• Title/Summary/Keyword: 양방향 유체-고체 연성해석

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Numerical Study of Surface Heat Transfer Effects of Multiple Fan-Shaped Small-Scale Fins (다중 미세 날개구조의 표면 열전달에 미치는 영향분석)

  • Park, Ki-Hong;Park, Sang Hu;Lee, Ju-Chul;Min, June-Kee;Ha, Man-Yeong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.37 no.5
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    • pp.523-530
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    • 2013
  • In this work, we study a heat transfer enhancement technology using fan-shaped small-scale fins. Fins having a thickness of 10 ${\mu}m$ move up-down by a pulsating flow. Owing to these motions, the heat transfer on a surface increases dramatically. The two-way FSI (fluid-structure interaction) method was applied for the analysis, and the analysis model was evaluated using a single fin model by comparing the experimental results. In summary, a maximum 40% increase in heat transfer capacity using a single and multiple small-scale fins was obtained in comparison with the results obtained without using fins. From this work, we believe that the proposed method can be a promising method for heat transfer enhancement in real applications.

A Numerical Study on the Effect of a Microfin with a Flexible Up-down Movement on Heat Transfer using a Fluid-structure Interaction (FSI) Method (양방향 유체-고체 연성해석을 통한 표면 위 미세날개의 진동이 열전달에 미치는 영향 분석)

  • Park, Ki-Hong;Min, June-Kee;Kim, Jin-Kyu;Kang, Seok-Hoon;Kim, Seong-Jin;Park, Sang-Hu
    • Journal of the Korean Society for Precision Engineering
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    • v.28 no.8
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    • pp.975-983
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    • 2011
  • A microfin on a heated surface and its effects of the heat transfer has been investigated. The thickness of the fin is about 8 micrometer to allow the flexible up-down motion of the fin. Two-way complete FSI (Fluid-Structure Interaction) method has been applied for the analysis. Firstly, the deformation of a microfin due to the pulsating flow is evaluated using structure analysis. The flow and temperature patterns are predicted by CFD (Computational Fluid Dynamics) method. At each time step, using the pressure force and temperature distribution from CFD, the deformation of the wing is evaluated by FEM. Also in order to estimate the resonance probability, the natural frequency of the wing structure is calculated by modal analysis. The proposed numerical procedure was validated through experiment using a single fin. Through this work, we show that the increase of 40% in heat transfer capacity using the microfin has been compared with that of flat plate case.