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Small-width wall-attached Coandǎ jets for flow control

Article dans une revue avec comité de lecture
Auteur
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

Résumé

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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  • Laboratoire de Mécanique des Fluides de Lille (LMFL)

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Visualiser des documents liés par titre, auteur, créateur et sujet.

  • Experimental Analysis of an Axial Compressor Operating under Flow Distorsion 
    Communication avec acte
    BARETTER, Alberto; ROUSSETTE, Olivier; ROMANO, Francesco; ccDAZIN, Antoine; ccJOSEPH, Pierric (ASME, 2022-06)
    In aircraft engines, compressor stages can encounter situations in which the flow is distorted at rotor inlet, for example during particular flight maneuvers, or due to the shape of the inlet of the airframe. The main ...
  • Experimental and Numerical Analysis of a Compressor Stage under Flow Distortion 
    Article dans une revue avec comité de lecture
    ccBARETTER, Alberto; GODARD, Benjamin; ccJOSEPH, Pierric; ccROUSSETTE, Olivier; ccROMANO, Francesco; BARRIER, Raphael; ccDAZIN, Antoine (MDPI AG, 2021-11)
    On many occasions, fan or compressor stages have to face azimuthal flow distortion at inlet, which affects their performance and stability. These flow distortions can be caused by external events or by some particular ...
  • Experimental and Numerical Analysis of a Compressor Stage under Flow Distortion 
    Article dans une revue avec comité de lecture
    BARETTER, Alberto; GODARD, Benjamin; ROUSSETTE, Olivier; ROMANÒ, Francesco; BARRIER, Raphael; ccDAZIN, Antoine; ccJOSEPH, Pierric (MDPI AG, 2021)
    On many occasions, fan or compressor stages have to face azimuthal flow distortion at inlet, which affects their performance and stability. These flow distortions can be caused by external events or by some particular ...
  • The ACONIT project: an innovative design approach of active flow control for surge prevention in gas turbines 
    Communication avec acte
    ccDAZIN, Antoine; ccJOSEPH, Pierric; ccROMANÒ, Francesco; GALLAS, Q; MARTY, J; AIGOUY, G; STÔΒEL, M; NIEHUIS, R (IOP Publishing, 2021-01-22)
    The objective of the ACONIT project is to design, manufacture and test actuators for flow control for an implantation in an aircraft engine. The actuators will fulfil aeronautics requirement in order to increase the ...
  • Pulsed air injection system characterization for stall margin improvement in an axial compressor 
    Communication avec acte
    MARGALIDA, Gabriel; ROUSSETTE, Olivier; DELVA, Jérôme; ccDAZIN, Antoine; ccJOSEPH, Pierric (EUCASS association, 2022-06-27)
    This paper presents the design and the characterization of a pulsed air injection system on a single stage axial compressor. The goal of this system is to delay the rotating stall onset and to extend the compressor operating ...

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