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Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

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Related citation:BIAN Wen-feng,GUO Jing-zhe,DU Shan-yi.Residual strength model for composite laminates[J].Journal of Harbin Institute Of Technology(New Series),2010,17(3):424-426.DOI:10.11916/j.issn.1005-9113.2010.03.025.
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Residual strength model for composite laminates
Author NameAffiliation
BIAN Wen-feng Postdoctoral Flow Station of Materials Science and Engineering,Harbin Institute of Technology,Harbin 150001,China
School of Civil Engineering,Harbin Institute of Technology at Weihai,Weihai 264209,China 
GUO Jing-zhe School of Civil Engineering,Harbin Institute of Technology at Weihai,Weihai 264209,China 
DU Shan-yi Postdoctoral Flow Station of Materials Science and Engineering,Harbin Institute of Technology,Harbin 150001,China 
Abstract:
To research the approach of predicting composites fatigue life,the cumulative fatigue damage of fiber-reinforced plastic laminates(FRP) was investigated,and based on the complex exponential function,the residual strength model was obtained. This model can accurately describe the propagation of cumulative fatigue damage of FRP in three stages,especially in the initial stage and the ceasing stage. Applying this model in the experiment with two loading cycles,it can be found that the prediction result has good coincidence with experimental data. So a reliable residual strength model can be provided for studying the cumulative fatigue damage of FRP.
Key words:  composite material  residual strength  fatigue life  cumulative damage
DOI:10.11916/j.issn.1005-9113.2010.03.025
Clc Number:O346
Fund:

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