News and Updates

Improving Intermediate Pressure Turbine Performance by Using a Nonorthogonal Stator

Influence of Film Cooling Hole Angles and Geometries on Aerodynamic Loss and Net Heat Flux Reduction

Aerodynamic Design of High End Wall Angle Turbine Stages—Part II: Experimental Verification

Aerodynamic Design of High End Wall Angle Turbine Stages—Part I: Methodology Development