Frequency Response Analysis of Composite Aircraft Wing Using a Finite Element Euler-Bernoulli Beam Model. Romanian Journal of Acoustics and Vibration, [S. l.], v. 15, n. 1, p. 26–32, 2018. Disponível em: https://rjav.sra.ro/index.php/rjav/article/view/47.. Acesso em: 4 apr. 2026.