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Effect of Forward Splitter Plate Leading Edge Shape on the Cylinder Flow

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Abstract

Experiments have been conducted on a cylinder with a forward splitter plate at Reynolds number of 5.33 × 104. Ten different splitter plate configurations are considered wherein the leading edge of the splitter plate is modified. The flow development on the splitter plate and on the cylinder has been examined using PIV. Static pressure on the cylinder surface and hot wire measurements in the cylinder wake have been carried out. A maximum of 57% increase in base pressure is observed with the use of splitter plate leading edge modification as compared to the simple cylinder case.

Keywords

  • Cylinder flow
  • Shedding frequency
  • Splitter plate

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  • DOI: 10.1007/978-981-15-5183-3_37
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References

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  4. Chutkey K, Suriyanarayanan P, Venkatakrishnan L (2018) Near wake field of circular cylinder with a forward splitter plate. J Wind Eng Ind Aerodyn 173:28–38

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Correspondence to Kiran Chutkey .

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Chutkey, K., Suriyanarayanan, P., Venkatakrishnan, L. (2021). Effect of Forward Splitter Plate Leading Edge Shape on the Cylinder Flow. In: Venkatakrishnan, L., Majumdar, S., Subramanian, G., Bhat, G.S., Dasgupta, R., Arakeri, J. (eds) Proceedings of 16th Asian Congress of Fluid Mechanics. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-15-5183-3_37

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  • DOI: https://doi.org/10.1007/978-981-15-5183-3_37

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  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-15-5182-6

  • Online ISBN: 978-981-15-5183-3

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