An airfoil tip vortex mitigation arrangement comprising one or more flow directors configured and positioned to re-direct freestream air over a low pressure surface of an airfoil in such a way as to displace and weaken a main tip vortex generated at a tip of the airfoil.
Minimally intrusive wingtip vortex wake mitigation using microvane arrays
20.02.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Airfoil comprising a minimally intrusive wingtip vortex mitigation device
Europäisches Patentamt | 2023
|Aircraft wake flow adjusting device for accelerating wingtip vortex dissipation
Europäisches Patentamt | 2021
|NTIS | 1984
|