Analysis of delamination in laminates with angle-ply matrix cracks: Onset of damage and residual stiffness properties

Engineering

• Matrix Crack 100%
• Stiffness Property 100%
• Strain-Energy Release Rate 100%
• Local Delamination 100%
• Residual Stiffness 100%
• Ply Angle 100%
• Induced Delamination 100%
• Delamination 100%
• Two Dimensional 50%
• Shear Lag 50%
• Failure Process 50%
• Intralaminar 50%
• Crack Density 50%
• Fatigue Loading 50%
• Axis Ply 50%
• Damage Mode 50%
• In-Plane Loading 50%
• Delamination Area 50%
• Laminate Stiffness 50%
• Representative Segment 50%
• Fracture Criterion 50%
• Matrix Cracking 50%
• Symmetric Laminate 50%
• Ply Stress 50%
• Ply Orientation 50%

Material Science

• Delamination 100%
• Composite Laminate 28%
• Density 14%
• Matrix Cracking 14%