首页> 外文会议>Congress of the International Council of the Aeronautical Sciences;ICAS 2008 >SURVEY OF FEASIBLE NUMERICAL APPROACHES TO ANALYSE THE BEHAVIOUR OF A COMPOSITE SKIN PANEL DURING A WATER IMPACT
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SURVEY OF FEASIBLE NUMERICAL APPROACHES TO ANALYSE THE BEHAVIOUR OF A COMPOSITE SKIN PANEL DURING A WATER IMPACT

机译:水冲击过程中复合皮肤面板行为的可行数值方法研究

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摘要

Water impacts are likely to have tragic consequences for the passengers of helicopters. Most of the passive safety devices developed for helicopter crashworthiness are designed for ground impact. When impacting a solid or a soft surface, impact loads are rather different and therefore energy absorption devices developed for ground impact are not effective during a water impact.In order to collect reliable data for numerical model validation, water impact drop tests were carried out: a Carbon Fiber Reinforced Plastic panel, similar to modern aircraft skin panels, was mounted on a specific test device and tested. Impact decelerations and deformations of the panels were measured. Afterwards, numerical models of the tests were created. Finite element and meshless approaches were used to model the water region. Eventually, a close experimental-numerical correlation was obtained for each model in terms of impact dynamics, decelerations and deformations. The main features of the event and the differences between the four numerical approaches were discussed. Guidelines for further investigations were also drawn.
机译:水的冲击可能会对直升机的乘客造成悲剧性的后果。为防止直升机坠毁而开发的大多数被动安全装置都是为地面撞击而设计的。当冲击坚固或柔软的表面时,冲击载荷会大不相同,因此为地面冲击而开发的能量吸收装置在水冲击期间无效。 为了收集用于数值模型验证的可靠数据,进行了水冲击试验:将类似于现代飞机蒙皮面板的碳纤维增强塑料面板安装在特定的测试设备上并进行测试。测量了面板的冲击减速度和变形。之后,创建测试的数值模型。使用有限元和无网格方法对水域进行建模。最终,在冲击动力学,减速度和变形方面,每个模型都获得了紧密的实验-数值相关性。讨论了事件的主要特征以及四种数值方法之间的差异。还制定了进一步调查的指南。

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