Effect of Wing Twisting on Aerodynamic Performance of Flapping Wing System SCIE SCOPUS
DC Field | Value | Language |
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dc.contributor.author | Tri Quang Truong | - |
dc.contributor.author | Vu Hoang Phan | - |
dc.contributor.author | Park, Hoon Cheol | - |
dc.contributor.author | Ko, Jin Hwan | - |
dc.date.accessioned | 2020-04-20T05:40:27Z | - |
dc.date.available | 2020-04-20T05:40:27Z | - |
dc.date.created | 2020-01-28 | - |
dc.date.issued | 2013-07 | - |
dc.identifier.issn | 0001-1452 | - |
dc.identifier.uri | https://sciwatch.kiost.ac.kr/handle/2020.kiost/3157 | - |
dc.description.abstract | In this paper, a simple but effective design for implementing a negative wing twist in a beetle-mimicking wing system is presented. The effectiveness of the design in terms of force generation and power consumption is confirmed by both experiment and calculation. An unsteady blade-element-theory model is used to estimate the aerodynamic forces produced by two different wing kinematics of a flapping-wing system. The model was first validated with the measurement data and two three-dimensional computational-fluid-dynamics results from the literature. The difference between the estimated average lift and the measured lift is 5.6%, which proves that the unsteady blade-element-theory model provides reasonable aerodynamic force estimation. The time history of the current estimation is also close to the measured data and is in between the two computational-fluid-dynamics results. The forces generated by the flapping wings with and without wing twist are estimated using the unsteady blade-element theory to investigate effect of the wing twist on the force generation. The result shows that the flapping-wing system with wing twist produces a 9.5% larger average vertical force or thrust while consuming 37% less power than the flapping-wing system without wing twist. The measured thrust by the swing test also shows 13.2% increase for the flapping wing with wing twist. Thus, by the estimation and measurement, it is confirmed that the wing twist improves the thrust generation. | - |
dc.description.uri | 1 | - |
dc.language | English | - |
dc.publisher | AMER INST AERONAUTICS ASTRONAUTICS | - |
dc.subject | MODEL | - |
dc.subject | FLIGHT | - |
dc.subject | ROTATION | - |
dc.title | Effect of Wing Twisting on Aerodynamic Performance of Flapping Wing System | - |
dc.type | Article | - |
dc.citation.endPage | 1620 | - |
dc.citation.startPage | 1612 | - |
dc.citation.title | AIAA JOURNAL | - |
dc.citation.volume | 51 | - |
dc.citation.number | 7 | - |
dc.contributor.alternativeName | 고진환 | - |
dc.identifier.bibliographicCitation | AIAA JOURNAL, v.51, no.7, pp.1612 - 1620 | - |
dc.identifier.doi | 10.2514/1.J051831 | - |
dc.identifier.scopusid | 2-s2.0-84880243793 | - |
dc.identifier.wosid | 000321680900007 | - |
dc.type.docType | Article | - |
dc.description.journalClass | 1 | - |
dc.subject.keywordPlus | MODEL | - |
dc.subject.keywordPlus | FLIGHT | - |
dc.subject.keywordPlus | ROTATION | - |
dc.relation.journalWebOfScienceCategory | Engineering, Aerospace | - |
dc.description.journalRegisteredClass | scie | - |
dc.description.journalRegisteredClass | scopus | - |
dc.relation.journalResearchArea | Engineering | - |