Failure Model for Rate-Dependent Polymer Matrix Composite Laminates under High-Velocity Impact

2008 ◽  
Vol 21 (3) ◽  
pp. 132-139 ◽  
Author(s):  
Linfa Zhu ◽  
Aditi Chattopadhyay ◽  
Robert K. Goldberg
2007 ◽  
Vol 334-335 ◽  
pp. 73-76
Author(s):  
Gui Ping Zhao ◽  
Zheng Hao Wang ◽  
Jian Xin Zhang ◽  
Chong Du Cho

The response of Carbon/epoxy composites under high velocity impact was investigated experimentally. The strain rate dependent behavior of T300 Carbon/epoxy matrix composite in tension is studied experimentally by split Hopkinson bar technique. Dynamic stress-strain plot was obtained and compared with the quasi-static tensile test results. The results of the study indicate that Carbon/epoxy composites are strain rate dependent materials. Stacking sequence has a significant effect on the material response. Tensile strength of the composites all increased with increasing strain rate. And failure strain decreased when strain rate increased.


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