Experimental study and computer simulation on degradation of z-pin reinforcement under cyclic fatigue

Keyphrases

• Beam Theory 16%
• Bridging Force 100%
• Bridging Law 16%
• Bridging Traction 16%
• Carbon-epoxy Laminate 16%
• Computer Simulation Results 16%
• Control Condition 16%
• Control Control 16%
• Crack Surface 16%
• Cyclic Fatigue 100%
• Cyclic Loading 16%
• Debonding 16%
• Debonding Force 33%
• Degradation Rate 16%
• Delamination 16%
• Delamination Criterion 16%
• Delamination Growth 16%
• Displacement Control 16%
• Energy Method 16%
• Energy Release Rate 16%
• Exponential Function 16%
• External Force 16%
• Fatigue Data 16%
• Fatigue Degradation 16%
• Fatigue Load 16%
• Force Applied 16%
• Fracture Energy 16%
• Fracture Toughness 16%
• Friction 16%
• Friction Force 33%
• Growth Rate 16%
• Load Control 16%
• Load Cycle 16%
• Load-displacement 16%
• Loading Cycles 33%
• Micromechanical Modeling 16%
• Open Crack 16%
• Pin Reinforcement 100%
• Polymer Laminates 16%
• Power-law Function 16%
• Pullout 16%
• Reinforced 16%
• Through-thickness 16%
• Through-thickness Direction 16%
• Volume Content 16%
• Z-pin 100%

Engineering

• Bridging 33%
• Bridging Force 100%
• Carbon-Epoxy Laminate 16%
• Crack Opening 16%
• Crack Surface 16%
• Cyclic Fatigue 100%
• Cyclic Loading 16%
• Debonding 50%
• Degradation Rate 16%
• Delamination 33%
• Delamination Growth 16%
• Energy Method 16%
• Energy Release Rate 16%
• Experimental Observation 16%
• Exponential Function 16%
• Fatigue Loading 16%
• Fracture Energy 16%
• Fracture Strength 16%
• Friction Force 33%
• Load Control 16%
• Load Cycle 16%
• Loading Cycle 33%
• Max 16%
• Micromechanics Model 16%
• Simulation Result 16%
• Test Result 16%
• Thickness Direction 16%