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Comparison of the Near-Field Flow Structures of a Triangular Jet with and without the Initial Confinement of a Chamber

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Fluid-Structure-Sound Interactions and Control

Part of the book series: Lecture Notes in Mechanical Engineering ((LNME))

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Abstract

This paper reports a large eddy simulation (LES) of the precession-like oscillation produced by partially confining a triangular-jet flow with a short cylindrical chamber. The present LES, which has been verified by previous experimental data, shows that there is a strong inward swirl around the jet near the inlet end of the chamber. At the center of the swirl, there is a cluster of three sink foci, where each focus is aligned midway between the corners of the triangular inlet orifice. In the time-averaged flow field, the vortices rising from the foci are helically twisted about the core of the jet. As the flow passes through the chamber, the foci merge to form a closed-loop “bifurcation line” which separates the inward swirl and the core flow. The core of the emerging jet is visible as a source node at the approximate centerline of the chamber. If the chamber is removed, a cluster of six counter-rotating foci is produced in the “free” jet. When this happens, the net swirl circulation is zero and there is no jet oscillation.

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Acknowledgments

This project is financially supported by the Fundamental Research Funds for the Central Universities (Grant No. 3132013029) and the Nature Science Foundation of China (Grant Nos. 11072005 and 10921202).

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Correspondence to J. Mi .

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© 2014 Springer-Verlag Berlin Heidelberg

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Xu, M., Lee, S.K., Mi, J., Li, P., Zhang, J. (2014). Comparison of the Near-Field Flow Structures of a Triangular Jet with and without the Initial Confinement of a Chamber. In: Zhou, Y., Liu, Y., Huang, L., Hodges, D. (eds) Fluid-Structure-Sound Interactions and Control. Lecture Notes in Mechanical Engineering. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-40371-2_21

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  • DOI: https://doi.org/10.1007/978-3-642-40371-2_21

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-40370-5

  • Online ISBN: 978-3-642-40371-2

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