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
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