Effect of high-temperature degradation on the mode I critical strain energy release rate of a graphite/epoxy composite

Keyphrases

• Graphite-epoxy Composite 100%
• High Temperature Degradation 100%
• Critical Strain Energy Release Rate 100%
• Graphite 33%
• Rack 33%
• Weight Loss 33%
• Crack Propagation 33%
• Continuous Flow 33%
• Thermal Oxidation 33%
• Composite Materials 33%
• Delamination 33%
• Matrix Materials 33%
• Pre-crack 33%
• Fiber-matrix Interface 33%
• Fiber-reinforced Polymer Composites 33%
• Epoxy Resin Systems 33%
• Double Cantilever Beam Test 33%
• Polymer Matrix Composite Materials 33%
• Continuous Fiber Reinforced Polymer 33%
• Forced Air Convection 33%
• Convection Oven 33%
• Ageing Cycles 33%
• Interfacial Degradation 33%
• Rubber-toughened Epoxy 33%
• Laboratory Air 33%

Engineering

• Epoxy Composite 100%
• Composite Material 100%
• Crack Propagation 50%
• Delamination 50%
• Fiber-Reinforced Polymer 50%
• Matrix Material 50%
• Starters 50%
• Matrix Interface 50%
• Double Cantilever Beam Test 50%
• Forced Air 50%

Material Science

• Composite Material 100%
• Reinforced Plastic 100%
• Graphite Epoxy Composites 100%
• Film 50%
• Oxidation Reaction 50%
• Crack Propagation 50%
• Delamination 50%