Bonora, Rafael Gustavo [UNESP]Cornelis Voorwald, Herman Jacobus [UNESP]Hilario Cioffi, Maria Odila [UNESP]Clark, G.Wang, C. H.2014-12-032014-12-032014-01-0111th International Fatigue Congress, Pts 1 And 2. Stafa-zurich: Trans Tech Publications Ltd, v. 891-892, p. 668-673, 2014.1022-6680http://hdl.handle.net/11449/113597This 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.668-673engFatigueCustom 465AISI 4340 steelTrabalho apresentado em evento10.4028/www.scientific.net/AMR.891-892.668WOS:000337767700104Acesso aberto6119671014416126