3D Investigation of Film Cooling Effectiveness for Nozzle Vane Platform of High Pressure Turbine with “Meridian Constriction” and Laidback Fan-Shaped Film-Cooling Holes
Russian aeronautics ; 62 , 3 ; 476-483
2019
Aufsatz (Zeitschrift)
Englisch
Lokalklassifikation TIB: | 770/7040/8000 | |
BKL: | 55.50 Luftfahrzeugtechnik |
Deposition Near Film Cooling Holes on a High Pressure Turbine Vane
Online Contents | 2012
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