مشخصات مقاله | |
ترجمه عنوان مقاله | مطالعه شاخص های مختلف برای تعیین حد فرسودگی برای کامپوزیت های کربن / اپوکسی بافته شده تحت روش گرمایش خودی |
عنوان انگلیسی مقاله | A study of various indicators to determine the fatigue limit for woven carbon/epoxy composites under self heating methodology |
انتشار | مقاله سال 2018 |
تعداد صفحات مقاله انگلیسی | 12 صفحه |
هزینه | دانلود مقاله انگلیسی رایگان میباشد. |
پایگاه داده | نشریه الزویر |
نوع نگارش مقاله |
مقاله پژوهشی (Research Article) |
مقاله بیس | این مقاله بیس نمیباشد |
نوع مقاله | ISI |
فرمت مقاله انگلیسی | |
ایمپکت فاکتور(IF) |
0.970 در سال 2018 |
شاخص H_index | 51 در سال 2019 |
شاخص SJR | 0.277 در سال 2018 |
شناسه ISSN | 1877-7058 |
مدل مفهومی | ندارد |
پرسشنامه | ندارد |
متغیر | ندارد |
رفرنس | دارد |
رشته های مرتبط | مهندسی پلیمر، مهندسی مکانیک |
گرایش های مرتبط | مهندسی مواد مرکب، ساخت و تولید |
نوع ارائه مقاله |
ژورنال و کنفرانس |
مجله / کنفرانس | پروسیدیای مهندسی – Procedia Engineering |
دانشگاه | Machine Design Section, Department of Mechnical Engineering, Indian Institute of Technology Madras, Chennai – 600036, India |
کلمات کلیدی | حد تحمل، گرمایش خودی، رفتار انتقال گرما، کربن / اپوکسی، بافته شده، کامپوزیت |
کلمات کلیدی انگلیسی | endurance limit ; self-heating ; heat transfer behavior ; carbon/epoxy, woven, composite |
شناسه دیجیتال – doi |
https://doi.org/10.1016/j.proeng.2018.02.018 |
کد محصول | E12461 |
وضعیت ترجمه مقاله | ترجمه آماده این مقاله موجود نمیباشد. میتوانید از طریق دکمه پایین سفارش دهید. |
دانلود رایگان مقاله | دانلود رایگان مقاله انگلیسی |
سفارش ترجمه این مقاله | سفارش ترجمه این مقاله |
فهرست مطالب مقاله: |
Abstract
1. Introduction 2. Self-Heating Methodology 3. Experimentation 4. Results and Discussion 5. Conclusion Acknowledgements Reference |
بخشی از متن مقاله: |
Abstract
The main objective of this paper is to present three indicators to determine the fatigue limit of woven carbon-fiber epoxy-matrix laminates using the Self-Heating test method. The approach adopted in the self-heating methodology consists usually in plotting the heat transfer indicator values versus the maximum stress values. This plot is named the self-heating curve and from the profile of the self-heating curve, one can identify the fatigue limit. During the self-heating experiments, the temperature of the specimen increases with the number of applied cycles and then stabilizes after a certain number of cycles. In this study a novel “peak-temperature point” approach was identified as the most suitable methodology to determine the fatigue limit for a class of composite materials. The paper also sheds some light on how a suitable approach can be chosen to uphold the economic aspect of the self-heating methodology. The purpose of the present paper is to validate this approach for an impacted laminate. Introduction CFRP structures have mostly replaced aluminium and steel, primarily due to their high strength and high stiffness to weight ratios, which are more than five times greater than conventional structural materials. Therefore, it is of utmost important for the scientific society to clearly understand the mechanical properties of these fibre reinforced composite materials, and especially the fatigue properties. CFRP composites are highly anisotropic and hence have complex failure mechanisms. Wöhler curves have been used to estimate the fatigue life of metals as well as composite materials [1-4]. The determination of the fatigue limit of materials is mostly time consuming and expensive. To have a quick determination of fatigue limit of materials, a quite new methodology named the SelfHeating methodology was adopted by several researchers for metals [5-9] and composites [10-11]. This methodology has been proven successful in evaluating the fatigue limit of unidirectional and woven CFRP materials without any inherent flaws. The fatigue experiments based on the self-heating methodology take only a couple of hours (maximum of one day) in comparison to the conventional fatigue tests which takes months to produce results. |