Aerodynamic tip desensitization of an axial turbine rotor using tip platform extensions

Keyphrases

• Aerodynamic Field 33%
• Aerodynamic Loss 33%
• Aerodynamics 100%
• Axial Flow Turbine 66%
• Axial Turbine 100%
• Blade Tip 33%
• Desensitization 100%
• Efficiency Gain 33%
• Leakage Flow 33%
• Pennsylvania 33%
• Pressure Differential 33%
• Pressure Measurement 33%
• Pressure Side 100%
• Rotor 33%
• Rotor Blade 33%
• Rotor Tip 33%
• Single-stage 33%
• State Universities 33%
• Streamwise 33%
• Suction Side 100%
• Tangential Directions 33%
• Time Response 33%
• Time-accurate 33%
• Tip Extension 33%
• Total Pressure 66%
• Total Pressure Probe 33%
• Turbine Rotor 100%
• Viscous Loss 33%
• Vortex Structure 33%
• Vortical Structures 33%
• Winglet 33%

Engineering

• Axial Flow 66%
• Blade Tip 33%
• Differential Pressure 33%
• Exit Plane 33%
• Flow Turbine 66%
• Leakage Flow 33%
• Pressure Probe 33%
• Pressure Side 100%
• Response Time 33%
• Rotor Blade 33%
• Rotors 100%
• Single Stage Turbine 33%
• Streamwise 33%
• Suction Side 100%
• Turbine 100%
• Vortex 66%
• Winglets 33%