Aerospace, Volume 6, Issue 1 (January 2019) – 9 articles
A single slotted flap with airfoil camber adaptivity was first proved to be a valid replacement for a conventional double slotted flap owing to superior aerodynamic performance and lower deployment system complexity and noise footprint.
The feasibility of a morphing camber structure was then shown by means of rational analysis followed by experimental evidence; a novel flap architecture was proposed, as a smart integration of a robotic load-bearing structure and robust electromechanical actuators. View this paper.
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