The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel. Fracture and Structural Integrity, [S. l.], v. 13, n. 50, p. 126–140, 2019. DOI: 10.3221/IGF-ESIS.50.12. Disponível em: https://staging.fracturae.com/index.php/fis/article/view/2548. Acesso em: 16 oct. 2026.