• Title/Summary/Keyword: Reverse $K\acute{a}rm\acute{a}n$ vortex street

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Characteristics of Vortical Jet Structures of a Hydrofoil

  • Yang, Chang-Jo;Kim, You-Taek;Choi, Min-Seon
    • Journal of Advanced Marine Engineering and Technology
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    • v.31 no.7
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    • pp.842-851
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    • 2007
  • Oscillating foil propulsion, the engineering application of fish-like movement of a hydrofoil, has received in recent decades as a possible competitor for propellers. The oscillating foil produces an effective angle of attack, resulting in a normal force vector with thrust and lift components, and it can be expected to be a new highly effective propulsion system. We have explored propulsion hydrodynamics as a concept in wake flow pattern. The present study has been examined various conditions such as oscillating frequencies and amplitudes in NACA0010 profile. Flow visualizations showed that high thrust was associated with the generation of moderately strong vortices, which subsequently combine with trailing-edge vorticity leading to the formation of a reverse $K\acute{a}rm\acute{a}n$ vortex street. Vortex generation was inherent to jet production and playeda fundamental role in the wake dynamics. And it was shown that the strong thrust coefficient obtained as the Strouhal number was larger.

A Study on Vortical Flow Patterns of a Heaving Foil (히빙익 후류의 유통패턴에 관한 연구)

  • Yang, Chang-Jo;Kim, You-Taek;Choi, Min-Seon;Lee, Young-Ho
    • Proceedings of the Korean Society of Marine Engineers Conference
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    • 2005.11a
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    • pp.31-32
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    • 2005
  • It is known that an oscillating airfoil can produce a driving force through the generation of a reversed $K\acute{a}rm\acute{a}n$ vortex street, and this can be expected to be a new highly effective propulsion system. We have been examined various conditions such as frequency number, amplitude in NACA 0010. As Strouhal number is greater than 0.08, wake profile with velocity deficit can be transformed into the wake with velocity excess. We also presented the experimental results on the unsteady vortices structure of the heaving airfoil at various parameters.

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