Crack path in aeronautical titanium alloy under ultrasonic torsion loading. Fracture and Structural Integrity, [S. l.], v. 10, n. 35, p. pages 213–222, 2015. DOI: 10.3221/IGF-ESIS.35.25. Disponível em: https://staging.fracturae.com/index.php/fis/article/view/1646. Acesso em: 16 oct. 2026.