Internal shear damage evolution of CFRP laminates ranging from −100 °C to 100 °C using in-situ X-ray computed tomography

Engineering

• Damage Evolution 100%
• Shear Damage 100%
• Carbon Fibre Reinforced Polymer 100%
• Internal Shear 100%
• Room Temperature 60%
• Failure Mechanism 40%
• Carbon Fibre-Reinforced Polymer Composite 40%
• In-Plane Shear 40%
• Plane Shear Failure 40%
• Matrix Cracking 20%
• Tensiles 20%
• Failure Behavior 20%
• Fracture Strain 20%
• Deformation Field 20%
• Failure Mode 20%
• Debonding 20%
• Strain Field 20%
• Damage Area 20%
• Fracture Morphology 20%
• Correlation Method 20%
• Mechanical Damage 20%
• Critical Region 20%
• Delamination Damage 20%
• Fatigue Property 20%
• Stiffness Property 20%
• Modulus of Shear 20%
• Mechanical Property 20%

Material Science

• Delamination 20%