Abstract: Aerodynamic and heat-transfer measurements were acquired using a modern stage and 1∕2 high-pressure turbine operating at design corrected conditions and pressure ratio. These measurements were ...

Abstract: Aerodynamic measurements were acquired on a modern single-stage, transonic, high-pressure turbine with the adjacent low-pressure turbine vane row (a typical civilian one and one-half stage turbine ...

Abstract: This paper presents both measurements and predictions of the hot-gas-side heat transfer to a modern, 112 stage high-pressure, transonic turbine. Comparisons of the predicted and measured heat ...