航空学报 > 1995, Vol. 16 Issue (4): 118-121

随机取向短纤维增强SMC复合材料疲劳损伤模型

张子龙1, 张双寅2   

  1. 1. 北京航空材研究所7室;2. 中国科学院力学所12室
  • 收稿日期:1993-09-28 修回日期:1994-05-05 出版日期:1995-08-25 发布日期:1995-08-25

A FATIGUE DAMAGE MODEL FOR RANDOM SHORT FIBER COMPOSITE SMC

Zhang Zilong1, Zhang Shuangyin2   

  1. 1. Faculty 7, Beijing Institute of Aeronautical Materials Beijing,100095;2. Faculty 12, Institute of Mechanics,Chinese Academy of Sciences Beijing,10080
  • Received:1993-09-28 Revised:1994-05-05 Online:1995-08-25 Published:1995-08-25

摘要: 讨论了复合材料疲劳损伤的数学描述方法,引用等效模量随疲劳过程的降低作为损伤的度量,借助于连续介质损伤力学CDM,建立起损伤速率与循环次数之间的幂函数关系。试验发现,疲劳损伤的演变可分为3个阶段,而在一定的应力水平下,稳定扩展的第2阶段占据主导地位,为从理论上预测疲劳寿命成为可能。

Abstract: The characterization of fatigue damage of composite materials was discussed.The degradation of effective modulus was used as a measurement of damage. Using continuous damage mechanics(CDM) theory, a power relationship is setup between the damage rate (d D /d n ) and cyclic numbers. This provides a well model for the life prediction of composite materials under cyclic loading. Experimental procedures were also performed in order to investigate the damage development during fatigue process.It was found that damage development shows three different stages. This makes it possible to describe fatigue damage theoretically.

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