As the result of ANSYS CFX calculation, a conclusion was drawn about the greater cooling effectiveness of vane platform with laidback fan-shaped perforation holes as compared with cooling effectiveness of vane platform with cylindrical holes.
3D Investigation of Film Cooling Effectiveness for Nozzle Vane Platform of High Pressure Turbine with “Meridian Constriction” and Laidback Fan-Shaped Film-Cooling Holes
Russ. Aeronaut.
Russian Aeronautics ; 62 , 3 ; 476-483
2019-07-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Deposition Near Film Cooling Holes on a High Pressure Turbine Vane
Online Contents | 2012
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