In this numerical study, the flow obtained behind a trailing edge separating two streams of different velocities is studied by means of direct numerical simulation. The main originality of this work is that the splitter plate itself is included in the computational domain using an immersed boundary method. The influence of the trailing-edge shape is considered through the analysis of the destabilizing mechanisms and their resulting effect on the spatial development of the flow. The streamwise evolution of the different flows is found to be very different for each of the configurations considered, both in terms of mean quantities and flow dynamics. Present results suggest that the wake component, which dominates the flow close to the trailing edge, is still influential further downstream, as already observed in pure wake flows but only conjectured in mixing layer. A detailed analysis of the vortex dynamics is proposed using instantaneous visualizations, statistical/stability analysis considerations, and proper orthogonal decomposition in order to better understand how the transition regime from the wake to the mixing layer occurs and why it can influence the self-similarity, in a region where no wake influence can be locally detected.
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January 2010
Research Article|
January 11 2010
Direct numerical simulation of a mixing layer downstream a thick splitter plate Available to Purchase
Sylvain Laizet;
Sylvain Laizet
a)
1Department of Aeronautics,
Imperial College London
, London SW7 2AZ, United Kingdom
2Laboratoire d’Etudes Aérodynamiques UMR 6609,
Université de Poitiers
, CNRS Téléport 2, Bd. Marie et Pierre Curie, BP 179, 86962 Futuroscope Chasseneuil Cedex, France
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Sylvain Lardeau;
Sylvain Lardeau
1Department of Aeronautics,
Imperial College London
, London SW7 2AZ, United Kingdom
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Eric Lamballais
Eric Lamballais
2Laboratoire d’Etudes Aérodynamiques UMR 6609,
Université de Poitiers
, CNRS Téléport 2, Bd. Marie et Pierre Curie, BP 179, 86962 Futuroscope Chasseneuil Cedex, France
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Sylvain Laizet
1,2,a)
Sylvain Lardeau
1
Eric Lamballais
2
1Department of Aeronautics,
Imperial College London
, London SW7 2AZ, United Kingdom
2Laboratoire d’Etudes Aérodynamiques UMR 6609,
Université de Poitiers
, CNRS Téléport 2, Bd. Marie et Pierre Curie, BP 179, 86962 Futuroscope Chasseneuil Cedex, France
a)
Author to whom correspondence should be addressed. Electronic mail: [email protected].
Physics of Fluids 22, 015104 (2010)
Article history
Received:
July 13 2009
Accepted:
October 19 2009
Citation
Sylvain Laizet, Sylvain Lardeau, Eric Lamballais; Direct numerical simulation of a mixing layer downstream a thick splitter plate. Physics of Fluids 1 January 2010; 22 (1): 015104. https://doi.org/10.1063/1.3275845
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