Aerodynamic effects of trailing edge geometry, hole size, angle, spacing, and shape have been studied in two- and three-dimensional cascades and in a warm turbine test series. Heat transfer studies have been carried out in various two- and three-dimensional test facilities in order to provide corresponding heat transfer data. Results are shown in terms of cooling effectiveness and aerodynamic efficiency for various coolant fractions, coolant-primary temperature ratios, and cooling configurations.
Summary of NASA Aerodynamic and Heat Transfer Studies in Turbine Vanes and Blades
Sae Technical Papers
Aerospace Engineering and Manufacturing Meeting ; 1976
01.02.1976
Aufsatz (Konferenz)
Englisch
Summary of NASA Aerodynamic and Heat Transfer Studies in Turbine Vanes and Blades
Kraftfahrwesen | 1976
|Predictions of External Heat Transfer for Turbine Vanes and Blades With Secondary Flowfields
Online Contents | 2003
|Air Cooling of Turbine Blades and Vanes
Emerald Group Publishing | 1967
|Cooling Modern Aero Engine Turbine Blades and Vanes
SAE Technical Papers | 1966
|Computer-Aided Design Of Turbine Blades And Vanes
NTRS | 1988
|