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3D Investigation of Film Cooling Effectiveness for Nozzle Vane Platform of High Pressure Turbine with “Meridian Constriction” and Laidback Fan-Shaped Film-Cooling Holes
Gorelov, Yu. G.Volume:
62
Language:
english
Journal:
Russian Aeronautics
DOI:
10.3103/S1068799819030164
Date:
July, 2019
File:
PDF, 428 KB
english, 2019