An experimental study of the influence of fibre-matrix interface on fatigue tensile strength of notched composite laminates

Keyphrases

• Tensile Strength 100%
• Fiber-matrix Interface 100%
• Composite Laminates 100%
• Interfacial Adhesion 100%
• Residual Strength 100%
• Notched Composite Laminate 100%
• Surface Treatment 50%
• Carbon Fiber 50%
• Composite System 50%
• Flexural Strength 50%
• Circular Hole 50%
• Cyclic Loading 50%
• Fiber Matrix 50%
• Cyclic Fatigue 50%
• Damage Mechanism 50%
• Polymer-matrix Composites 50%
• Load Level 50%
• Material System 50%
• Fatigue Experiment 50%
• C-scan 50%
• SEM Fractography 50%
• Fatigue Residual Strength 50%
• Notched Laminates 50%

Engineering

• Tensiles 100%
• Matrix Interface 100%
• Interfacial Adhesion 100%
• Ultimate Tensile Strength 100%
• Material System 50%
• Circular Hole 50%
• Damage Mechanism 50%
• Load Level 50%
• Polymer Matrix Composite 50%
• Cyclic Fatigue 50%
• Fractography 50%
• Cyclic Loading 50%
• Notched Laminate 50%

Material Science

• Residual Strength 100%
• Composite Laminate 100%
• Ultimate Tensile Strength 100%
• Flexural Strength 33%
• Fractography 33%
• Scanning Electron Microscopy 33%
• Carbon Fiber 33%
• Complex Systems 33%
• Reinforced Plastic 33%