کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
4912107 | 1428539 | 2017 | 28 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Effect of distance between impact point and hole position on the impact fatigue strength of composite laminates
ترجمه فارسی عنوان
اثر فاصله بین نقطه ضربه و موقعیت سوراخ شده بر مقاومت خستگی اثر چند لایه کامپوزیت
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کلمات کلیدی
کامپوزیت قدرت ضربه، مشخصات مکانیکی، سوراخ،
موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی عمران و سازه
چکیده انگلیسی
An impact fatigue study was performed to evaluate the effect of the distance between the impact point and the hole on the fatigue life of glass fibre/epoxy laminates. For this purpose, experimental tests were carried out in square plates and for the distances of 0, 5, 10 and 20Â mm, from the impact point. The results were compared with the ones obtained in plates without hole. It was possible to conclude that the fatigue life decreased, comparatively to the control samples, about 10.9%, 40%, 63.6% and 69.1% for the distances of 20Â mm, 10Â mm, 5Â mm and 0Â mm, respectively. Higher distances promote higher maximum loads and elastic restitution, but an opposite trend in terms of maximum displacement. For example, it was found for 20Â mm a maximum load around 5.54Â kN, a displacement of about 4.4Â mm and an elastic energy of 59.2%, while for 0Â mm these values were about 4.59Â kN, 5.7Â mm and 40.4%, respectively. In terms of multi-impacts, the damage severity is also very influenced by the distance. For small distances the damage progresses quickly, while three stages can be found for the control samples and for the distance of 20Â mm.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Composite Structures - Volume 168, 15 May 2017, Pages 33-39
Journal: Composite Structures - Volume 168, 15 May 2017, Pages 33-39
نویسندگان
R.A.M. Santos, P.N.B. Reis, M.J. Santos, C.A.C.P. Coelho,