Hovering Hinge-Connected Flapping Plate with Passive Deflection
In this paper, numerical simulations are conducted to study the aerodynamic performance of a completely and partially rigid plate with passive rotation under various stroke amplitudes. Optimal aerodynamic performance and input power are then obtained from these studies.
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| Veröffentlicht in: | AIAA journal 2012-09, Vol.50 (9), p.2020-2027 |
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| container_issue | 9 |
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| container_title | AIAA journal |
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| creator | Wan, Hui Dong, Haibo Huang, George P |
| description | In this paper, numerical simulations are conducted to study the aerodynamic performance of a completely and partially rigid plate with passive rotation under various stroke amplitudes. Optimal aerodynamic performance and input power are then obtained from these studies. |
| doi_str_mv | 10.2514/1.J051375 |
| format | Article |
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Systems</topic><topic>Exact sciences and technology</topic><topic>Flapping</topic><topic>Flapping wings</topic><topic>Flexibility</topic><topic>Fluid dynamics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Insects</topic><topic>Lift</topic><topic>Numerical analysis</topic><topic>Physics</topic><topic>Robotics</topic><topic>Simulation</topic><topic>Wings (aircraft)</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Wan, Hui</creatorcontrib><creatorcontrib>Dong, Haibo</creatorcontrib><creatorcontrib>Huang, George P</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>Wan, Hui</au><au>Dong, Haibo</au><au>Huang, George P</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Hovering Hinge-Connected Flapping Plate with Passive Deflection</atitle><jtitle>AIAA journal</jtitle><date>2012-09-01</date><risdate>2012</risdate><volume>50</volume><issue>9</issue><spage>2020</spage><epage>2027</epage><pages>2020-2027</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><coden>AIAJAH</coden><abstract>In this paper, numerical simulations are conducted to study the aerodynamic performance of a completely and partially rigid plate with passive rotation under various stroke amplitudes. 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| fulltext | fulltext |
| identifier | ISSN: 0001-1452 |
| ispartof | AIAA journal, 2012-09, Vol.50 (9), p.2020-2027 |
| issn | 0001-1452 1533-385X |
| language | eng |
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| source | Alma/SFX Local Collection |
| subjects | Aerodynamics Aircraft Amplitudes Applied fluid mechanics Applied sciences Computer science control theory systems Control theory. Systems Exact sciences and technology Flapping Flapping wings Flexibility Fluid dynamics Fundamental areas of phenomenology (including applications) Insects Lift Numerical analysis Physics Robotics Simulation Wings (aircraft) |
| title | Hovering Hinge-Connected Flapping Plate with Passive Deflection |
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