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Volume 27 Issue 1
Jan.  2001
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Journal of Beijing University of Aeronautics and Astronautics  > 2001  >  27(1): 73-75.
YE Ning, LI Zheng-neng. Finite Element Analysis of Shape Memory Alloys Reinforced Composite Laminate[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(1): 73-75. (in Chinese)
Citation: YE Ning, LI Zheng-neng. Finite Element Analysis of Shape Memory Alloys Reinforced Composite Laminate[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(1): 73-75. (in Chinese)
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Finite Element Analysis of Shape Memory Alloys Reinforced Composite Laminate

  • Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics

  • Received Date: 09 Oct 1999
  • Publish Date: 31 Jan 2001
    Abstract
  • The intelligent structure was made up by which the shape memory alloys (SMAs) be embedded in composite laminate.Applied by the loads or the variation of the temperature,the SMAs would change the distributing of the stress and strain of the structure and the shape of the structure.Because of the non-linear brought with the large displacement of the SMAs,a model is calculated and analyzed with the finite element which used for conducting large deformation analysis of laminated shells,the effect of SMAs is changed for a equivalent mechanical load.The accurate result is obtained.

     

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  • [1] 王 征,吴建生,董建伟,等.形状记忆合金丝增强复合材料的热机特性——智能复合材料研究[J].复合材料学报,1997,14(4):52~56. [2] Bathe K J.Finite element procedures in engineering analysis[M]. Englewood Cliffs:Prentice-Hall,1982. [3] Reddy J N,Chandrashekhara K.Nonlinear analysis of laminated shells including transverse shear strains[J].AIAA Journal, 1985,23(3):440~441. [4] 谢贻权,何福保.弹性和塑性力学中的有限单元法[M].北京:机械工业出版社,1981. [5] 何君毅,林祥都.工程结构非线性问题的数值解法[M].北京:国防工业出版社,1994. [6] 蒋咏秋,陆逢升,顾志建.复合材料力学[M]. 西安:西安交通大学出版社 ,1990.
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