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Experimental study of wave slamming of sandwich composites panels.

机译:夹芯复合材料板波浪冲击的实验研究。

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摘要

Slamming of ship hull structures was simulated using sandwich composite panels that were repeatedly slammed on to a body of calm water with the main objective of understanding the damage accumulation mechanism and corresponding lifetime. Literature is abundant on ship hull slamming; however, it is limited to single slamming; while damage accumulation and progression under repeated slamming is largely absent. Therefore, an extensive experimental program was carried out to understand damage accumulation and failure in sandwich composites under repeated slamming as a function of deadrise angle and slamming energy. The two model material systems used consisted of polyester foam filled honeycomb sandwich composites and polyurethane foam core sandwich composites. Honeycomb core sandwich composites indicted a significant damage accumulation as a function of increasing slamming energy. Similarly, foam core sandwich composites revealed a gradual but substantial damage accumulation as a function of increasing slamming energy or decreasing deadrise angle. The modes of failure corresponded primarily to local facesheet yielding with evidence of core crushing for the honeycomb core sandwich composites. While, the modes of failure indicated mainly interface tearing, core shear and facesheet buckling in the case of foam core sandwich composites. Interestingly, the peak pressures and strains were observed to occur near the keel while the maximum damage was obtained near the chine at deadrise angles between 15° and 20°; as ship hull design is primarily based on peak pressures, this result is quite significant.
机译:使用夹层复合材料板模拟了船体结构的撞击,该复合材料板反复撞击在平静的水体上,其主要目的是了解损坏的累积机理和相应的寿命。关于船体砰击的文献很多。但是,它仅限于单次撞击;而在反复撞击中,损伤的积累和发展基本上不存在。因此,进行了广泛的实验计划,以了解夹心复合材料在反复砰击下的累积和破坏,其作用是死角和砰击能量的函数。所使用的两种模型材料系统包括填充聚酯泡沫的蜂窝状夹心复合材料和聚氨酯泡沫芯状夹心复合材料。蜂窝芯夹芯复合材料表明,随着撞击能量的增加,损伤累积明显。类似地,泡沫芯夹芯复合材料显示出逐渐但实质性的损伤积累,其是随着砰击能量的增加或死角的减小而变化的。破坏模式主要对应于局部面板屈服,并具有蜂窝状芯夹层复合材料的芯部破碎迹象。同时,在泡沫芯夹芯复合材料的情况下,失效模式主要表现为界面撕裂,芯剪和面板屈曲。有趣的是,观察到峰值压力和应变出现在龙骨附近,而在死角在15°和20°之间时,在脊骨附近获得了最大的破坏。由于船体设计主要基于峰值压力,因此这一结果非常重要。

著录项

  • 作者

    Charca Mamani, Samuel.;

  • 作者单位

    University of Puerto Rico, Mayaguez (Puerto Rico).;

  • 授予单位 University of Puerto Rico, Mayaguez (Puerto Rico).;
  • 学科 Engineering Civil.;Engineering Marine and Ocean.;Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2009
  • 页码 88 p.
  • 总页数 88
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 建筑科学;机械、仪表工业;海洋工程;
  • 关键词

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