SUBMERGED VORTEX GENERATOR

A vortex generator (200) includes a depression (202) in an aerodynamic surface (126), and a vortex generator leading edge (300) located in the depression (202). The vortex generator leading edge includes a leading edge upper surface (312). The leading edge upper surface (312) is positioned at or bel...

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Bibliographische Detailangaben
Hauptverfasser:	Dehaan, Mark, Vassberg, John Charles, Sclafani, Anthony J, Harrison, Neal A
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOWOF GASES OR LIQUIDS FLUID-PRESSURE ACTUATORS HEATING HELICOPTERS HYDRAULICS OR PNEUMATICS IN GENERAL LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A vortex generator (200) includes a depression (202) in an aerodynamic surface (126), and a vortex generator leading edge (300) located in the depression (202). The vortex generator leading edge includes a leading edge upper surface (312). The leading edge upper surface (312) is positioned at or below a tangent line defined at a location along the aerodynamic surface (126) upstream of the depression (202) relative to an oncoming local flow.