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首页> 外文期刊>Advances in Aircraft and Spacecraft Science >Implementation and assessment of advanced failure criteria for composite layered structures in FEMAP
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Implementation and assessment of advanced failure criteria for composite layered structures in FEMAP

机译:FEMAP中复合层状结构的高级破坏准则的实施和评估

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摘要

AMOSC (Automatic Margin Of Safety Calculation) is a SW tool which has been developed to calculate the Mure index of layered composite structures by referring to the cutting edge state-of-the-art LaRC05 criterion. The stress field is calculated by a finite element code. AMOSC allows the user to calculate the Mure index also by referring to the classical Hoffman criterion (which is commonly applied in the aerospace industry). When developing the code, particular care was devoted to the computational efficiency of the code and to the automatic reporting capability. The tool implemented is an API which has been embedded into Femap Siemens SW custom tools. Then, a user friendly graphical interface has been associated to the API. A number of study-cases have been solved to validate the code and they are illustrated through this work. Moreover, for the same structure, the differences in results produced by passing from Hoffman to LaRC05 criterion have been identified and discussed. A number of additional comparisons have thus been produced between the results obtained by applying the above two criteria. Possible future developments could explore the sensitivity of the failure indexes to a more accurate stress field inputs (e.g. by employing finite elements formulated on the basis of higher order/hierarchical kinematic theories).
机译:AMOSC(安全边际自动计算)是一种SW工具,已经开发出来,可以通过参考最新的LaRC05准则来计算层状复合结构的Mure指数。应力场由有限元代码计算。 AMOSC还允许用户通过参考经典的霍夫曼准则(在航空航天行业中普遍使用)来计算Mure指数。在开发代码时,要特别注意代码的计算效率和自动报告功能。所实现的工具是已嵌入Femap Siemens SW自定义工具中的API。然后,用户友好的图形界面已与API关联。解决了许多研究案例以验证代码,并通过这项工作进行了说明。此外,对于相同的结构,已经确定并讨论了从霍夫曼转换为LaRC05准则产生的结果差异。因此,在通过应用上述两个标准获得的结果之间进行了许多其他比较。未来可能的发展可能会探索失效指标对更准确的应力场输入的敏感性(例如,通过使用基于高阶/分层运动学理论制定的有限元)。

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