The 3D Computational Investigation of Film Cooling Effectiveness for Turbine Nozzle Vanes with “Meridian Constriction” and Shaped Film-Cooling Holes
Russian aeronautics ; 61 , 1
2018
Article (Journal)
English
Local classification TIB: | 770/7040/8000 | |
BKL: | 55.50 Luftfahrzeugtechnik |