논문 상세보기
The Study on the Curvature Changes by the Experimental Impact Characteristics of Laminated Shells KCI 등재
Yang, Hyun Soo
- 언어ENG
- URLhttps://db.koreascholar.com/Article/Detail/230522
4,000원
한국기계항공기술학회지(구 한국기계기술학회지)
(Journal of the Korean Society of Mechanical and Aviation Technology)
제15권 제1호 (2013.02)
pp.15-19
pp.15-19
한국기계항공기술학회(구 한국기계기술학회)
(Korean Society of Mechanical Technology)
초록
The object of this study is to investigate the penetration characteristics according to the change of stacking sequences and curvature radius in the composite laminated shell. They are staked to [02/902]S and [0/902/0]s, their interlaminar number are two and four. We manufactured the composite laminated shells with various curvature radiuses. Curvature radiuses of composite shell are 100, 150, 200mm and ∞ (it's meaning flat-plate). In general, the kinetic energy before and after impact increased linearly in all specimens, and the absorbed energy of the specimen [02/902]S with a small number of the interlaminars was higher than specimen [0/902/0]s.
키워드
관통특성Penetration Characteristics적층구성Stacking Sequence곡률반경Curvature Radius복합재 적층 쉘Composite Laminated Shell흡수 에너지Absorbed Energy탄소섬유 강화수지Carbon Fiber Reinforced Plastics
목차
Abstract
1. Introduction
2. Method
2.1 Manufacturing specimen
2.2 Experimental Method
3. Experimental results and examination
3.1 The impact velocities and penetration characteristics
3.2 Comparison of the energy absorption due to the curvature
3.3 Cross-sectional shape and penetrating mode of the specimen
4. Conclusion
References
1. Introduction
2. Method
2.1 Manufacturing specimen
2.2 Experimental Method
3. Experimental results and examination
3.1 The impact velocities and penetration characteristics
3.2 Comparison of the energy absorption due to the curvature
3.3 Cross-sectional shape and penetrating mode of the specimen
4. Conclusion
References
저자
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