Kasim KA, Segard P, Mat S, Mansor S, Dahalan MN, N. Mohd NAR, et al. Effects of the Propeller Advance Ratio on Delta Wing UAV Leading Edge Vortex. Int. J. Automot. Mech. Eng. [Internet]. 2019 Oct. 3 [cited 2024 Dec. 18];16(3):6958-70. Available from: https://journal.ump.edu.my/ijame/article/view/1304