Design issues in using integral textile ceramic composites in turbine engine combustors

Physics & Astronomy

• turbine engines 100%
• textiles 72%
• combustion chambers 70%
• ceramics 42%
• low conductivity 40%
• oxides 39%
• composite materials 38%
• composite structures 36%
• heat transfer coefficients 34%
• heat flux 28%
• thermal expansion 27%
• costs 24%
• cooling 21%
• fabrication 19%

Engineering & Materials Science

• Combustors 64%
• Textiles 62%
• Oxides 54%
• Turbines 49%
• Ceramic materials 37%
• Composite materials 36%
• Composite structures 32%
• Thermal expansion 32%
• Heat transfer coefficients 29%
• Heat flux 28%
• Skin 27%
• Fabrication 23%
• Cooling 22%
• Hot Temperature 15%
• Costs 12%

Earth & Environmental Sciences

• turbine 59%
• textile 59%
• engine 58%
• oxide 47%
• thermal expansion 37%
• heat flux 29%
• tolerance 28%
• skin 28%
• heat transfer 27%
• conductivity 25%
• material 25%
• cooling 22%
• matrix 19%
• parameter 11%