全部文献期刊学位论文会议报纸专利标准年鉴图书|学者科研项目
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作者:R. Citarella , M. Perrella
来源:[J].Theoretical and Applied Fracture Mechanics(IF 0.628), 2019, Vol.103Elsevier
摘要:Abstract(#br)This work presents two distinct procedures to perform fatigue crack-growth simulations in a high pressure compressor disc of a turbofan engine.(#br)Two distinct load cases were separately considered as applied to the compressor disc under analysis: one load case was ...
作者:R. Citarella , P. Carlone ...
来源:[J].Engineering Fracture Mechanics(IF 1.413), 2016, Vol.162, pp.38-50Elsevier
摘要:Abstract(#br)In this paper a numerical–experimental procedure useful to numerically assess the fatigue performance of friction stir welded aluminium joints is presented. The impact of manufacturing residual stresses on crack propagation in the joint driven by a remote fatigu...
作者:R. Citarella , M. Lepore ...
来源:[J].Engineering Fracture Mechanics(IF 1.413), 2014, Vol.131, pp.439-453Elsevier
摘要:Abstract(#br)The subject for studies is a steel bar of circular cross-section with straight-fronted edge notch undergoing fatigue loads. Both the optical microscope measurements and the crack opening displacement (COD) method are used to monitor and investigate both crack depth a...
作者:R. Citarella , G. Cricrì ...
来源:[J].Advances in Engineering Software(IF 1.22), 2014, Vol.67, pp.57-69Elsevier
摘要:Abstract(#br)New generation jet engines are subject to severe reduced fuel consumption requirements. This usually leads to thin components in which damage issues such as thermo-mechanical fatigue, creep and crack propagation can be quite important. The combination of mechani...
作者:R. Citarella , P. Carlone ...
来源:[J].Advances in Engineering Software(IF 1.22), 2016, Vol.101, pp.50-59Elsevier
摘要:Abstract(#br)This paper deals with the simulation of multiple crack propagation in friction stir welded butt joints and the aim is to assess the influence of process induced residual stresses on the fatigue behavior of the assembly. The distribution of the process induced residua...
作者:R. Citarella , W. Gentzsch ...
来源:[J].Advances in Engineering Software(IF 1.22), 2016, Vol.101, pp.1-2Elsevier
作者:R. Citarella , G. Cricrì
来源:[J].Applied Composite Materials(IF 1.048), 2014, Vol.21 (3), pp.557-577Springer
摘要:Abstract(#br)This paper concerns the numerical characterization of the fatigue strength of a flat stiffened panel, designed as a fiber metal laminate (FML) and made of Aluminum alloy and Fiber Glass FRP. The panel is full scale and was tested (in a previous work) under fatigue bi...
作者:A. R. Maligno , R. Citarella , V. V. Silberschmidt
来源:[J].Fatigue & Fracture of Engineering Materials & Structures(IF 0.861), 2017, Vol.40 (9), pp.1484-1500Wiley
摘要:Abstract(#br)Fatigue data are generally derived under constant‐amplitude loading conditions, but aircraft components are subjected to variable‐amplitude loading. Without interaction effects, caused by overloads and underloads intermingled in a loading sequence, it could be r...

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