A vortex generation apparatus including a vortex generator that deploys in response to deployment of a wing leading edge lift augmentation device. The vortex generator deploys into a position to generate vortices over a main wing body upper surface region trailing the vortex generator.
Vortex generation
2016-11-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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