Coupled thermal-mechanical damage model of laminated carbon fiber/resin composite subjected to lightning strike

Keyphrases

• Carbon Fiber 100%
• Lightning Strike 100%
• Resin Composite 100%
• Coupled Thermo-mechanical 100%
• Mechanical Damage Model 100%
• Thermal Ablation 100%
• Thermo-mechanical Damage 100%
• Damage Depth 66%
• Thermal Expansion 66%
• Coupling Damage 66%
• Damage Variable 33%
• Continuum Damage Mechanics 33%
• Lightning 33%
• User-defined Subroutine 33%
• Strain Damage 33%
• Combined Impact 33%
• Abaqus Explicit 33%
• VUMAT 33%
• ABAQUS Software 33%
• In-plane Damage 33%
• Carbon Fiber Reinforced Polymer Laminates 33%
• Degradation Model 33%
• Stiffness Matrix 33%
• Ablation Model 33%
• Lightning Effects 33%
• Phenomenological Analysis Method 33%
• Mechanics Analysis 33%
• Stress-strain State 33%
• Thermal-mechanical Coupling Model 33%
• Thermal-mechanical Coupling 33%

Engineering

• Experimental Result 100%
• Lightning Strike 100%
• Damage Model 100%
• Mechanical Damage 100%
• Resin Composite 100%
• Mechanical Coupling 100%
• Continuum Damage Mechanics 50%
• Damage Variable 50%
• Carbon Fibre Reinforced Polymer 50%
• Degradation Model 50%
• State Variable 50%
• Stiffness Matrix 50%
• Strain State 50%