A propulsion system coupled to a vehicle. The system includes a convex surface, a diffusing structure coupled to the convex surface, and at least one conduit coupled to the convex surface. The conduit is configured to introduce to the convex surface a primary fluid Produced by the vehicle. The system further includes an intake structure coupled to the convex surface and configured to introduce to the diffusing structure a secondary fluid accessible to the vehicle. The diffusing structure comprises a terminal end configured to provide egress from the system for the introduced primary fluid and secondary fluid.
EJECTOR AND AIRFOIL CONFIGURATIONS
EJEKTOR UND TRAGFLÄCHENKONFIGURATIONEN
CONFIGURATIONS D'ÉJECTEUR ET DE PROFIL AÉRODYNAMIQUE
2020-10-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |