GEORGIEV, Gabriel. Blade element – momentum aerodynamic model of a helicopter rotor operating at low-Reynolds numbers in ground effect. Aviation, [S. l.], v. 29, n. 2, p. 71–81, 2025. DOI: 10.3846/aviation.2025.23587. Disponível em: https://journals.vilniustech.lt/index.php/Aviation/article/view/23587. Acesso em: 29 may. 2025.