Computational predictions of heat transfer and film-cooling for a turbine blade with nonaxisymmetric endwall contouring

Keyphrases

• Endwall 100%
• Endwall Heat Transfer 100%
• Heat Transfer 100%
• Film Cooling 100%
• Turbine Blade 100%
• Computational Prediction 100%
• Non-axisymmetric Endwall Contouring 100%
• Turbulence Model 66%
• Non-axisymmetric 66%
• Three-dimensional (3D) 33%
• Kinetic Energy 33%
• Cooling Flows 33%
• Gas Turbine Engine 33%
• Effective Method 33%
• Flow Field 33%
• Computational Fluid Dynamics Simulation 33%
• Heat Transfer Enhancement 33%
• Turbine Endwall 33%
• Endwall Film Cooling 33%
• Aerodynamic Loss 33%
• Vortical Structures 33%

Engineering

• Blade Turbine 100%
• Turbine 100%
• Gas Turbine Engine 50%
• Experimental Measurement 50%
• Computational Fluid Dynamics 50%
• Aerodynamics 50%