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A numerical analysis was performed considering elastic behaviour at the crack tip.
A new strain field related cohesive damage law is introduced to describe the behaviour at the crack tip.
The recently modified two-parameter fatigue crack growth model based on the local stress strain material behaviour at the crack tip [1,2] was used to account for the variable amplitude loading effects.
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Plastic deformation within the crack tip region introduces internal stresses that modify subsequent behaviour of the crack and are at the origin of history effects in fatigue crack growth.
Furthermore, hardness indents are performed to examine the crack initiation and the crack propagation behaviour at the interface.
Results showed distinctive strain ratchetting behaviour near the crack tip, leading to progressive accumulation of tensile strain normal to the crack growth plane.
The plastic deformation behaviour at a fatigue crack tip following a tensile overload has been dynamically analysed in pure titanium using an electrochemical method.
FE computations are carried out to calculate stress intensity factor range ΔK at the crack tip for the complex loading configuration, revealing short and long crack propagation behaviours.
Up at the crack.
At the crack of dawn.
I tried very hard not to look at the crack.
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