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Development of a physics-based multi-scale progressive damage model for assessing the durability of wind turbine blades

机译:基于物理的多尺度渐进式损伤模型的开发,用于评估风力涡轮机叶片的耐久性

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A physics-based multi-scale progressive damage model was developed for predicting the durability of wind turbine blade structures. Computational micromechanics was coupled within a continuum damage mechanics (CDM) framework, and implemented through a user-defined subroutine within commercial finite element software, for evaluating sub-critical damage evolution and stiffness degradation of the blade structure. The study is the first step in developing an accurate prediction model for composite wind turbines that accounts for the multi-scale nature of damage in rotor blades. The quasi-static and fatigue simulation results demonstrate the ability of the model to predict the evolution of damage in the critical regions of the blade structure, which is an important contribution and essential for increasing the accuracy of damage tolerance analyses and for certification of composite structures. A parametric study of blade geometric parameters also revealed a correlation with damage evolution, providing valuable insight for optimization of blade designs. (C) 2016 Elsevier Ltd. All rights reserved.
机译:建立了基于物理的多尺度渐进式损伤模型,用于预测风力涡轮机叶片结构的耐久性。计算微力学在连续损伤力学(CDM)框架内耦合,并通过商业有限元软件中的用户定义子程序实现,以评估叶片结构的次临界损伤演变和刚度退化。该研究是开发复合风力涡轮机的精确预测模型的第一步,该模型可以解释转子叶片损坏的多尺度性质。准静态和疲劳仿真结果证明了该模型能够预测叶片结构关键区域中损伤的演变,这对提高损伤容限分析的准确性和复合结构的认证具有重要的贡献和至关重要。叶片几何参数的参数研究也揭示了其与损伤演变的相关性,为优化叶片设计提供了宝贵的见识。 (C)2016 Elsevier Ltd.保留所有权利。

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