Multiaxial fatigue of in-service aluminium longerons for helicopter rotor-blades. Frattura ed Integrità Strutturale, [S. l.], v. 10, n. 38, p. Pages 399–404, 2018. DOI: 10.3221/IGF-ESIS.38.49. Disponível em: https://ww3.fracturae.com/index.php/fis/article/view/1813. Acesso em: 12 nov. 2024.