LASTIVKA, Ivan. Raising gas-dynamic stability margin of axial and centrifugal compressor stages by means of vaned diffuser boundary layer control. Aviation, [S. l.], v. 15, n. 3, p. 76–81, 2011. DOI: 10.3846/16487788.2011.624262. Disponível em: https://journals.vilniustech.lt/index.php/Aviation/article/view/4974. Acesso em: 30 may. 2025.