Modelling damage due to low speed impact in laminated composites of toughened interfaces through 'ex situ' technique

Keyphrases

• Laminated Composites 100%
• Low-speed Impact 100%
• Ex Situ Technique 100%
• Aeronautical Material 66%
• Critical Energy Release Rate 66%
• Double Cantilever Beam 66%
• Lateral Impact 66%
• End-notched Flexure 66%
• China 33%
• High Performance 33%
• Aerospace Applications 33%
• Numerical Modeling 33%
• Finite Element 33%
• Prepreg 33%
• Impact Resistance 33%
• Aerospace Industry 33%
• Finite Element Model 33%
• Toughening Effect 33%
• Theoretical Modeling 33%
• Delamination 33%
• Ex-situ Toughening 33%
• Appropriate Treatment 33%
• Delamination Damage 33%
• Input Values 33%
• Load-carrying Structure 33%
• Mode Test 33%
• Contamination Assessment 33%
• Model Simulating 33%
• Mixed Mode 33%

Engineering

• Toughening 100%
• Resin Transfer Molding 100%
• Delamination 66%
• End-Notched Flexure 66%
• Double-Cantilever Beam 66%
• Critical Energy Release Rate 66%
• Finite Element Method 33%
• Aerospace Applications 33%
• Numerical Modeling 33%
• Impact Damage 33%
• Conducted Experiment 33%
• Delamination Damage 33%
• Input Value 33%
• Test Standard 33%
• Mixed Mode 33%

Material Science

• Resin Transfer Molding 100%
• Laminated Composite 100%
• Delamination 100%
• Finite Element Method 33%
• Prepreg 33%
• Theoretical Modeling 33%