A method for active flow control of a fluid flow that flows along a flow surface includes generating a first local velocity field in the fluid flow by introducing a first vortex structure into the fluid flow by means of a first flow control actuator coupled to a first actuation site of the flow surface, and introducing a second vortex structure into the first local velocity field by means of a second flow control actuator coupled to a second actuation site of the flow surface located downstream of the first actuation site, when a head vortex of the first vortex structure has propagated with the fluid flow downstream the second actuation site.
METHOD FOR ACTIVE FLOW CONTROL, FLOW BODY, AND AIRCRAFT
VERFAHREN ZUR AKTIVEN STRÖMUNGSSTEUERUNG, STRÖMUNGSKÖRPER SOWIE FLUGZEUG
PROCÉDÉ DE RÉGULATION ACTIVE DE FLUX, CORPS DE FLUX ET AÉRONEF
2023-07-05
Patent
Electronic Resource
English
Active flow control for aircraft wings
British Library Conference Proceedings | 2017
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