各向异性损伤理论与复合材料层板损伤测量的实验研究(二)-复合材料层板损伤测量的实验研究

ANISOTROPIC THOERIES AND EXPERIMENTAL STUDIES OF DAMAGE IN LAMINATED COMPOSITES-Ⅱ

  • 摘要: 鉴于传统的断裂力学无法用于受损复合材料层板,本文探索了损伤力学在复合材料层板中的应用.文内介绍了复合材料层板损伤试验的概况及损伤测试方法,文中三种层板单向拉伸损伤试验结果的分析表明在单向拉伸载荷下基于J.Lemaitre应变等效性假设的损伤能释放率Y2可用于描述受损复合材料层板的力学状态,它的演变方程通常可用Y2=α(σ/σc)β的简单函数形式来描述.对特定的层板,α、β是与初始缺陷无关的常数,可由层板损伤试验确定.试验数据表明在单向拉伸载荷下,临界损伤能释放率对特定的层板也是与初始缺陷无关的常数,反应了材料抗损伤扩展的能力.所有这些结论都为进一步建立完整损伤破坏判据奠定了基础.

     

    Abstract: The application of the anisolropic damage mechanics to composites is explore in this paper.The outline of the damage tests for laminated composites and some measurement methods are briefly presented.The experimental results of three kinds of laminates under uniaxial tension show the damage energy release rate under uniaxial tension,Y2,based on Lemaitre's hypothesis of strain equivalence can be used to describe the mechanical state of damaged laminates.The damage evolution law can be represented by the simple function form of Y2=α(σ/σc)β,where α and β are coefficients which are inedpendent of the shape and size of the initial defect in laminates and can be experimentally determined.The critical damage energy release rate under uniaxial tension,Y2c,represents the capscity against the damage evolution in the laminates and it is independent o:the shape and sizc of initial defects in laminates.

     

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