A vortex generator may include a depression in an aerodynamic surface, and a vortex generator leading edge located in the depression. The vortex generator leading edge may include a leading edge upper surface. The leading edge upper surface may be positioned at or below a tangent line defined at a location along the aerodynamic surface upstream of the depression relative to an oncoming local flow.
SUBMERGED VORTEX GENERATOR
2016-02-04
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Submerged Inlet Performance Enhancement Using a Unique Bump-Shaped Vortex Generator
Online Contents | 2016
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