Numerical study of aerodynamics of turbine rotor with leading edge modification near hub

Keyphrases

• Aerodynamics 100%
• Turbine Rotor 100%
• Leading Edge Modifications 100%
• Small Engine 66%
• Numerical Simulation 33%
• Helicopter 33%
• Working Fluid 33%
• Heat Transfer Rate 33%
• Heat Transfer Characteristics 33%
• Structural Weakness 33%
• High Pressure High Temperature 33%
• High-pressure Gas 33%
• SST Turbulence Model 33%
• Blade Tip 33%
• Behavior Transfer 33%
• Aerodynamic Efficiency 33%
• Endwall Loss 33%
• Aerodynamic Heating 33%
• Heat Load 33%

Engineering

• Numerical Study 100%
• Rotors 100%
• Leading Edge 100%
• Experimental Result 50%
• Heat Transfer Rate 50%
• Pressure Gas 50%
• Aerodynamic Efficiency 50%
• Blade Tip 50%
• Computer Simulation 50%
• Thermal Load 50%