Towards the understanding the effect of surface integrity on the fatigue performance of silicon carbide particle reinforced aluminium matrix composites

Keyphrases

• Bulk Metal 20%
• Compressive Residual Stress 20%
• Crack Formation 20%
• Crack Growth 20%
• Crack Initiation 20%
• Cutting Parameters 20%
• Cutting Regime 20%
• Defect Damage 20%
• Ductile Regime 40%
• Fatigue Life 60%
• Fatigue Mechanism 20%
• Fatigue Performance 100%
• Finish Milling 20%
• High Cycle Fatigue 20%
• High Feed 40%
• High Stress 20%
• Low Cycle Fatigue 20%
• Low Surface Roughness 20%
• Matrix Materials 20%
• Metal Matrix Composites 60%
• Metallographic 40%
• Particle Behavior 20%
• Particle Reinforced Aluminum Matrix Composites 100%
• Reinforcement Particles 40%
• Residual Stress 20%
• Retardation 20%
• Semi-brittle 60%
• Silicon Carbide Particles 100%
• Stress Damage 20%
• Subsurface Damage 40%
• Surface Anomaly 20%
• Surface Integrity 100%
• Surface Topography 20%
• Three-point Bending Fatigue 20%
• Tool-particle Interaction 20%

Engineering

• Aluminum Matrix 100%
• Brittle Regime 60%
• Compressive Residual Stress 20%
• Crack Growth 20%
• Cutting Parameter 20%
• Defects 20%
• Failure Mechanism 20%
• Fatigue Failure 20%
• Fatigue Life 60%
• Fatigue Performance 100%
• High Cycle Fatigue 20%
• Induced Surface 20%
• Initiation of Crack 20%
• Low Cycle Fatigue 20%
• Matrix Material 20%
• Mechanical Fatigue Test 20%
• Metal Matrix Composite 60%
• Morphologic 20%
• Point Bending 20%
• Residual Stress 20%
• Retardation 20%
• Subsurface 40%
• Surface Anomaly 20%
• Surface Integrity 100%
• Surface Topography 20%