Static and fatigue experimental tests on a full scale fuselage panel and FEM analyses. Fracture and Structural Integrity, [S. l.], v. 10, n. 35, p. pages 534–550, 2015. DOI: 10.3221/IGF-ESIS.35.59. Disponível em: https://staging.fracturae.com/index.php/fis/article/view/1685. Acesso em: 16 oct. 2026.