Aiming at the dynamic stall problem that restricts the improvement of aircraft maneuverability, a new dynamic stall control method based on leading-edge DSJ is proposed in this paper. The results show ...
Considering the characteristics of large slenderness ratio structure, it is reasonable to simplify the dynamics of a HALE aircraft as the plunge, pitch, and flap motions of a planar airfoil. The ...
[Harms et al.(2025)Harms, Nikoueeyan, and Naughton] Tanner D. Harms, Pourya Nikoueeyan, and Jonathan W. Naughton. Experimental evaluation of the cycle-to-cycle variations observed in dynamic stall.
Some results have been hidden because they may be inaccessible to you
Show inaccessible results