Development of the design scheme of cooling for a nozzle vane of high pressure turbine of gas turbine engine
Russian aeronautics ; 59 , 1
2016
Aufsatz (Zeitschrift)
Englisch
BKL: | 55.50 Luftfahrzeugtechnik | |
Lokalklassifikation TIB: | 770/7040/8000 |
AIAA-2005-1113 BALLISTIC COOLING OF TURBINE NOZZLE GUIDE VANE PLATFORMS
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