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Suction and Oscillatory Blowing Applied to the Rounded Front Edges of a Square Prism

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Book cover Instability and Control of Massively Separated Flows

Part of the book series: Fluid Mechanics and Its Applications ((FMIA,volume 107))

Abstract

An experimental study of a 2D square prism with rounded front edges is described. The purpose of the study is to reduce the aerodynamic drag by Active Flow Control (AFC) of boundary layer separation. Robust and efficient suction and pulsed blowing (SaOB) actuators are installed inside a circular cylinder that forms the upper-front curved edge. In addition and for simplicity, steady suction is applied at the lower-front round edge. The AFC results in significant form-drag reduction, narrower wake and correspondingly an increase in the base pressure.

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References

  1. Hucho W-H (2002) Aerodynamics of road vehicles. In: Hucho W-H, Ahmed SR (eds) Butterworths, London, Boston.

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  2. Choi H, Jeon W-P, Kim J (2008) Control of flow over a bluff body. Ann Rev Fluid Mech 40(1):113–139

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Acknowledgments

This project was partially supported by The RinnaBolle Student Travel Fund of Tel Aviv University and by the Meadow and Gordon family funds.

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Correspondence to G. Lubinsky .

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© 2015 Springer International Publishing Switzerland

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Lubinsky, G., Seifert, A. (2015). Suction and Oscillatory Blowing Applied to the Rounded Front Edges of a Square Prism. In: Theofilis, V., Soria, J. (eds) Instability and Control of Massively Separated Flows. Fluid Mechanics and Its Applications, vol 107. Springer, Cham. https://doi.org/10.1007/978-3-319-06260-0_23

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  • DOI: https://doi.org/10.1007/978-3-319-06260-0_23

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-06259-4

  • Online ISBN: 978-3-319-06260-0

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