4   Artículos

Heat Transfer in a Two-Pass Rectangular Rotating Channel With 45-deg Angled Rib Turbulators

Revista: JOURNAL OF TURBOMACHINERY    Formato: Impreso

Tabla de contenido: Vol: 124 Num: 2 Par: 0 Año: 2002

Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 1¿Effect of Cut-Back Length, Spanwise Rib Spacing, Free-Stream Reynolds Number, and Chordwise Rib Length on Discharge Coefficients

Revista: JOURNAL OF TURBOMACHINERY    Formato: Impreso

Tabla de contenido: Vol: 123 Num: 2 Par: 0 Año: 2001

Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I¿Aerodynamic Measurements in the Stationary Frame

Revista: JOURNAL OF TURBOMACHINERY    Formato: Impreso

Tabla de contenido: Vol: 123 Num: 4 Par: 0 Año: 2001

Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part II¿Aerodynamic Measurements in the Rotational Frame

Revista: JOURNAL OF TURBOMACHINERY    Formato: Impreso

Tabla de contenido: Vol: 123 Num: 4 Par: 0 Año: 2001