Comparisons of pins/dimples/protrusions cooling concepts for a turbine blade tip-wall at high reynolds numbers

Engineering

• High Reynolds Number 100%
• Turbine 100%
• Blade Tip 100%
• Reynolds' Number 12%
• Pressure Drop 12%
• Hot Gas 12%
• Blade Turbine 12%
• Leakage Flow 12%
• Thermal Load 12%
• Convective 12%
• Heat Transfer Enhancement 12%
• Active Area 12%
• Mechanical Stress 12%
• Safe Operation 12%
• Gas Leakage 12%