Flow migration and mixing in a high pressure turbine rotor passage with axisymmetrically contoured endwall and leakage flow

Keyphrases

• Flow Migration 100%
• Flow Mixing 100%
• High Pressure Turbine 100%
• Contoured Endwall 100%
• Endwall 100%
• Turbine Rotor 100%
• Leakage Flow 100%
• Endwall Flow 100%
• Approach Flow 40%
• Streamwise 40%
• Coolant 40%
• Secondary Flow 40%
• Cooling Effect 40%
• High-pressure Gas 40%
• Endwall Contour 40%
• Temperature Profile 20%
• Management Techniques 20%
• Bleeding 20%
• Gas Turbine 20%
• Thermal Loading 20%
• Adverse Effects 20%
• Flow Field 20%
• Combustor 20%
• Pressure Gradient 20%
• Linear Cascade 20%
• Mixing Effect 20%
• Steep Slope 20%
• Mass Flow Rate 20%
• Thermal Field 20%
• Stator 20%
• Shortest Distance 20%
• Film Cooling 20%
• Flow Discharge 20%
• High Thermals 20%
• Coolant Flow 20%
• Adiabatic Effectiveness 20%
• Gas Turbine Design 20%
• Dolphin 20%
• Exit Temperature 20%
• Mainstream Flow 20%
• Leakage Flow Rate 20%
• Combustor Liner 20%
• Low-NOx 20%
• Transverse Pressure 20%
• Cooling Management 20%
• Gas Turbine Rotor 20%
• Rotor Disc 20%
• Disk Cavity 20%
• Large Distances 20%
• Flow Environment 20%
• Sharks 20%

Engineering

• Rotors 100%
• Leakage Flow 100%
• High-Pressure Turbine 100%
• Gas Turbine 60%
• Streamwise 40%
• Flow Rate 40%
• Combustor 40%
• Cooling Effect 40%
• Secondary Flow 40%
• Flow Velocity 40%
• Limitations 20%
• Axisymmetric 20%
• Mass Flowrate 20%
• Exit Temperature 20%
• Coolant Flow 20%
• Field Data 20%
• Thermal Field 20%
• Mainstream Flow 20%
• Rotor Disc 20%
• Temperature Profile 20%
• Flow Distribution 20%
• Pressure Gradient 20%