Abstract A convective-film system of high pressure-differential turbine blade cooling is presented. The results of calculating the thermal-hydraulic blade state using the KW3D software are given.
Development of a high pressure-differential turbine blade cooling system
Russian Aeronautics (Iz VUZ) ; 53 , 4 ; 475-478
2010-12-01
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Development of a high pressure-differential turbine blade cooling system
Online Contents | 2010
|Turbine Blade Cooling System Optimization
Online Contents | 2013
|Turbine Blade Internal Cooling System
British Library Conference Proceedings | 1999
|Recent Development in Turbine Blade Film Cooling
Online Contents | 2001
|Turbine Blade Cooling: The Blade Temperature Distribution
Online Contents | 2006
|