Impact characteristics of S2-glass fibre/FM94-epoxy composites under high and cryogenic temperatures: experimental and numerical investigation

Keyphrases

• Numerical Investigation 100%
• High Temperature 100%
• Cryogenic Temperature 100%
• S-glass Fiber 100%
• Epoxy Composites 100%
• Impact Characteristics 100%
• Polymer Plate 66%
• Impact Energy 66%
• Energy Absorption 66%
• Damage Area 66%
• Glass Fiber Reinforced Polymer Composites 66%
• Glass Fiber Reinforced Polymer 66%
• Perforation 33%
• Strong Correlation 33%
• Finite Element Model 33%
• Load-deflection Curve 33%
• Deflection 33%
• Strength-to-weight Ratio 33%
• Failure Mechanism 33%
• Commercial Aircraft 33%
• Damage Mechanism 33%
• Load Energy 33%
• Numerical Model 33%
• Drop Test 33%
• Aerospace Industry 33%
• Wide Temperature Range 33%
• Impact Load 33%
• Low Altitude 33%
• High Altitude 33%
• Epoxy 33%
• Corrosion Resistance 33%
• Abaqus Explicit 33%
• Temperature Environment 33%
• Coupled Temperature 33%
• Glass Fibre Reinforced Polymer Laminate 33%
• Temperature Displacements 33%
• Aircraft Operation 33%
• Load Absorption 33%
• Impact Damage 33%
• Impact Parameter 33%
• Unidirectional Prepreg 33%
• Structural Parts 33%

Engineering

• Epoxy Composite 100%
• S2-Glass 100%
• Cryogenic Temperature 100%
• Reinforced Plastic 100%
• Fibre-Reinforced Polymer Composite 66%
• Energy Absorption 66%
• Damaged Area 66%
• Commercial Aircraft 33%
• Impact Energy 33%
• Impact Loads 33%
• Damage Mechanism 33%
• Strength-to-Weight Ratio 33%
• Numerical Model 33%
• Temperature Range 33%
• Abaqus 33%
• Failure Mechanism 33%
• Experimental Finding 33%
• Impact Test 33%
• Corrosion Resistance 33%
• Impact Damage 33%
• Environment Temperature 33%
• Impact Scenario 33%

Material Science

• Glass Fiber 100%
• Reinforced Plastic 71%
• Aircraft 42%
• Polymer Composite 28%
• Impact Loads 14%
• Corrosion Resistance 14%
• Impact Testing 14%
• Prepreg 14%