The leading-edge sweep angle significantly influences the flight performance of swept
wings. The vortex flow structures affect the flow behavior of the moderate to highly swept …

The design of unmanned combat aerial vehicles (UCAVs) is primarily governed by the low-
observability requirement for military applications rather than aerodynamic performance …

View Video Presentation: https://doi. org/10.2514/6.2022-0428. vid At low speeds, the
leading-edge sweep angle influences the flight performance of swept wings. The flow …

In this paper, the low-speed aerodynamic performance of lambda wing with a chord length
of c= 210 mm and sweep angle of Λ= 51°, thickness 3 mm, and beveled leading edges on …

View Video Presentation: https://doi. org/10.2514/6.2022-3374. vid The design of unmanned
combat aerial vehicles (UCAVs) used for military applications is dictated by their low …

In this paper, the low-speed aerodynamic performance of unmanned combat air vehicle
(UCAV) X-45 delta wing was investigated by a numerical method using computational fluid …

Actualmente los túneles de agua constituyen un equipo de gran importancia para el
desarrollo e investigación en cuanto a la interacción sólido-fluido, pues permite mejorar el …

In this paper, a low-speed aerodynamic flow structure of the original F35 aircraft model was
investigated in a closed-circuit water tunnel experiment, and the investigation was also …