Computational and experimental studies of Midpassage gap leakage and misalignment for a non-Axisymmetric contoured turbine blade Endwall

Keyphrases

• Leakage Flow 100%
• Turbine Blade 100%
• Non-axisymmetric 100%
• Misalignment 100%
• Blade Endwall 100%
• Endwall Heat Transfer 75%
• Local Heat Transfer 75%
• Endwall 50%
• Heat Transfer Coefficient 50%
• Steady RANS 50%
• Computational Study 25%
• Surface Temperature 25%
• Endwall Flow 25%
• Thermal Expansion 25%
• Turbine Vane 25%
• Heat Transfer 25%
• Secondary Flow 25%
• Computational Model 25%
• Turbine Disk 25%
• Airfoil Section 25%
• High-pressure Coolant 25%
• Heater 25%
• Centrifugal Force 25%
• Turbulence 25%
• Accurately Model 25%
• Spatially Resolved 25%
• Flow Transferring 25%
• Flow Interaction 25%
• Flux Surface 25%
• Contoured Endwall 25%
• Infrared Thermography 25%
• Recirculation Region 25%
• Backward-facing Step 25%
• Expansion Force 25%
• Blade Passage 25%
• RANS CFD 25%
• Uniform Heat Flux 25%
• Non-axisymmetric Endwall 25%
• Misprediction 25%

Engineering

• Axisymmetric 100%
• Leakage Flow 100%
• Blade Turbine 100%
• Computational Fluid Dynamics 75%
• Local Heat Transfer 75%
• Heat Transfer Coefficient 50%
• Facing Step 50%
• Secondary Flow 25%
• Experimental Observation 25%
• Airfoil Section 25%
• Disc Turbine 25%
• Centrifugal Force 25%
• Infrared Thermography 25%
• Blade Passage 25%
• Uniform Heat Flux 25%
• Turbine 25%