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Small-width wall-attached Coandǎ jets for flow control

Article dans une revue avec comité de lecture
Author
EL MOKKADEM, Oussama
531216 Laboratoire de Mécanique des Fluides de Lille - Kampé de Fériet [LMFL]
CHEN, Xintong
531216 Laboratoire de Mécanique des Fluides de Lille - Kampé de Fériet [LMFL]
PHAN, Charlene
531216 Laboratoire de Mécanique des Fluides de Lille - Kampé de Fériet [LMFL]
DELVA, Jérôme
531216 Laboratoire de Mécanique des Fluides de Lille - Kampé de Fériet [LMFL]
ccJOSEPH, Pierric
531216 Laboratoire de Mécanique des Fluides de Lille - Kampé de Fériet [LMFL]
ccDAZIN, Antoine
531216 Laboratoire de Mécanique des Fluides de Lille - Kampé de Fériet [LMFL]
ccROMANO, Francesco
531216 Laboratoire de Mécanique des Fluides de Lille - Kampé de Fériet [LMFL]

URI
http://hdl.handle.net/10985/24321
DOI
10.1017/flo.2023.9
Date
2023-06
Journal
Flow

Abstract

The flow dynamics of small-width wall-attached jets generated by a Coand-effect nozzle is investigated by unsteady Reynolds-averaged Navier–Stokes simulations. The data are validated by comparison with hot-wire velocity measurements performed on the same flow configurations. The jets exhibit a complex topology strongly influenced not only by the spanwise vorticity (as usually observed in wall jets) but also by a vorticity component normal to the wall and induced by the shear layer developing on the jet sides. This results in an original U-shaped jet whose characteristics are studied in detail for three different mass flow rates. The robustness of the flow topology on a larger range of injected mass flow rates is finally presented and discussed in terms of the injected momentum near the wall. The resulting flow profiles point out that our injector is expected to be a promising candidate for active flow control in gas-turbine compressors for aeronautical and energy applications.

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