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End-Effects of a Finite Synthetic Jet on Flow Control

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Fluid-Structure-Sound Interactions and Control

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

Abstract

The end-effects of a finite synthetic jet used for controlling the flow around a two-dimensional circular cylinder are experimentally investigated in this study. The Reynolds number based on the cylinder diameter is Re = 800, and the corresponding natural vortex shedding frequency f 0 is 0.24 Hz (St = 0.21). The synthetic jet is actuated at excitation frequency f e /f 0  = 2.08, with the equivalent momentum coefficient C μ  = 0.139. Six xy planes of view from the mid-span to one of the slot ends with identical interval 5 mm are measured using two-dimensional time-resolved PIV system. It is found that the end-effects of the finite synthetic jet do not have a crucial influence on flow fields in the mid-span regions, which are independent of the slot length if it is longer than one cylinder diameter.

Supported by the National Natural Science Foundation of China (Grant no. 11202015).

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Correspondence to Li-Hao Feng .

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© 2014 Springer-Verlag Berlin Heidelberg

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Feng, LH., Ma, LQ., Wang, JJ. (2014). End-Effects of a Finite Synthetic Jet on Flow Control. 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_18

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  • DOI: https://doi.org/10.1007/978-3-642-40371-2_18

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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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