1.
Терещенко ЮМ, Дихановський ВМ, Волянська ЛГ, Юрченко ОВ. Quasi-spatial method for finding optimal design angles for the entrance and exit of blade crowns of the axial compressor of a gas turbine engine. Proceedings of National Aviation University [Internet]. 2020 Jan. 17 [cited 2024 Dec. 20];11(4):30-4. Available from: https://jrnl.nau.edu.ua/index.php/visnik/article/view/13108