Numerical investigation of high pressure turbine blade tip-shaping effects on the aerothermal and dynamic performance

Engineering

• High-Pressure Turbine 100%
• Dynamic Performance 100%
• Blade Tip 100%
• Streamwise 100%
• Aerothermal Performance 100%
• Leakage Flow 33%
• Aerodynamics 16%
• Heat Transfer Coefficient 16%
• Pressure Distribution 16%
• Flow Distribution 16%
• Local Pressure 16%
• Turbine 16%
• Flow Pressure 16%
• Flow Loss 16%
• Leakage Loss 16%
• Static Pressure 16%
• Turbine Efficiency 16%