Development of a high pressure-differential turbine blade cooling system
Russian aeronautics ; 53 , 4 ; 475-478
2010
Aufsatz (Zeitschrift)
Englisch
Lokalklassifikation TIB: | 770/7040/8000 | |
BKL: | 55.50 Luftfahrzeugtechnik |
Development of a high pressure-differential turbine blade cooling system
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