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Theoretical model for laminated composite beam consisting of multiple superelastic shape memory alloy layers

机译:多层超弹性形状记忆合金层组成的层合组合梁的理论模型

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摘要

A novel theoretical model for a laminate cantilever beam consisting of numerous superelastic shape memoryalloy (SMA) layers, based on the ZM model and Timoshenko theory is introduced. The mathematical equations arefirst developed to predict and describe the internal material structure of laminated beam, according to the solid phasetransformation in SMA layers. Then, the theoretical expression of the moment and shear force for a superelasticSMA composite cantilever beam is derived. The proposed model is validated against a 3D finite element analysismodel (FEA), giving very good agreement in each case. The moment-curvature response, and distribution ofmartensite volume fraction and axial stress along the beam length are investigated.
机译:基于ZM模型和Timoshenko理论,提出了一种由多层超弹性形状记忆\合金\ SMA组成的叠层悬臂梁的理论模型。首先根据SMA层中的固相转变,开发了数学方程来预测和描述层压梁的内部材料结构。然后,推导了超弹性\ r \ nSMA复合悬臂梁的弯矩和剪力的理论表达式。所提出的模型已通过3D有限元分析\ r \ n模型(FEA)进行了验证,在每种情况下均具有很好的一致性。研究了梁的弯矩-曲率响应,马氏体体积分数和轴向应力的分布。

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  • 来源
  • 会议地点 0277-786X;1996-756X
  • 作者

    N. V. Viet; W. Zaki; R. Umer;

  • 作者单位

    Department of Aerospace Engineering, Khalifa University of Science and Technology, Abu Dhabi, UAE nguyen.viet@kustar.ac.ae;

    Department of Aerospace Engineering, Khalifa University of Science and Technology, Abu Dhabi, UAE;

    Department of Aerospace Engineering, Khalifa University of Science and Technology, Abu Dhabi, UAE;

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