Abstract Some results of investigating the geometrical and jet impact on secondary flows and thermal state of cooled inter-profile end surfaces of gas turbine engine nozzles have been set forth under different secondary flows interaction degree in a blade channel.
Special features of aerodynamic and thermal improvement of turbine nozzles for advanced gas turbine engines
Russian Aeronautics (Iz VUZ) ; 59 , 1 ; 89-94
2016-01-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Turbine nozzles and diaphragms
Engineering Index Backfile | 1933
|Turbine pyrometry for advanced engines
AIAA | 1987
|