A generalized plane-strain crack density-based model for evaluating the finite fracture toughness of composite laminates

Engineering

• Crack Density 100%
• Generalized Plane Strain 100%
• Fracture Strength 100%
• Experimental Result 50%
• Stress Field 50%
• Closed Form Solution 50%
• Matrix Cracking 50%
• Stiffness Degradation 50%
• Composite Ply 50%

Material Science

• Density 100%
• Fracture Toughness 100%
• Composite Laminate 100%
• Laminated Composite 33%
• Composite Material 33%
• Matrix Cracking 33%
• Stress Field 33%
• Materials Property 33%

Keyphrases

• Density Model 100%
• Plane Strain Crack 100%
• Derived Relations 33%
• Stress Stiffness 33%
• Master Plots 33%