Micro-CT based trans-scale damage analysis of 3D braided composites with pore defects

Engineering

• Cohesive Zone Model 16%
• Damage Analysis 100%
• Damage Behavior 33%
• Damage Model 16%
• Debonding 16%
• Effective Property 16%
• Failure Mode 16%
• Final Failure 16%
• Scale Analysis 33%
• Scale Damage 100%
• Strength Behavior 16%
• Stress-Strain Relations 16%

Material Science

• Cohesive Zone Model 50%
• Debonding 50%
• Stress-Strain Relations 50%