Applied Mathematics and Mechanics (English Edition) ›› 1998, Vol. 19 ›› Issue (3): 279-287.

• 论文 • 上一篇    下一篇

PROPERTY DEGRADATION OF ANISOTROPIC COMPOSITELAMINATES WITH MATRIX CRACKING(Ⅰ)──CONSTITUTIVE RELATION DEVELOPING FOR (θm/90n) CRACKED LAMINATES BY STIFFNESS PARTITION

华玉1, 王兴国1, 郦正能2   

  1. 1. Hebei Institute of Technology, Tangshan 063009, P. R. China;
    2. Peking University of Aeronautics and Astronautics, Beding 100083, P. R. China
  • 收稿日期:1995-12-29 修回日期:1997-12-15 出版日期:1998-03-18 发布日期:1998-03-18

PROPERTY DEGRADATION OF ANISOTROPIC COMPOSITE LAMINATES WITH MATRIX CRACKING (I)-CONSTITUTIVE RELATION DEVELOPING FOR (θm/90n) CRACKED LAMINATES BY STIFFNESS PARTITION

Hua Yu1, Wang Xingguo1, Li Zhengneng2   

  1. 1. Hebei Institute of Technology, Tangshan 063009, P. R. China;
    2. Peking University of Aeronautics and Astronautics, Beding 100083, P. R. China
  • Received:1995-12-29 Revised:1997-12-15 Online:1998-03-18 Published:1998-03-18

摘要: The study on property degradation of damaged composite laminates is extendedto anisotropic laminates with matrix cracking. In (I) of the paper, an idea of "stiffnesspatition" is proposed to deal with the puzzle that the in-plane normal response iscoupled with the shear response of the laminates. For (θm/90n.), laminates containingtransversely cracked layers under general in-plane loading, the constitutive relationsare derived and the effective stiffnesses are expressed as the function of crack density.

关键词: composite laminate, anisotropy, damage, constitutive relation, stiffness partition

Abstract: The study on property degradation of damaged composite laminates is extendedto anisotropic laminates with matrix cracking. In (I) of the paper, an idea of "stiffnesspatition" is proposed to deal with the puzzle that the in-plane normal response iscoupled with the shear response of the laminates. For (θm/90n.), laminates containingtransversely cracked layers under general in-plane loading, the constitutive relationsare derived and the effective stiffnesses are expressed as the function of crack density.

Key words: composite laminate, anisotropy, damage, constitutive relation, stiffness partition

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