DC Field | Value | Language |
---|---|---|
dc.contributor.author | Nguyen, Anh Tuan | ko |
dc.contributor.author | Kim, Joong-Kwan | ko |
dc.contributor.author | Han, Jong-seob | ko |
dc.contributor.author | Han, Jae-Hung | ko |
dc.date.accessioned | 2017-01-23T02:56:00Z | - |
dc.date.available | 2017-01-23T02:56:00Z | - |
dc.date.created | 2017-01-05 | - |
dc.date.created | 2017-01-05 | - |
dc.date.created | 2017-01-05 | - |
dc.date.issued | 2016-11 | - |
dc.identifier.citation | JOURNAL OF AIRCRAFT, v.53, no.6, pp.1709 - 1718 | - |
dc.identifier.issn | 0021-8669 | - |
dc.identifier.uri | http://hdl.handle.net/10203/220195 | - |
dc.description.abstract | An extended unsteady vortex-lattice method is developed to study the aerodynamics of insect flapping wings while hovering and during forward flight. Leading-edge suction analogy and vortex-core growth models are used as an extension, which is incorporated into a conventional unsteady vortex-lattice method in an effort to overcome the challenges that arise when simulating insect aerodynamics such as wing-wake interaction and leading-edge effects. A convergence analysis was carried out to derive an optimal aerodynamic mesh and a time-step size for flapping-wing models. A parallel computing technique was used to reduce computational time. The aerodynamics of hawkmoth (Manduca sexta) wing models was simulated, and the results were validated against previous numerical and experimental data. | - |
dc.language | English | - |
dc.publisher | AMER INST AERONAUT ASTRONAUT | - |
dc.title | Extended Unsteady Vortex-Lattice Method for Insect Flapping Wings | - |
dc.type | Article | - |
dc.identifier.wosid | 000390097300012 | - |
dc.identifier.scopusid | 2-s2.0-85012113162 | - |
dc.type.rims | ART | - |
dc.citation.volume | 53 | - |
dc.citation.issue | 6 | - |
dc.citation.beginningpage | 1709 | - |
dc.citation.endingpage | 1718 | - |
dc.citation.publicationname | JOURNAL OF AIRCRAFT | - |
dc.identifier.doi | 10.2514/1.C033456 | - |
dc.contributor.localauthor | Han, Jae-Hung | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordPlus | HAWKMOTH MANDUCA-SEXTA | - |
dc.subject.keywordPlus | LEADING-EDGE VORTEX | - |
dc.subject.keywordPlus | MICRO-AIR VEHICLES | - |
dc.subject.keywordPlus | AERODYNAMIC MODEL | - |
dc.subject.keywordPlus | FLIGHT | - |
dc.subject.keywordPlus | OPTIMIZATION | - |
dc.subject.keywordPlus | HOVER | - |
dc.subject.keywordPlus | CONFIGURATIONS | - |
dc.subject.keywordPlus | PERFORMANCE | - |
dc.subject.keywordPlus | KINEMATICS | - |
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