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دانلود رایگان مقاله انگلیسی رفتارهای خمش خارج از محور و مشخصه شکست کامپوزیت های ۳D بافته شده – الزویر ۲۰۱۹

عنوان فارسی: رفتارهای خمش خارج از محور و مشخصه شکست کامپوزیت های 3D بافته شده
عنوان انگلیسی: Off-axis bending behaviors and failure characterization of 3D woven composites
تعداد صفحات مقاله انگلیسی : 28 تعداد صفحات ترجمه فارسی : ترجمه نشده
سال انتشار : 2019 نشریه : الزویر - Elsevier
فرمت مقاله انگلیسی : PDF نوع مقاله : ISI
نوع نگارش : مقالات پژوهشی (تحقیقاتی) پایگاه : اسکوپوس
کد محصول : E10807 رفرنس : دارد
محتوای فایل : PDF حجم فایل : mb 2
رشته های مرتبط با این مقاله: مهندسی عمران، مهندسی مواد
گرایش های مرتبط با این مقاله: سازه، کامپوزیت
مجله: سازه های کامپوزیتی - Composite Structures
دانشگاه: Key Laboratory of Eco-Textiles - Ministry of Education - Jiangnan University - China
کلمات کلیدی: کامپوزیت 3D بافته شده؛ رفتار خمشی خارج از محور؛ ویژگی های مکانیکی؛ مکانیسم شکست
doi یا شناسه دیجیتال: https://doi.org/10.1016/j.compstruct.2018.10.009
برای سفارش ترجمه این مقاله با کیفیت عالی و در کوتاه ترین زمان ممکن توسط مترجمین مجرب سایت ایران عرضه؛ روی دکمه سبز رنگ کلیک نمایید.
چکیده

Abstract

This paper presents the influence of the off-axis angles on the flexure behaviors of three-dimensional (3D) woven carbon/epoxy composites. Four kind of samples with different angles, 0 degree, 30 degree, 45 degree and 90 degree, are experimentally tested via three-point bending method. The immersion focused ultrasound imaging and micro-computed tomography (Micro-CT) techniques are employed to investigate the deformation and damage mechanisms in the specimens fractured in bending. Results indicate that the stress-deflections of on-axis (0 degree and 90 degree) samples exhibit obvious quasi-brittle behaviors, whereas those of off-axis (30 degree and 45 degree) samples show important ductile features. Furthermore, the dominant failure mechanism of on-axis samples are identified to be inter-ply delamination and fiber bundle fractures, whereas those of off-axis samples are matrix cracks and tows debonding.

نتیجه گیری

Conclusions

3D woven angle-interlock composites have excellent enhanced inter-laminar performance over 2D woven composite laminates and hence are increasing favored for the aircraft and space applications. In the current study, experimental investigations are carried out to assess the effects of off-axis directions on the flexure mechanical behaviors and failure mechanism of 3D woven angle-interlock carbon/epoxy composites. Based on the detailed analysis, following conclusions are made: 1) Compared to 0 degree and 90 degree samples, 30 degree and 45 degree samples show lower flexure strength, initial modulus and larger flexure deflection. Also, the stress-deflections of 0 degree and 90 degree samples exhibit an obvious quasi-brittle behavior, whereas that of 30 degree and 45 degree samples show an important ductile feature. 2) With 30% of the received echo amplitude as the threshold, the calculated damage area proportions of off-axis samples are larger than that of on-axis samples. This phenomenon is because that off-axis samples are capable to produce a larger bending deflection. 3) Under the flexural loading, 30 degree and 45 degree off-axis samples show small localized cracks with little delamination. However, 0 degree and 90 degree on-axis samples exhibit serious damages, mainly including the inter-ply delamination and fiber bundles fracture. For afore-mentioned results, further study is expected to examine how the manipulation and design of wide range of off-axis angles can optimize the maximum stress, dissipation, and damage initiation/evolution. More importantly, developing a reasonable mechanical theory is promising to be exploited for the evaluation of anisotropy characteristics of 3D woven composites.