The crack path in fuselage panel under mixed mode biaxial loading. Fracture and Structural Integrity, [S. l.], v. 13, n. 48, p. 87–96, 2019. DOI: 10.3221/IGF-ESIS.48.11. Disponível em: https://staging.fracturae.com/index.php/fis/article/view/2326. Acesso em: 16 oct. 2026.