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Experimental characterization of high temperature fatigue crack growth in a single crystal superalloy for gas turbine applications

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dc.contributor.author Fedelich, B en
dc.contributor.author Affeldt, E en
dc.contributor.author Harders, H en
dc.contributor.author Marchal, N en
dc.contributor.author Muller, F en
dc.contributor.author Onofrio, G en
dc.contributor.author Remy, L en
dc.contributor.author Toulios, M en
dc.date.accessioned 2014-03-01T02:51:40Z
dc.date.available 2014-03-01T02:51:40Z
dc.date.issued 2008 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/35596
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-84866121638&partnerID=40&md5=b1a00d38eae79fbe1c02731d998b50eb en
dc.subject Crack Growth en
dc.subject Creep-Fatigue en
dc.subject LCF en
dc.subject Oxidation en
dc.subject Single Crystal Superalloy en
dc.title Experimental characterization of high temperature fatigue crack growth in a single crystal superalloy for gas turbine applications en
heal.type conferenceItem en
heal.publicationDate 2008 en
heal.abstract Crack growth tests under Low Cycle Fatigue (LCF) loading have been performed at 950°C with a single crystal superalloy used in gas turbines. The tests have been performed with various specimen shapes and orientations. Also the influence of hold time has been investigated. Some tests have been repeated in vacuum. The results are presented on the basis of the stress intensity factors K and of the C * creep fracture parameter. A beneficial influence of oxidation due to enhanced crack closure could be demonstrated for the low crack growth rates. The tests without hold time are consistent with the small scale yielding hypothesis and the crack growth data can be well described with the K factors. On the other hand, the use of the C * parameter can be shown to rationalize fairly well the crack propagation rates for tests with hold time and for a large range of conditions. en
heal.journalName 17th European Conference on Fracture 2008: Multilevel Approach to Fracture of Materials, Components and Structures en
dc.identifier.volume 2 en
dc.identifier.spage 1336 en
dc.identifier.epage 1343 en


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