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
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.
- Publisher
- 한국항공우주학회
- Issue Date
- 1999-08
- Language
- Korean
- Citation
한국항공우주학회지, v.27, no.5, pp.60 - 70
- ISSN
- 1225-1348
- Appears in Collection
- ME-Journal Papers(저널논문)
- Files in This Item
- There are no files associated with this item.
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