Experimental Investigation Into the Effect of a Ceramic Matrix Composite Surface on Film Cooling

Engineering

• Cooling Performance 100%
• Experimental Investigation 100%
• Boundary Layer 100%
• Turbulence Intensity 100%
• Cooling Hole 50%
• Gas Turbine 50%
• Smooth Surface 50%
• Particle Image Velocimetry 50%
• Operating Temperature 50%
• Density Ratio 50%
• Infrared Camera 50%
• Component Metal 50%
• Surface Increase 50%
• Tunnel 50%
• Turbine 50%

Keyphrases

• Film Cooling 100%
• Ceramic Matrix Composites 100%
• Composite Surface 100%
• Boundary Layer 33%
• Turbulence Intensity 33%
• Composite Component 33%
• Blowing Ratio 33%
• Free-stream Turbulence 33%
• Near-wall 33%
• Adiabatic Film Effectiveness 33%
• Film Cooling Hole 16%
• Coolant 16%
• Flow Field 16%
• Gas Turbine 16%
• Smooth Surface 16%
• Wind Tunnel 16%
• Effectiveness Evaluation 16%
• Metal Components 16%
• Operating Temperature 16%
• Efficiency Improvement 16%
• Turbulence 16%
• Infrared Camera 16%
• Wall Velocity 16%
• Surface Topology 16%
• High-speed Particle Image Velocimetry 16%
• Satin Weave 16%
• Weave Pattern 16%
• Strengthening Components 16%
• Temperature Capability 16%
• Wavy Pattern 16%
• Turbine Entry Temperature 16%