Whirl flutter optimisation-based solution of twin turboprop aircraft using a full-span model. Applied and Computational Mechanics, [S. l.], v. 11, n. 1, 2017. DOI: 10.24132/acm.2017.324. Disponível em: https://acm.kme.zcu.cz//article/view/324. Acesso em: 24 may. 2025.