A numerical study of anti-vortex film-cooling holes designs in a 1-1/2 turbine stage using LES
Al-Zurfi, Nabeel, Turan, Ali, Nasser, Adel, Alhusseny, AhmedLanguage:
english
Journal:
Propulsion and Power Research
DOI:
10.1016/j.jppr.2019.10.001
Date:
December, 2019
File:
PDF, 9.74 MB
english, 2019