DSpace@nitr >
National Institue of Technology- Rourkela >
Journal Articles >

Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/266

Title: Fatigue crack growth delay following overload
Authors: Verma, B B
Kumar, A
Ray, P K
Keywords: aluminium alloys
copper alloys
crack-edge stress field analysis
fatigue cracks
magnesium alloys
Issue Date: 2000
Publisher: Indian Institute of Metals
Citation: Transaction of the Indian Institute of Metals, Vol 53, No 6, P 291-295
Abstract: Fatigue crack growth retardation behaviour on application of single overload cycle in 2024-T3 aluminium-alloy sheet has been studied. It is concluded that a critical value of overloading ratio is required to develop substantial crack growth retardation. The overload induced crack tip plastic zone and crack closure level have been found to control the delay behaviour significantly. It is also found that a power relationship exists between delay cycles and retarded crack length
Description: Copyright for this article belongs to Indian Institute of Metals
URI: http://hdl.handle.net/2080/266
Appears in Collections:Journal Articles

Files in This Item:

File Description SizeFormat
iim-verma-2000.pdf2652KbAdobe PDFView/Open

Show full item record

All items in DSpace are protected by copyright, with all rights reserved.


Powered by DSpace Feedback