FATIGUE IN CUSTOM 465 STAINLESS STEEL FOR AERONAUTIC APPLICATION

dc.contributorUniversidade Estadual Paulista (UNESP)
dc.creatorCornelis Voorwald, Herman Jacobus
dc.creatorBonora, Rafael Gustavo
dc.creatorHilario Cioffi, Maria Odila
dc.creatorSilvaGomes, J. F.
dc.creatorVaz, MAP
dc.date2015-03-18T15:57:01Z
dc.date2016-10-25T20:36:19Z
dc.date2015-03-18T15:57:01Z
dc.date2016-10-25T20:36:19Z
dc.date2012-01-01
dc.date.accessioned2017-04-06T07:21:54Z
dc.date.available2017-04-06T07:21:54Z
dc.identifierIcem15: 15th International Conference On Experimental Mechanics. Porto: Inegi-inst Engenharia Mecanica E Gestao Industrial, 6 p., 2012.
dc.identifierhttp://hdl.handle.net/11449/117844
dc.identifierhttp://acervodigital.unesp.br/handle/11449/117844
dc.identifierWOS:000320722901130
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/928491
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 was tested in axial fatigue. The objective is to compare the behavior of the Custom 465 stainless steel with plated AISI 4340 steel coated with cadmium. Fractographic analysis was conducted using scanning electron microscopy. X-ray diffraction method was used to determine the residual stress field induced by shot peening.
dc.languageeng
dc.publisherInegi-inst Engenharia Mecanica E Gestao Industrial
dc.relationIcem15: 15th International Conference On Experimental Mechanics
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectfatigue
dc.subjectCustom 465
dc.subjectshot peening
dc.titleFATIGUE IN CUSTOM 465 STAINLESS STEEL FOR AERONAUTIC APPLICATION
dc.typeOtro


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