Thermomechanical properties of carbon fabric reinforced epoxy laminates with h-BN and MoS₂fillers

Engineering & Materials Science

• Boron nitride 100%
• Fillers 67%
• Laminates 64%
• Carbon 53%
• Composite materials 41%
• Pyrolysis 19%
• Raman scattering 14%
• Solid lubricants 13%
• High temperature applications 12%
• Crosslinking 12%
• Dynamic mechanical analysis 12%
• Molybdenum 11%
• Glass transition 11%
• Thermogravimetric analysis 11%
• Superconducting transition temperature 11%
• Epoxy resins 10%
• Thermodynamic stability 10%
• Carbon fibers 9%
• Vacuum 8%
• Elastic moduli 8%
• Stiffness 7%
• Fibers 6%
• Temperature 4%

Physics & Astronomy

• boron nitrides 75%
• fillers 69%
• laminates 66%
• carbon 47%
• composite materials 43%
• thermal decomposition 22%
• solid lubricants 14%
• molybdenum disulfides 13%
• bags 12%
• stirring 11%
• crosslinking 11%
• matrices 11%
• epoxy resins 10%
• carbon fibers 10%
• glass transition temperature 9%
• stiffness 8%
• thermal stability 8%
• Raman spectra 7%
• vacuum 6%
• augmentation 6%
• fibers 5%
• performance 4%
• temperature 3%

Chemical Compounds

• Thermomechanical Property 86%
• Boron Nitride 80%
• Filler 60%
• Hexagonal Space Group 55%
• Composite Material 35%
• Carbon Atom 33%
• Pyrolysis 14%
• Molybdenum Disulfide 12%
• Storage Modulus 10%
• Epoxy Resin 9%
• Carbon Fiber 9%
• Crosslinking 8%
• Glass Transition Temperature 8%
• Raman Spectrum 8%
• Vacuum 8%
• Compound Mobility 7%
• Thermogravimetric Analysis 7%
• Thermal Stability 6%
• Application 3%