Fatigue crack growth in laser shock peened aerofoils subjected to foreign object damage
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- Type
- dissertation
- Published
- 2011-01-01
- Cited by
- 3
- References
- 131
- Access
- Open access
- OpenAlex
- https://openalex.org/W42315594
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:108008330
Keywords
Damage tolerance, Paris' law, Peening, Structural engineering, Residual stress
References
- Measurement and Understanding of the Level and Effect of Residual Stresses Induced by the Laser Shock Peening Process
- Fatigue behavior of titanium alloys
- Incorporating Residual Stresses in Life Prediction of Turbine Engine Disks
- Mechanical relaxation of localized residual stresses associated with foreign object damage
- The compendium of stress intensity factors
- High Cycle Fatigue: A Mechanics of Materials Perspective
- Weight Functions and Stress Intensity Factor Solutions
- Mixed-mode, high-cycle fatigue-crack growth thresholds in Ti–6Al–4V: I. A comparison of large- and short-crack behavior
- NOVEL PRINCIPLE FOR THE COMPUTATION OF STRESS INTENSITY FACTORS
- Improved High-Cycle Fatigue (HCF) Life Prediction
- Influence of residual stresses on high cycle fatigue strength of Ti–6Al–4V subjected to foreign object damage
- Impact damage on titanium leading edges from small hard objects
- Relaxation of Shot Peening Induced Compressive Stress during Fatigue of Notched Steelsamples
- Limited weld residual stress measurements in fatigue crack propagation: Part I. Complete field representation through least-squares finite-element smoothing
- Improvement of fatigue life of Ti–6Al–4V alloy by laser shock peening
- Fatigue damage and crack growth in aluminium alloys
- Residual Stress and Microstructure Effects on Fatigue Crack Growth in AA2050 Friction Stir Welds
- Notes on Direct Current Potential Drop Calibration for Crack Growth in Compact Tension Specimens
- Investigation of the stress intensity factor changing on the hole crack subject to laser shock processing
- Microstructure evolution associated with adiabatic shear bands and shear band failure in ballistic plug formation in Ti―6Al―4V targets
Cited by
- Fatigue crack growth in complex residual stress fields due to surface treatment and foreign object damage under simulated flight cycles
- Effect of microstructure on the fatigue properties of Ti-6Al-4V titanium alloys
- High Cycle Fatigue Performance in Laser Shock Peened TC4 Titanium Alloys Subjected to Foreign Object Damage
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