액체연료 탱크내부의 연료슬로슁 해석 및 최적 배플설계에 관한 연구A Study on the analysis of fuel sloshing in a liquid propellant tank and optimum design of ring baffles
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | 유준태 | ko |
| dc.contributor.author | 연정흠 | ko |
| dc.contributor.author | 윤성기 | ko |
| dc.date.accessioned | 2013-02-27T22:25:07Z | - |
| dc.date.available | 2013-02-27T22:25:07Z | - |
| dc.date.created | 2012-02-06 | - |
| dc.date.created | 2012-02-06 | - |
| dc.date.issued | 1999-08 | - |
| dc.identifier.citation | 한국항공우주학회지, v.27, no.5, pp.60 - 70 | - |
| dc.identifier.issn | 1225-1348 | - |
| dc.identifier.uri | http://hdl.handle.net/10203/71193 | - |
| dc.description.abstract | In this study, sloshing analyst and optimum ring baffle design are studied. Sloshing in axisymmetric tank of arbitrary shape `is modeled by spring-mass-damper model. Sloshing analysis results for tanks in various shape are verified by comparing the results with those obtained from references and commercial code(MSC/NASTRAN). Optimum ring baffle design is also studied. An algorithm is developed with which optimum ring baffle locations and width can be obtained. In this algorithm, the lateral force for a given lateral acceleration history is minimized. | - |
| dc.language | Korean | - |
| dc.publisher | 한국항공우주학회 | - |
| dc.title | 액체연료 탱크내부의 연료슬로슁 해석 및 최적 배플설계에 관한 연구 | - |
| dc.title.alternative | A Study on the analysis of fuel sloshing in a liquid propellant tank and optimum design of ring baffles | - |
| dc.type | Article | - |
| dc.type.rims | ART | - |
| dc.citation.volume | 27 | - |
| dc.citation.issue | 5 | - |
| dc.citation.beginningpage | 60 | - |
| dc.citation.endingpage | 70 | - |
| dc.citation.publicationname | 한국항공우주학회지 | - |
| dc.contributor.localauthor | 윤성기 | - |
| dc.contributor.nonIdAuthor | 유준태 | - |
| dc.contributor.nonIdAuthor | 연정흠 | - |
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