Pages that link to "Item:Q2325487"
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The following pages link to Analysis of two-dimensional fatigue crack propagation in thin aluminum plates using the Paris law modified by a closure concept (Q2325487):
Displaying 6 items.
- Modeling of fatigue crack growth in notched fiber metal laminates (Q374393) (← links)
- Fracture mechanics analysis for residual stress and crack closure corrections (Q994037) (← links)
- A numerical analysis of constraint effects in fatigue crack growth by use of an irreversible cohesive zone model (Q1959843) (← links)
- A numerical lattice method to characterize a contact fatigue crack growth and its Paris coefficients using configurational forces and stress-life curves (Q1986297) (← links)
- PREDICTIONS OF ANISOTROPY AFFECTED FATIGUE CRACK PROPAGATION PATHS IN PURE ALUMINUM SHEETS (Q3055997) (← links)
- Comprehensive model for predicting the crack initiation and propagation life of the TC4 titanium alloy considering the closure effect (Q6136397) (← links)