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Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/1216

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contributor.authorMohanty, J R-
contributor.authorVerma, B B-
contributor.authorRay, P K-
date.accessioned2010-04-01T09:17:07Z-
date.available2010-04-01T09:17:07Z-
date.issued2010-
identifier.citationInt. J. Microstructure and Materials Properties, Vol 5, No. 1, P 79-87en
identifier.urihttp://hdl.handle.net/2080/1216-
description.abstractThe determination of crack growth rate from laboratory observations of crack length and number of cycles is certainly a tedious job in order to considerably reduce the scatter in the test results. There are several curve-fitting methods currently in use including the standard ASTM methods. In this work, an alternative technique has been presented which has been found to be efficient in determining the crack growth rate in 2024 T3 and 7020 T7 aluminum alloy specimensen
format.extent215555 bytes-
format.mimetypeapplication/pdf-
language.isoen-
publisherInderscienceen
subjectFatigue crack growth rateen
subjectSpecific growth rateen
subjectIncremental polynomialen
subjectExponential equationen
titleDetermination of fatigue crack growth rate from experimental data: A new approachen
typeArticleen
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