing's material and structural properties, the fluid-structure interaction (FSI) method is used in ANSYS-Workbench to calculate the stress that is caused by pressure and temperature. Simulation analysis results show that with the increase of Mach number, the pressure and temperature on the wing's surface both increase exponentially and thermal stress that is caused by temperature will be the main factor in the coupled stress. When compared with three kinds of materials, titanium alloy, aluminum alloy, and Haynes alloy, carbon fiber composite material has better performance in service at high speed, and natural frequency under coupling pre-stressing will get smaller. |
| doi_str_mv | 10.3390/s18041248 |
| format | Article |
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The flow field of aircraft wing materials under different Mach numbers is simulated by Fluent in order to extract pressure and temperature on the wing in this paper. To determine the effect of coupling stress on the wing's material and structural properties, the fluid-structure interaction (FSI) method is used in ANSYS-Workbench to calculate the stress that is caused by pressure and temperature. Simulation analysis results show that with the increase of Mach number, the pressure and temperature on the wing's surface both increase exponentially and thermal stress that is caused by temperature will be the main factor in the coupled stress. When compared with three kinds of materials, titanium alloy, aluminum alloy, and Haynes alloy, carbon fiber composite material has better performance in service at high speed, and natural frequency under coupling pre-stressing will get smaller.</description><identifier>ISSN: 1424-8220</identifier><identifier>EISSN: 1424-8220</identifier><identifier>DOI: 10.3390/s18041248</identifier><identifier>PMID: 29670023</identifier><language>eng</language><publisher>Switzerland: MDPI AG</publisher><subject>Aircraft ; Aircraft components ; Carbon fiber reinforced plastics ; Carbon fibers ; Composite materials ; Fiber composites ; Fluid-structure interaction ; Mach number ; Prestressing ; Simulation ; Thermal stress ; Wings (aircraft)</subject><ispartof>Sensors (Basel, Switzerland), 2018-04, Vol.18 (4), p.1248</ispartof><rights>Copyright MDPI AG 2018</rights><rights>2018 by the authors. 2018</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c403t-a3412da8b9ebbf44ff6ecc7c76813a646a63ff454402f8a3fc0f2a24177175d73</citedby><cites>FETCH-LOGICAL-c403t-a3412da8b9ebbf44ff6ecc7c76813a646a63ff454402f8a3fc0f2a24177175d73</cites><orcidid>0000-0002-5273-6867</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.ncbi.nlm.nih.gov/pmc/articles/PMC5948487/pdf/$$EPDF$$P50$$Gpubmedcentral$$Hfree_for_read</linktopdf><linktohtml>$$Uhttps://www.ncbi.nlm.nih.gov/pmc/articles/PMC5948487/$$EHTML$$P50$$Gpubmedcentral$$Hfree_for_read</linktohtml><link.rule.ids>230,314,723,776,780,860,881,27903,27904,53769,53771</link.rule.ids><backlink>$$Uhttps://www.ncbi.nlm.nih.gov/pubmed/29670023$$D View this record in MEDLINE/PubMed$$Hfree_for_read</backlink></links><search><creatorcontrib>Zhang, Lijun</creatorcontrib><creatorcontrib>Sun, Changyan</creatorcontrib><title>Simulation Analysis of Fluid-Structure Interaction of High Velocity Environment Influence on Aircraft Wing Materials under Different Mach Numbers</title><title>Sensors (Basel, Switzerland)</title><addtitle>Sensors (Basel)</addtitle><description>Aircraft service process is in a state of the composite load of pressure and temperature for a long period of time, which inevitably affects the inherent characteristics of some components in aircraft accordingly. 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When compared with three kinds of materials, titanium alloy, aluminum alloy, and Haynes alloy, carbon fiber composite material has better performance in service at high speed, and natural frequency under coupling pre-stressing will get smaller.</description><subject>Aircraft</subject><subject>Aircraft components</subject><subject>Carbon fiber reinforced plastics</subject><subject>Carbon fibers</subject><subject>Composite materials</subject><subject>Fiber composites</subject><subject>Fluid-structure interaction</subject><subject>Mach number</subject><subject>Prestressing</subject><subject>Simulation</subject><subject>Thermal stress</subject><subject>Wings (aircraft)</subject><issn>1424-8220</issn><issn>1424-8220</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2018</creationdate><recordtype>article</recordtype><recordid>eNpdkU9vFCEchkmjaevaQ79AQ-JFD6MMsANzMdnU1jZp9VC1R8IwsEvDQOVPk_0YfmMZWzfVE5Dfw5MXXgCOW_SekB59SC1HtMWU74HDlmLacIzRi2f7A_AqpTuEMCGE74MD3HdsPh2CXzd2Kk5mGzxceem2ySYYDDx3xY7NTY5F5RI1vPRZR6n-cHV8Ydcb-EO7oGzewjP_YGPwk_a5gsYV7ZWGs9FGFaXJ8Nb6NbyW1WGlS7D4UUf4yRqj43zpWqoN_FKmQcf0Grw0ldFHT-sCfD8_-3Z60Vx9_Xx5urpqFEUkN5LUF4-SD70eBkOpMZ1WiinW8ZbIjnayI8bQJaUIGy6JUchgiWnLWMuWIyML8PHRe1-GSY-q5ojSiftoJxm3Ikgr_p14uxHr8CCWPeWUz4K3T4IYfhadsphsUto56XUoSWCEWYcQqnkW4M1_6F0osX73TFHEGV32M_XukVIxpBS12YVpkZiLFruiK3vyPP2O_Nss-Q12daXM</recordid><startdate>20180418</startdate><enddate>20180418</enddate><creator>Zhang, Lijun</creator><creator>Sun, Changyan</creator><general>MDPI AG</general><general>MDPI</general><scope>NPM</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>K9.</scope><scope>7X8</scope><scope>5PM</scope><orcidid>https://orcid.org/0000-0002-5273-6867</orcidid></search><sort><creationdate>20180418</creationdate><title>Simulation Analysis of Fluid-Structure Interaction of High Velocity Environment Influence on Aircraft Wing Materials under Different Mach Numbers</title><author>Zhang, Lijun ; Sun, Changyan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c403t-a3412da8b9ebbf44ff6ecc7c76813a646a63ff454402f8a3fc0f2a24177175d73</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Aircraft</topic><topic>Aircraft components</topic><topic>Carbon fiber reinforced plastics</topic><topic>Carbon fibers</topic><topic>Composite materials</topic><topic>Fiber composites</topic><topic>Fluid-structure interaction</topic><topic>Mach number</topic><topic>Prestressing</topic><topic>Simulation</topic><topic>Thermal stress</topic><topic>Wings (aircraft)</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zhang, Lijun</creatorcontrib><creatorcontrib>Sun, Changyan</creatorcontrib><collection>PubMed</collection><collection>CrossRef</collection><collection>ProQuest Health & Medical Complete (Alumni)</collection><collection>MEDLINE - Academic</collection><collection>PubMed Central (Full Participant titles)</collection><jtitle>Sensors (Basel, Switzerland)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Zhang, Lijun</au><au>Sun, Changyan</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Simulation Analysis of Fluid-Structure Interaction of High Velocity Environment Influence on Aircraft Wing Materials under Different Mach Numbers</atitle><jtitle>Sensors (Basel, Switzerland)</jtitle><addtitle>Sensors (Basel)</addtitle><date>2018-04-18</date><risdate>2018</risdate><volume>18</volume><issue>4</issue><spage>1248</spage><pages>1248-</pages><issn>1424-8220</issn><eissn>1424-8220</eissn><abstract>Aircraft service process is in a state of the composite load of pressure and temperature for a long period of time, which inevitably affects the inherent characteristics of some components in aircraft accordingly. The flow field of aircraft wing materials under different Mach numbers is simulated by Fluent in order to extract pressure and temperature on the wing in this paper. To determine the effect of coupling stress on the wing's material and structural properties, the fluid-structure interaction (FSI) method is used in ANSYS-Workbench to calculate the stress that is caused by pressure and temperature. Simulation analysis results show that with the increase of Mach number, the pressure and temperature on the wing's surface both increase exponentially and thermal stress that is caused by temperature will be the main factor in the coupled stress. When compared with three kinds of materials, titanium alloy, aluminum alloy, and Haynes alloy, carbon fiber composite material has better performance in service at high speed, and natural frequency under coupling pre-stressing will get smaller.</abstract><cop>Switzerland</cop><pub>MDPI AG</pub><pmid>29670023</pmid><doi>10.3390/s18041248</doi><orcidid>https://orcid.org/0000-0002-5273-6867</orcidid><oa>free_for_read</oa></addata></record> |
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| source | DOAJ Directory of Open Access Journals; Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals; MDPI - Multidisciplinary Digital Publishing Institute; PubMed Central; Free Full-Text Journals in Chemistry |
| subjects | Aircraft Aircraft components Carbon fiber reinforced plastics Carbon fibers Composite materials Fiber composites Fluid-structure interaction Mach number Prestressing Simulation Thermal stress Wings (aircraft) |
| title | Simulation Analysis of Fluid-Structure Interaction of High Velocity Environment Influence on Aircraft Wing Materials under Different Mach Numbers |
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