Experimental investigation on heat transfer characteristics in a ribbed leading edge channel of turbine blade

Engineering

• Leading Edge 100%
• Blade Turbine 100%
• Experimental Investigation 100%
• Reynolds' Number 50%
• Heat Transfer Area 50%
• Transients 25%
• Liquid Crystal 25%
• Cooling Channel 25%
• Flow Velocity 25%
• Flow Rate 25%
• Flow Direction 25%
• Coolant Flow 25%
• Reduced Velocity 25%
• Stagnation Point 25%