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Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/139

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contributor.authorVerma, B B-
contributor.authorAtkinson, J D-
contributor.authorKumar, M-
date.accessioned2005-09-20T09:16:05Z-
date.available2005-09-20T09:16:05Z-
date.issued2001-
identifier.citationBulletin of Material Science, Vol 24, No 2, P 231-236en
identifier.urihttp://hdl.handle.net/2080/139-
descriptionCopyright for this article belongs to Indian Academy of Sciencesen
description.abstractFatigue properties of a thermomechanically treated 7475 aluminium alloy have been studied in the present investigation. The alloy exhibited superior fatigue life compared to conventional structural aluminium alloys and comparable stage II crack growth rate. It was also noticed that the fatigue crack initiated from a surface grain and the crack extension was dominated by ductile striations. Analysis also revealed that this alloy possessed fracture toughness and tensile properties superior to that noticed with other structural aluminium alloys. Therefore the use of this alloy can safely reduce the overall weight of the aircraft.en
format.extent452314 bytes-
format.mimetypeapplication/pdf-
language.isoen-
publisherIndian Academy of Sciencesen
subject7475 Aluminium alloyen
subjectfatigue lifeen
subjectfatigue crack growthen
subjectcyclic cleavageen
subjectductile striationsen
titleStudy of fatigue behaviour of 7475 aluminium alloyen
typeArticleen
Appears in Collections:Journal Articles

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