An aircraft includes a fuselage and at least one primary wing having an upper surface, at least one recess in the upper surface and at least one conduit in fluid communication with the at least one recess. At least one ejector is disposed within the at least one recess and is configured to receive compressed air via the at least one conduit.
FLUIDIC PROPULSIVE SYSTEM
2024-05-09
Patent
Elektronische Ressource
Englisch