...
首页> 外文期刊>International journal of impact engineering >Barely visible impact damage in scaled composite laminates: Experiments and numerical simulations
【24h】

Barely visible impact damage in scaled composite laminates: Experiments and numerical simulations

机译:鳞片复合层压板中几乎看不见的冲击损伤:实验和数值模拟

获取原文
获取原文并翻译 | 示例
           

摘要

This paper investigates the effect of size and complexity of composite structures on the formation of low velocity impact damage via experimental tests and numerical modelling. The ASTM standard low-velocity impact test and a scaled-up version of the test were conducted. A novel numerical technique is presented that combines 3D solid and thin 2D shell elements for modelling different domains to achieve a high level of fidelity locally under the impact location, whilst achieving good computational efficiency for large structures. Together with the experimental studies at the different scales, the predictive capability of the numerical models was systematically validated. This modelling method demonstrated an advanced computational efficiency without compromising predictive accuracy. The models are applied to a case study of low-velocity impact of a large-scale stringer-stiffened panel, showing this modelling approach to be suitable for predicating low-velocity impact damage and structural response of laminated composites over a range of sizes and complexities. (C) 2017 Elsevier Ltd. All rights reserved.
机译:本文通过实验测试和数值模拟研究了复合结构的尺寸和复杂性对低速冲击损伤形成的影响。进行了ASTM标准低速冲击试验和试验的放大版本。提出了一种新颖的数值技术,该技术结合了3D实体和薄2D壳体元素来对不同的区域进行建模,从而在碰撞位置下局部实现了高保真度,同时为大型结构实现了良好的计算效率。结合不同规模的实验研究,系统地验证了数值模型的预测能力。这种建模方法展示了先进的计算效率,而不会影响预测精度。该模型被应用于大型纵梁加劲板的低速冲击的案例研究,表明该建模方法适用于预测层状复合材料在各种尺寸和复杂度范围内的低速冲击损伤和结构响应。 (C)2017 Elsevier Ltd.保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号