کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
9796618 | 1514950 | 2005 | 7 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Spherical indentation fatigue cracking
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موضوعات مرتبط
مهندسی و علوم پایه
مهندسی مواد
دانش مواد (عمومی)
پیش نمایش صفحه اول مقاله

چکیده انگلیسی
The maximum principle stress in spherical indentation occurs at the periphery of the contact area. In a purely elastic material, the radial stress component Ïr is tensile whilst the hoop component Ïθ is compressive. The positions of Ïr and Ïθ are reversed in an elastic-plastic material under fully plastic indentation, where Ïr is tensile and Ïθ is compressive. It follows that the relative positions of Ïr and Ïθ vary as the load increases from yield towards the fully plastic deformation. This was demonstrated using a finite element (FE) model, where Ïr, initially positive, was found to increase to a maximum and then decline with increasing load. In contrast, Ïθ was negative at the yield load, but increased monotonically with increasing load to become the maximum principle stress component. The FE analysis is in line with experimental observations of fatigue induced by cyclic indentation. Ring cracks were generated with lower peak loads but fatigue fracture was dominated by radial cracks when cycling was done with higher peak loads. However, shallow ring cracks were observed to form under all loads. It is believed that the shallow ring cracks result from short-range asperity interactions, which are not modelled in the FE analysis.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Materials Science and Engineering: A - Volume 391, Issues 1â2, 25 January 2005, Pages 181-187
Journal: Materials Science and Engineering: A - Volume 391, Issues 1â2, 25 January 2005, Pages 181-187
نویسندگان
F.B. Abudaia, J.T. Evans, B.A. Shaw,