航空学报 > 1994, Vol. 15 Issue (3): 303-309

约束开裂复合材料层板的裂纹密度计算与斜交铺层处理

华玉, 何庆芝, 郦正能, 寇长河   

  1. 北京航空航天大学五系,北京,100083
  • 收稿日期:1993-09-08 修回日期:1993-11-27 出版日期:1994-03-25 发布日期:1994-03-25

CALCULATION OF CRACK DENSITY AND MANIPULATION OF ANGLE-PLIEDLAMINA FOR COMPOSITE LAMINATES WITH CONSTRAINED CRACKING

Hua Yu, He Qingzhi, Li Zhengneng, Kou Changhe   

  1. Fifth Department, Beijing University of Aeronautics and Astronautics,Beijing, 100083
  • Received:1993-09-08 Revised:1993-11-27 Online:1994-03-25 Published:1994-03-25

摘要: 对约束开裂复合材料层板给出随裂纹密度变化的刚度衰减公式。构造了裂纹密度与损伤区应力的关系函数,借助这一函数可由损伤区应力直接预测其刚度衰减。引入两次转轴变换方法,将刚度衰减公式由90°基体开裂推广到应用于±θ层的基体开裂。

关键词: 复合材料层板, 基体开裂, 裂纹密度, 刚度衰减, 斜交铺层

Abstract: Stiffness degradation formulas are given for a composite laminate with constrained cracking.Because the formulas are expressed as a function ofcrack density,the relation between crack density and stresses in the damage zone is constructed so as to predict the stiffness degrada- tion directly from the stress distribution in damage zone. The generalization of the stiffness deg- radation formulas is made for any angle-plied lamina by rotating the coordinate axes twice.

Key words: composite laminate, matrix cracking, crack density, stiffness degradation, angle-plied lamina

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