کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
7889553 | 1509863 | 2018 | 10 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Ply thickness dependence of the intralaminar fracture in thin-ply carbon-epoxy laminates
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
مهندسی مواد
سرامیک و کامپوزیت
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: Ply thickness dependence of the intralaminar fracture in thin-ply carbon-epoxy laminates Ply thickness dependence of the intralaminar fracture in thin-ply carbon-epoxy laminates](/preview/png/7889553.png)
چکیده انگلیسی
The effect of ply thickness t in intralaminar fracture of unidirectional thin-ply carbon-epoxy laminates is characterized by testing double cantilever beam (DCB) and compact tension (CT) specimens with different t. While the average intralaminar energy release rate (ERR) at initiation is found equal to the corresponding interlaminar values, the steady-state intralaminar ERRs, only reached in the DCB configuration, are approximately three times higher than the corresponding interlaminar values. Due to changes in the extent of bridging, intralaminar steady-state ERRs are â¼30% higher in thick-ply (tâ¯=â¯0.150â¯mm) than in thin-ply laminates (tâ¯=â¯0.030â¯mm). Thin-ply composite laminates exhibit a faster ERR growth with crack length, and for DCB, reach steady-state at a much shorter crack extension than thick-ply composites. Traction profiles, due to bridging, are identified using R-curves and implemented in cohesive element simulations to predict intralaminar fracture of DCB and CT specimens. The experimental and simulated load-displacement responses are in good agreement.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Composites Part A: Applied Science and Manufacturing - Volume 109, June 2018, Pages 95-104
Journal: Composites Part A: Applied Science and Manufacturing - Volume 109, June 2018, Pages 95-104
نویسندگان
G. Frossard, J. Cugnoni, T. Gmür, J. Botsis,