کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
777739 | 1463792 | 2012 | 9 صفحه PDF | دانلود رایگان |
The effect of delamination resistance on fatigue crack growth behavior of composite laminates is studied. The strain energy release rate normalized to fatigue delamination resistance (Gcf) is proposed as a controlling parameter to evaluate the fatigue crack growth rates and thresholds. Compared to previously developed Gcf determination method, the compliance approach presented in this paper shows obvious advantages, such as no interruption to the fatigue crack growth and independence on the specimen dimensions. Based on this approach, the fatigue delamination growth rates and thresholds of carbon/bismaleimide composite laminates under mixed I/II mode loadings are determined experimentally.
► Strain energy release rate normalized to fatigue delamination resistance is proposed.
► A compliance approach to determine fatigue delamination resistance is presented.
► Fatigue delamination growth rates of composite laminates under MMB are determined.
► Fatigue thresholds of composite laminates under MMB are determined experimentally.
Journal: International Journal of Fatigue - Volume 40, July 2012, Pages 7–15