Supersonic flutter analysis of flat composite panels by unified formulation
In this paper, the linear flutter characteristics of laminated composite flat panels immersed in a supersonic flow is investigated using field consistent elements within the framework of unified formulation. The influence of the aerodynamic damping on the supersonic flutter characteristics of flat c...
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| creator | Natarajan, S Manickam, G Ferreira, AJM Carrera, E |
| description | In this paper, the linear flutter characteristics of laminated composite flat
panels immersed in a supersonic flow is investigated using field consistent
elements within the framework of unified formulation. The influence of the
aerodynamic damping on the supersonic flutter characteristics of flat composite
panels is also investigated. The aerodynamic force is evaluated using
two-dimensional static aerodynamic approximation for high supersonic flow.
Numerical results are presented for laminated composites that bring out the
influence of the flow angle, the boundary conditions, the plate thickness and
the plate aspect ratio on the flutter characteristics. |
| doi_str_mv | 10.48550/arxiv.1312.4233 |
| format | Article |
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panels immersed in a supersonic flow is investigated using field consistent
elements within the framework of unified formulation. The influence of the
aerodynamic damping on the supersonic flutter characteristics of flat composite
panels is also investigated. The aerodynamic force is evaluated using
two-dimensional static aerodynamic approximation for high supersonic flow.
Numerical results are presented for laminated composites that bring out the
influence of the flow angle, the boundary conditions, the plate thickness and
the plate aspect ratio on the flutter characteristics.</description><identifier>DOI: 10.48550/arxiv.1312.4233</identifier><language>eng</language><subject>Mathematics - Numerical Analysis</subject><creationdate>2013-12</creationdate><rights>http://arxiv.org/licenses/nonexclusive-distrib/1.0</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>228,230,776,881</link.rule.ids><linktorsrc>$$Uhttps://arxiv.org/abs/1312.4233$$EView_record_in_Cornell_University$$FView_record_in_$$GCornell_University$$Hfree_for_read</linktorsrc><backlink>$$Uhttps://doi.org/10.48550/arXiv.1312.4233$$DView paper in arXiv$$Hfree_for_read</backlink></links><search><creatorcontrib>Natarajan, S</creatorcontrib><creatorcontrib>Manickam, G</creatorcontrib><creatorcontrib>Ferreira, AJM</creatorcontrib><creatorcontrib>Carrera, E</creatorcontrib><title>Supersonic flutter analysis of flat composite panels by unified formulation</title><description>In this paper, the linear flutter characteristics of laminated composite flat
panels immersed in a supersonic flow is investigated using field consistent
elements within the framework of unified formulation. The influence of the
aerodynamic damping on the supersonic flutter characteristics of flat composite
panels is also investigated. The aerodynamic force is evaluated using
two-dimensional static aerodynamic approximation for high supersonic flow.
Numerical results are presented for laminated composites that bring out the
influence of the flow angle, the boundary conditions, the plate thickness and
the plate aspect ratio on the flutter characteristics.</description><subject>Mathematics - Numerical Analysis</subject><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2013</creationdate><recordtype>article</recordtype><sourceid>GOX</sourceid><recordid>eNotz71qwzAUBWAtGUrSvVPRC9i1_mxrLKFpSwMdmt1cWVcgsCUj2SF--yRtpwOHw4GPkCdWlbJVqnqBdPHnkgnGS8mFeCBfP8uEKcfge-qGZZ4xUQgwrNlnGt2tg5n2cZxi9jPSCQIOmZqVLsE7j5a6mMblNvIx7MjGwZDx8T-35HR4O-0_iuP3--f-9VhArUShK1Mz22IjlEWmjWUNOi2AOS6gd0a3NRrZA3LVSo5GabSNVEyixMoCii15_rv9xXRT8iOktbujujtKXAEKQklF</recordid><startdate>20131215</startdate><enddate>20131215</enddate><creator>Natarajan, S</creator><creator>Manickam, G</creator><creator>Ferreira, AJM</creator><creator>Carrera, E</creator><scope>AKZ</scope><scope>GOX</scope></search><sort><creationdate>20131215</creationdate><title>Supersonic flutter analysis of flat composite panels by unified formulation</title><author>Natarajan, S ; Manickam, G ; Ferreira, AJM ; Carrera, E</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a653-90b61d8e735de19bd17ef93a1f23acfb986eb4cae25842eb59ed74514e4e0dae3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2013</creationdate><topic>Mathematics - Numerical Analysis</topic><toplevel>online_resources</toplevel><creatorcontrib>Natarajan, S</creatorcontrib><creatorcontrib>Manickam, G</creatorcontrib><creatorcontrib>Ferreira, AJM</creatorcontrib><creatorcontrib>Carrera, E</creatorcontrib><collection>arXiv Mathematics</collection><collection>arXiv.org</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Natarajan, S</au><au>Manickam, G</au><au>Ferreira, AJM</au><au>Carrera, E</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Supersonic flutter analysis of flat composite panels by unified formulation</atitle><date>2013-12-15</date><risdate>2013</risdate><abstract>In this paper, the linear flutter characteristics of laminated composite flat
panels immersed in a supersonic flow is investigated using field consistent
elements within the framework of unified formulation. The influence of the
aerodynamic damping on the supersonic flutter characteristics of flat composite
panels is also investigated. The aerodynamic force is evaluated using
two-dimensional static aerodynamic approximation for high supersonic flow.
Numerical results are presented for laminated composites that bring out the
influence of the flow angle, the boundary conditions, the plate thickness and
the plate aspect ratio on the flutter characteristics.</abstract><doi>10.48550/arxiv.1312.4233</doi><oa>free_for_read</oa></addata></record> |
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| title | Supersonic flutter analysis of flat composite panels by unified formulation |
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