ABDALSALAM AWADALLA ALI HAJ AHMED. Estimate Anti-symmetrical Divergence Modes of an Aircraft Wing Utilizing Aero-structure Analysis via Aerodynamic Lifting Line Theory. Engineering And Technology Journal, [S. l.], v. 9, n. 10, p. 5321–5328, 2024. DOI: 10.47191/etj/v9i10.09. Disponível em: https://everant.org/index.php/etj/article/view/1560. Acesso em: 21 nov. 2024.