Yaw-Control Spoiler Design Using Design of Experiments Based Wind Tunnel Testing
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Jeong, Byeongmin | ko |
| dc.contributor.author | Lee, Dongoo | ko |
| dc.contributor.author | Shim, Ho-Joon | ko |
| dc.contributor.author | Ahn, Jaemyung | ko |
| dc.contributor.author | Choi, Han-Lim | ko |
| dc.contributor.author | Park, Seung-O | ko |
| dc.contributor.author | Oh, Se-Yoon | ko |
| dc.date.accessioned | 2015-11-20T09:06:43Z | - |
| dc.date.available | 2015-11-20T09:06:43Z | - |
| dc.date.created | 2015-02-24 | - |
| dc.date.created | 2015-02-24 | - |
| dc.date.created | 2015-02-24 | - |
| dc.date.issued | 2015-03 | - |
| dc.identifier.citation | JOURNAL OF AIRCRAFT, v.52, no.2, pp.713 - 718 | - |
| dc.identifier.issn | 0021-8669 | - |
| dc.identifier.uri | http://hdl.handle.net/10203/201012 | - |
| dc.language | English | - |
| dc.publisher | AMER INST AERONAUTICS ASTRONAUTICS | - |
| dc.title | Yaw-Control Spoiler Design Using Design of Experiments Based Wind Tunnel Testing | - |
| dc.type | Article | - |
| dc.identifier.wosid | 000352321100031 | - |
| dc.identifier.scopusid | 2-s2.0-84931076530 | - |
| dc.type.rims | ART | - |
| dc.citation.volume | 52 | - |
| dc.citation.issue | 2 | - |
| dc.citation.beginningpage | 713 | - |
| dc.citation.endingpage | 718 | - |
| dc.citation.publicationname | JOURNAL OF AIRCRAFT | - |
| dc.identifier.doi | 10.2514/1.C032747 | - |
| dc.contributor.localauthor | Ahn, Jaemyung | - |
| dc.contributor.localauthor | Choi, Han-Lim | - |
| dc.contributor.localauthor | Park, Seung-O | - |
| dc.contributor.nonIdAuthor | Jeong, Byeongmin | - |
| dc.contributor.nonIdAuthor | Oh, Se-Yoon | - |
| dc.description.isOpenAccess | N | - |
| dc.type.journalArticle | Article | - |
| dc.subject.keywordPlus | TAILLESS AIRCRAFT CONFIGURATION | - |
| dc.subject.keywordPlus | STABILITY | - |
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