DC Field | Value | Language |
---|---|---|
dc.contributor.author | 이성헌 | ko |
dc.contributor.author | 조영기 | ko |
dc.contributor.author | 조한진 | ko |
dc.contributor.author | 방효충 | ko |
dc.date.accessioned | 2017-05-08T08:49:47Z | - |
dc.date.available | 2017-05-08T08:49:47Z | - |
dc.date.created | 2017-01-12 | - |
dc.date.created | 2017-01-12 | - |
dc.date.created | 2017-01-12 | - |
dc.date.issued | 2017-01 | - |
dc.identifier.citation | 한국군사과학기술학회지, v.20, no.1, pp.148 - 157 | - |
dc.identifier.issn | 1598-9127 | - |
dc.identifier.uri | http://hdl.handle.net/10203/223548 | - |
dc.description.abstract | Miniature guided-bullet is an advanced military technology of developing guided missile which is designed to hit a target precisely while having easily carriable miniature size. A key issue of developing such system involves size reduction of the original guided missile system, and this in turn arouses stiffness issue regarding small and thin sized control surface. In this study, procedures on how to calculate the critical flutter speed of special type of control surface with the change of its dimension or material property is arranged. During this procedure, design parameters related to critical flutter speed are abridged to help preliminary design of similar structure even faster than time-consuming, and cumbersome computer analysis. | - |
dc.language | Korean | - |
dc.publisher | 한국군사과학기술학회 | - |
dc.title | 초소형 유도탄 구동날개 시스템의 플러터 예측에 관한 연구 | - |
dc.title.alternative | Study on the Flutter Prediction of the Miniature Guided-bullet Control Surface System | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 20 | - |
dc.citation.issue | 1 | - |
dc.citation.beginningpage | 148 | - |
dc.citation.endingpage | 157 | - |
dc.citation.publicationname | 한국군사과학기술학회지 | - |
dc.identifier.doi | 10.9766/KIMST.2017.20.1.148 | - |
dc.identifier.kciid | ART002195186 | - |
dc.contributor.localauthor | 방효충 | - |
dc.contributor.nonIdAuthor | 조영기 | - |
dc.contributor.nonIdAuthor | 조한진 | - |
dc.description.isOpenAccess | N | - |
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