مشخصه شکست کامپوزیت های 3D بافته شده
ترجمه نشده

مشخصه شکست کامپوزیت های 3D بافته شده

عنوان فارسی مقاله: رفتارهای خمش خارج از محور و مشخصه شکست کامپوزیت های 3D بافته شده
عنوان انگلیسی مقاله: Off-axis bending behaviors and failure characterization of 3D woven composites
مجله/کنفرانس: سازه های کامپوزیتی - Composite Structures
رشته های تحصیلی مرتبط: مهندسی عمران، مهندسی مواد
گرایش های تحصیلی مرتبط: سازه، کامپوزیت
کلمات کلیدی فارسی: کامپوزیت ۳D بافته شده؛ رفتار خمشی خارج از محور؛ ویژگی های مکانیکی؛ مکانیسم شکست
کلمات کلیدی انگلیسی: ۳D woven composites، Off-axis bending behaviors، Mechanical properties، Failure mechanism
نوع نگارش مقاله: مقاله پژوهشی (Research Article)
شناسه دیجیتال (DOI): https://doi.org/10.1016/j.compstruct.2018.10.009
دانشگاه: Key Laboratory of Eco-Textiles - Ministry of Education - Jiangnan University - China
صفحات مقاله انگلیسی: 28
ناشر: الزویر - Elsevier
نوع ارائه مقاله: ژورنال
نوع مقاله: ISI
سال انتشار مقاله: 2019
ایمپکت فاکتور: 4/345 در سال 2017
شاخص H_index: 115 در سال 2019
شاخص SJR: 1/905 در سال 2017
شناسه ISSN: 0263-8223
شاخص Quartile (چارک): Q1 در سال 2017
فرمت مقاله انگلیسی: PDF
وضعیت ترجمه: ترجمه نشده است
قیمت مقاله انگلیسی: رایگان
آیا این مقاله بیس است: خیر
کد محصول: E10807
فهرست مطالب (انگلیسی)

Abstract

1- Introduction

2- Experimental details

3- Results and discussion

4- Conclusions

References

بخشی از مقاله (انگلیسی)

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.

Introduction

3D woven preforms and their composites as structural components are being used increasingly for the aircraft and space applications owing to their excellent out-of-plane properties for delamination resistance and impact damage resistance [1-3]. In the past few years, researchers have mainly focused on the in-plane mechanical behaviors, while the bending large-deformation and failure mechanisms are still systematically unclear. This can be attributed to the variability and complexity of the microstructure, and the limitation of the experimental technology. Furthermore, 3D woven composites are highly anisotropic, leading to the obvious orientation-dependence. In practice, 3D woven composite materials acquire the load carrying capacities not only along the two principal directions coinciding with the warp and weft axes, but also along any other bias directions. Consequently, an improved understanding of the off-axis bending behaviors and failure characterizations of 3D woven composites will be helpful for researchers in designing and constructing the high-performance materials.