Predictive methods for initiation of delamination and intra-laminar damage in carbon fibre reinforced polymer laminated subject to impact

Keyphrases

• ABAQUS 66%
• Carbon Fiber Reinforced Polymer 100%
• Cohesive Zone Model 33%
• Composite Damage 33%
• Contact Algorithm 33%
• Damage Criteria 33%
• Damage Evolution 66%
• Damage Onset 33%
• Delamination 100%
• Delamination Initiation 33%
• Elastic Regime 33%
• Hashin 33%
• Impact Response 33%
• Impact Scenarios 33%
• Interlaminar 33%
• Interlaminar Damage 100%
• Isotropic Pyrocarbon 33%
• Lamin 33%
• Linear Elastic 33%
• Low-energy Impact 33%
• LS-DYNA 66%
• Modeling Methodology 33%
• NiTe 66%
• Polymer Laminates 33%
• Predictive Methods 100%
• Puck 33%
• Quasi-isotropic 33%
• Reinforced Polymer 33%
• Tiebreak Contact 33%
• Virtual Crack Closure Technique 33%

Engineering

• Abaqus 50%
• Carbon Fibre Reinforced Polymer 100%
• Cohesive Zone Model 25%
• Composite Damage 25%
• Damage Criterion 25%
• Damage Evolution 50%
• Damage Onset 25%
• Delamination 100%
• Elastic Regime 25%
• Impact Response 25%
• Impact Scenario 25%
• Initial Stage 25%
• Interlaminar Failure 25%
• Intralaminar Damage 100%
• Modeling Work 25%
• Reinforced Polymer 25%
• Software Element 25%
• Virtual Crack-Closure Technique 25%

Material Science

• Carbon Fiber 100%
• Cohesive Zone Model 25%
• Crack Closure 25%
• Damage Evolution 50%
• Delamination 100%
• Reinforced Plastic 100%