Fatigue crack propagation characteristics in SiC_p/6061-T6 composite

Engineering

• Stress Intensity 100%
• Fatigue Crack Propagation 50%
• Particle Size 33%
• Propagation Characteristic 33%
• Aluminum Alloys 33%
• High Stress 16%
• Composite 16%
• Crack Extension 16%
• Threshold Stress 16%
• Powder Metallurgy 16%
• Plastic Zone Size 16%

Physics

• Particle 50%
• Particle Size 33%
• Increasing 16%
• Composite 16%
• Powder Metallurgy 16%

Material Science

• Crack Tip 50%
• Volume Fraction 33%