ТЕРЕЩЕНКО, Ю. М.; ДИХАНОВСЬКИЙ, В. М.; ВОЛЯНСЬКА, Л. Г.; ЮРЧЕНКО, О. В. 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, [S. l.], v. 11, n. 4, p. 30–34, 2020. DOI: 10.18372/2306-1472.11.13108. Disponível em: https://jrnl.nau.edu.ua/index.php/visnik/article/view/13108. Acesso em: 28 aug. 2024.