KASIM, K. A.; SEGARD, P.; MAT, S.; MANSOR, S.; DAHALAN, M. N.; N. MOHD, N. A. R; M. NASIR, M. N. Effects of the Propeller Advance Ratio on Delta Wing UAV Leading Edge Vortex. International Journal of Automotive and Mechanical Engineering, [S. l.], v. 16, n. 3, p. 6958–6970, 2019. DOI: 10.15282/ijame.16.3.2019.10.0522. Disponível em: https://journal.ump.edu.my/ijame/article/view/1304. Acesso em: 24 nov. 2024.