Computational validation of the flow through a turbine stage and the effects of rim seal cavity leakage on secondary flows

Keyphrases

• Rotor 100%
• Secondary Flow 100%
• Validation Studies 100%
• Rim Seal 100%
• Turbine Stage 100%
• Computational Validation 100%
• Axial Flow Turbine 100%
• Sealed Cavity 100%
• Rotor-stator 100%
• Endwall 50%
• Vane 50%
• Nozzle Guide Vane 50%
• Flow Model 50%
• Reynolds number 50%
• Aerodynamics 50%
• Transitional Flow 50%
• Turbulence Model 50%
• Flow Condition 50%
• Computational Prediction 50%
• Interface Planes 50%
• Finite Volume 50%
• Aerodynamic Loss 50%
• Turbine Rotor 50%
• Generation Mechanism 50%
• Interface Model 50%
• Flow Solver 50%
• Geometry Modification 50%
• Kiel 50%
• Head Circumference 50%
• Structured Grid 50%
• Stage Model 50%
• Volume Flow 50%
• Five-hole Probe 50%
• Plane Measurement 50%
• Loss Generation 50%
• Total Pressure Coefficient 50%
• HP Turbine 50%

Engineering

• Rotors 100%
• Secondary Flow 100%
• Turbine 100%
• Axial Flow 40%
• Exit Plane 40%
• Flow Turbine 40%
• Guide Vane 20%
• Reynolds' Number 20%
• Flow Condition 20%
• Flow Model 20%
• Pressure Coefficient 20%
• Flow Solver 20%
• Structured Grid 20%
• Kiel Probe 20%