BA ZUHAIR, Mohammed. Balancing an aircraft with symmetrically deflected split elevator and rudder during short landing run. Aviation, [S. l.], v. 23, n. 1, p. 23–30, 2019. DOI: 10.3846/aviation.2019.10301. Disponível em: https://journals.vilniustech.lt/index.php/Aviation/article/view/10301. Acesso em: 25 may. 2025.