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Active flow control on a UCAV planform using synthetic jets
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Lee, Junhee | - |
dc.contributor.author | Lee, Byunghyun | - |
dc.contributor.author | Kim, Minhee | - |
dc.contributor.author | Kim, Chongam | - |
dc.date.accessioned | 2023-04-19T08:58:37Z | - |
dc.date.available | 2023-04-19T08:58:37Z | - |
dc.date.created | 2018-09-07 | - |
dc.date.created | 2018-09-07 | - |
dc.date.issued | 2016-09 | - |
dc.identifier.citation | International Journal of Aeronautical and Space Sciences, Vol.17 No.3, pp.315-323 | - |
dc.identifier.issn | 2093-274X | - |
dc.identifier.uri | https://hdl.handle.net/10371/191232 | - |
dc.description.abstract | This paper deals with experimental investigation of active flow control via synthetic jets using an unmanned combat air vehicle (UCAV) planform. Fourteen arrays of synthetic jets, mounted along both leading edges, were fully or partially activated to increase aerodynamic efficiency and reduce pitch-up moment. The measurements were carried out using a six-component external balance, a pressure scanner, and tuft flow visualization. It was observed that aerodynamic efficiency (L/D) and pitching moment were clearly affected by the location of jets. In particular, inboard and outboard actuation could effectively increase L/D. Moreover, inboard actuation showed a reduction in the pitch-up, even more than that generated by the full actuation. These results suggest that inboard actuation not only effectively increases L/D but also reduces the pitch-up using only a few actuators. | - |
dc.language | 영어 | - |
dc.publisher | The Korean Society for Aeronautical & Space Sciences | - |
dc.title | Active flow control on a UCAV planform using synthetic jets | - |
dc.type | Article | - |
dc.identifier.doi | 10.5139/IJASS.2016.17.3.315 | - |
dc.citation.journaltitle | International Journal of Aeronautical and Space Sciences | - |
dc.identifier.wosid | 000389069600003 | - |
dc.identifier.scopusid | 2-s2.0-84991336283 | - |
dc.citation.endpage | 323 | - |
dc.citation.number | 3 | - |
dc.citation.startpage | 315 | - |
dc.citation.volume | 17 | - |
dc.identifier.kciid | ART002153029 | - |
dc.description.isOpenAccess | Y | - |
dc.contributor.affiliatedAuthor | Kim, Chongam | - |
dc.type.docType | Article | - |
dc.description.journalClass | 1 | - |
dc.subject.keywordPlus | UNMANNED-AERIAL-VEHICLE | - |
dc.subject.keywordPlus | AIR VEHICLE | - |
dc.subject.keywordPlus | ACTUATORS | - |
dc.subject.keywordPlus | SEPARATION | - |
dc.subject.keywordAuthor | synthetic jet | - |
dc.subject.keywordAuthor | flow control | - |
dc.subject.keywordAuthor | pitch-up | - |
dc.subject.keywordAuthor | UCAV | - |
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