Abstract

Abstract This paper describes high-cycle fretting fatigue modelling for 7050-T7451 aluminium alloy using a cohesive zone law. For the sake of crack generation arising from cyclic bending, a bilinear, cycle-dependent cohesive zone law is used including stiffness degradation and reduction of fracture energy with respect to fatigue cycles. The reduction rate of fracture energy is determined with experimental data. Implicit analysis is employed with commercial finite element software. Additionally, bending fretting experiments are performed with unnotched specimens and flat-and-rounded pads. Imposed stress amplitude (S)–number of cycles to failure (N) curves are determined after fretting fatigue tests. Direct comparison between simulation and experimental S–N curves is performed; maximum error is found to be 20% at the 5×104th cycle. It is demonstrated that a proposed method allows simulating fretting fatigue and predicting fretting life of aluminium alloys.

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