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Understanding progressive failure mechanisms of a wind turbine blade trailing edge section through subcomponent tests and nonlinear FE analysis

机译:通过子组件测试和非线性有限元分析,了解风力涡轮机叶片后缘部分的渐进式失效机理

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This paper presents a comprehensive study on structural failure of a trailing edge section cut from a composite wind turbine blade. The focus is placed on understanding progressive failure behavior of the trailing edge section in subcomponent testing during its entire failure sequence. Digital Image Correlation (DIC) is used to capture buckling deformation and strain distributions of the specimen. Detailed post-test inspection is performed to identify failure modes and failure characteristics. A nonlinear Finite Element (FE) model that accounts for all observed failure modes is developed based on continuum damage mechanics and progressive failure analysis techniques. Multiple structural nonlinearities due to buckling, contact and material failures are included in the model to predict the failure process. The study shows that in addition to the buckling-driven failure phenomenon, the surface contact of sandwich panels contributes to the failure process of the trailing edge section. Foam materials start to fail before the ultimate load-carrying capacity of the specimen is reached, while both composite materials and adhesive materials fail in the post-peak regime. The matrix-dominant failure and delamination develop before the fiber-dominant failure in composite laminates. The proposed FE model captures the progressive failure process of the trailing edge section reasonably well.
机译:本文对从复合材料风力涡轮机叶片切下的后缘部分的结构破坏进行了全面的研究。重点放在了解后缘部分在其整个故障序列期间在子组件测试中的渐进式故障行为。数字图像关联(DIC)用于捕获样品的屈曲变形和应变分布。执行详细的测试后检查以识别故障模式和故障特征。基于连续损伤机制和渐进式故障分析技术,开发了一种非线性有限元(FE)模型,该模型解决了所有观察到的故障模式。该模型包括由于屈曲,接触和材料故障而导致的多种结构非线性,以预测故障过程。研究表明,除了屈曲驱动的破坏现象外,夹心板的表面接触还导致后缘部分的破坏过程。泡沫材料在达到样品的最终承载能力之前就开始失效,而复合材料和粘合材料都在峰后状态下失效。复合材料层压板中,以纤维为主的破坏先于基体破坏和分层。所提出的有限元模型可以很好地捕获后缘部分的渐进破坏过程。

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