Heat Transfer Coefficients of Film Cooling on a Rotating Turbine Blade Model: Part I. Effect of Blowing Ratio

Engineering

• Pressure Surface 100%
• Suction Surface 100%
• Spanwise Direction 100%
• Combined Action 50%
• Density Ratio 50%
• Mainstream Velocity 50%
• Local Heat Transfer Coefficient 50%
• Coriolis Effect 50%
• Rotating Speed 50%
• Averaged Density 50%
• Hole Diameter 50%
• Thermochromic Liquid Crystal 50%
• Blade Model 50%
• Film Coefficient of Heat Transfer 50%
• Significant Influence 50%
• Flat Blade 50%
• Circular Hole 50%
• Centrifugal Force 50%
• Streamwise 50%
• Surface Temperature Distribution 50%