학술논문

Influence of spanwise and streamwise film hole spacing on adiabatic film effectiveness for effusion-cooled gas turbine blades
Document Type
Article
Source
In: International Journal of Turbomachinery, Propulsion and Power. (International Journal of Turbomachinery, Propulsion and Power, September 2021, 6(3))
Subject
Language
English
ISSN
2504186X