Thermal-mechanical-chemical coupled model and three-dimensional damage evaluation based on computed tomography for high-energy laser-ablated CFRP

Engineering

• Internals 100%
• Pyrolysis 100%
• Coupled Model 100%
• Carbon Fibre Reinforced Polymer 100%
• Experimental Result 50%
• Delamination 50%
• Laser Power 50%
• Gas Flow 50%
• Thermal Stress 50%
• Tensile Stress σ 50%
• Synergistic Effect 50%
• Inhomogeneous Deformation 50%
• Carbon Fibre-Reinforced Polymer Composite 50%
• Process Time 50%
• Kinetic Model 50%
• Damage Morphology 50%
• Pyrolysis Gas 50%
• Mechanical Failure 50%

Material Science

• Delamination 50%