[1]
“Frequency Response Analysis of Composite Aircraft Wing Using a Finite Element Euler-Bernoulli Beam Model”, RJAV, vol. 15, no. 1, pp. 26–32, Aug. 2018, Accessed: Aug. 29, 2026. [Online]. Available: https://rjav.sra.ro/index.php/rjav/article/view/47