A synthetic jet evolving in a boundary layer with laminar separation

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Journal Article
Journal of Flow Visualization and Image Processing, 2010, 17 (3), pp. 229 - 242
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This paper reports our work on numerical modeling of a micro synthetic jet in a boundary layer with flow separation caused by an adverse pressure gradient. The numerical model was developed using a commercial code with three-dimensional Large Eddy Simulation (LES) being applied. The model was verified by experimental results. The numerical results enabled flow visualization which helped us understand the evolution of a synthetic jet between the synthetic jet actuator (SJA) and the onset of separation, which was not measured in the experiments. © 2010 by Begell House, Inc.
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