Mainstream aerodynamic effects due to wheelspace coolant injection in a high-pressure turbine stage: Part II - Aerodynamic measurements in the rotational frame

Keyphrases

• Aerodynamic Effect 100%
• Coolant Injection 100%
• Aerodynamic Measurement 100%
• High Pressure Turbine Stage 100%
• Rotational Frame 100%
• Rotor 75%
• Cooling Air 50%
• Exit Conditions 50%
• State Universities 25%
• Pennsylvania 25%
• Negligible Effects 25%
• Streamflow 25%
• Cooling Flows 25%
• Endwall 25%
• Nozzle Guide Vane 25%
• Secondary Flow 25%
• Wake Width 25%
• Flow Angle 25%
• Impingement Cooling 25%
• Current Measurement 25%
• Local Change 25%
• Secondary Effects 25%
• Rotating Frame 25%
• Stationary Frame 25%
• Flow Development 25%
• Axial Flow Turbine 25%
• Wall Boundary Layer 25%
• Performance Characters 25%
• 3D Velocity Field 25%
• Performance Condition 25%
• Three-dimensional Velocity Vector 25%
• Exit Route 25%

Engineering

• Rotors 100%
• Rotational 100%
• High-Pressure Turbine 100%
• Aerodynamic Effect 100%
• Aerodynamics 100%
• Cooling Air 66%
• Guide Vane 33%
• Velocity Field 33%
• Secondary Flow 33%
• Axial Flow 33%
• Boundary Layer 33%
• Pressure Coefficient 33%
• Current Measurement 33%
• Exit Flow 33%
• Negligible Effect 33%
• Velocity Vector 33%
• Flow Turbine 33%
• Main Stage 33%