Mode II Interlaminar fracture toughness of carbon/epoxy laminates

Keyphrases

• Medium Temperature 100%
• Mode II Fracture Toughness 100%
• Post-curing 100%
• Carbon-epoxy Laminate 100%
• Compression Strength 66%
• Temperature System 66%
• Low Temperature 33%
• Curing Conditions 33%
• Flexural Loading 33%
• Interlaminar Fracture 33%
• Maximum Load 33%
• Fracture Behavior 33%
• Delamination Resistance 33%
• SEM Micrographs 33%
• Elevated Temperature 33%
• Carbon-epoxy Composite 33%
• Matrix Materials 33%
• Prepreg 33%
• High Temperature 33%
• Crack Stopper 33%
• Failure Mechanism 33%
• End-notched Flexure 33%
• Delamination 33%
• Total Fracture 33%
• Fracture Toughness 33%
• Dynamic Mechanical Analysis 33%
• Fiber-matrix Interface 33%

Engineering

• Compression Strength 100%
• Delamination 100%
• Fracture Strength 100%
• Carbon-Epoxy Laminate 100%
• System Temperature 100%
• Failure Mechanism 50%
• Fracture Behavior 50%
• Curing Condition 50%
• End-Notched Flexure 50%
• Micrograph 50%
• Matrix Material 50%
• Low-Temperature 50%
• Dynamic Mechanical Analysis 50%
• Matrix Interface 50%
• Energy Engineering 50%
• Elevated Temperature 50%
• Epoxy Composite 50%
• Test Result 50%

Material Science

• Fracture Toughness 100%
• Delamination 100%
• Scanning Electron Microscopy 50%
• Prepreg 50%
• Fracture Behavior 50%
• Dynamic Mechanical Analysis 50%