dc.contributorUniversidade Estadual Paulista (UNESP)
dc.creatorBonora, Rafael Gustavo
dc.creatorCornelis Voorwald, Herman Jacobus
dc.creatorHilario Cioffi, Maria Odila
dc.creatorClark, G.
dc.creatorWang, C. H.
dc.date2014-12-03T13:11:49Z
dc.date2016-10-25T20:15:16Z
dc.date2014-12-03T13:11:49Z
dc.date2016-10-25T20:15:16Z
dc.date2014-01-01
dc.date.accessioned2017-04-06T06:35:08Z
dc.date.available2017-04-06T06:35:08Z
dc.identifier11th International Fatigue Congress, Pts 1 And 2. Stafa-zurich: Trans Tech Publications Ltd, v. 891-892, p. 668-673, 2014.
dc.identifier1022-6680
dc.identifierhttp://hdl.handle.net/11449/113597
dc.identifierhttp://acervodigital.unesp.br/handle/11449/113597
dc.identifier10.4028/www.scientific.net/AMR.891-892.668
dc.identifierWOS:000337767700104
dc.identifierhttp://dx.doi.org/10.4028/www.scientific.net/AMR.891-892.668
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/924338
dc.descriptionThis project was originated from the national aircraft industry requirements to reduce the use of coated materials with electroplated chromium or cadmium that produce waste, which is harmful to health or the environment. The selected material is a Custom 465 stainless steel used in the aeronautical field due to its high mechanical strength. Considering the load sustained by the wheel axis of the landing gear, the Custom 465 is tested in axial fatigue. The objective is to compare the behavior of the Custom 465 with plated AISI 4340 steel coated with cadmium. X-ray diffraction method was used to determine the residual stress field induced by shot peening.
dc.languageeng
dc.publisherTrans Tech Publications Ltd
dc.relation11th International Fatigue Congress, Pts 1 And 2
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectFatigue
dc.subjectCustom 465
dc.subjectAISI 4340 steel
dc.titleInfluence of shot peening on the fatigue strength of Custom 465 stainless steel for aeronautic application
dc.typeOtro


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