Assessment of cure residual strains through the thickness of carbon-epoxy laminates using FBGs, Part I: Elementary specimen

Engineering

• Carbon-Epoxy Laminate 100%
• Residual Strain 100%
• Structural Design 50%
• Early Stage 50%
• Residual Stress 50%
• Rheology 50%
• Laminate Thickness 50%
• Composite Part 50%
• Gelation 50%
• Strain 50%
• Initial State 50%
• Autoclave 50%

Keyphrases

• Carbon-epoxy Laminate 100%
• Autoclave 100%
• FBG Sensor 50%
• Cure Monitoring 50%
• Information Highlighting 50%
• Assessment Procedures 50%
• Laminate Thickness 50%
• Composite Parts 50%

Material Science

• Fiber Bragg Grating 100%
• Thermomechanical Property 33%
• Gelation 33%
• Rheology 33%
• Residual Stress 33%