• Title/Summary/Keyword: 국한 슬롯 제트

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Experimental Study on the Unsteady Behavior of a Confined Impinging Slot Jet (국한 충돌 슬롯 제트의 비정상 거동에 대한 실험적 연구)

  • Kim, Kyung-Chun;Oh, Sung-Jin;Lee, In-Won
    • Journal of the Korean Society of Visualization
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    • v.3 no.2
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    • pp.57-62
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    • 2005
  • The flow characteristics in a confined slot jet impinging on a flat plate were investigated by using cinematic Particle Image Velocimetry technique. The jet Reynolds number was varied from 250 to 1000 for a fixed jet-to-plate spacing of H/W=5. We found that the vortical structures in the shear layer are developed with increase of Reynolds number and that the jet becomes unsteady by the interaction of vortex pairs between 500 and 750 of Reynolds number. Vortical structures and their temporal evolution are verified by using proper orthogonal decomposition.

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An experimental study of the unsteady flow in a confined slot jet by the change of nozzle shape (노즐형상 변화에 따른 국한 슬롯형 제트의 비정상 거동에 대한 실험적 연구)

  • Min, Young-Uk;Kim, Kyung-Chun
    • 한국가시화정보학회:학술대회논문집
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    • 2006.12a
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    • pp.55-58
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    • 2006
  • The flow characteristics in a confined slot jet impinging on a flat plate were investigated by using cinematic Particle Image Velocimetry technique. The three different kinds of confined slot were applied to the jet with a view to evaluating the shape effect and the jet Reynolds number was varied from 250 to 1000 for a fixed jet-to-plate spacing of H/W=5. It was found that the vortex structures in the shear layer are developed with increase of Reynolds number and that the jet becomes unsteady by the interaction of vortex pairs between 500 and 750 of Reynolds number. Finally, the slot shape was proved to be related with the generation timing of vortex pair and the temporal vortex structure.

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Experimental Study on the Unsteady Behavior of a Confined Impinging jet (국한 충돌 제트의 비정상 거동에 대한 실험적 연구)

  • Kim, Kyung-Chun;Oh, Sung-Jin;Lee, In-Won
    • 한국가시화정보학회:학술대회논문집
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    • 2005.12a
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    • pp.23-27
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    • 2005
  • The flow characteristics in a confined slot jet impinging on a flat plate were Investigated by using cinematic Particle Image Velocimetry technique. The jet Reynolds number was varied from 250 to 1000 for a fixed jet-to-plate spacing of H/W=5. We found that the vortical structures in the shear layer are developed with increase of Reynolds number and that the jet becomes unsteady by the interaction of vortex pairs between 500 and 750 of Reynolds number. Vortical structures and their temporal evolution are verified by using cinematic Particle Image Velocimetry technique.

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Investigation on the Unsteadiness of a Low Reynolds Number Confined Impinging Jet using POD Analysis (POD 기법을 이용한 저 레이놀즈 수 충돌 제트의 비정상 거동 연구)

  • An, Nam-Hyun;Lee, In-Won
    • Journal of the Korean Society of Visualization
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    • v.6 no.1
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    • pp.34-40
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    • 2008
  • The flow characteristics in a confined slot jet impinging on a flat plate were investigated in low Reynolds number regime (Re$\leq$1,000) by using time-resolved particle image velocimetry technique. The jet Reynolds number was varied from 404 to 1026, where it is presumed that the transient regime exists. It is found that the vortical structures in the shear layer are developed with increasing Reynolds number and that the jet remains steady at the Reynolds number of 404. Vortical structures and their temporal evolution are verified and the results were compared with previous numerical studies.

Thermal and flow characteristics of confined multiple slot jet impingement with exhaust ports (배기구를 가진 국한된 다중 슬롯 충돌제트의 열유동 특성)

  • Kang, Soo-Jin;Cho, Woo-Jin;Lee, Jong-Hyeok;Lee, Kwan-Soo
    • Proceedings of the SAREK Conference
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    • 2009.06a
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    • pp.835-840
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    • 2009
  • In this paper, confined multiple slot jet impingement with exhaust ports is investigated numerically. A flow cell, defined as volume sectioned by the impingement and confinement surfaces and the centerlines of adjacent nozzle and exhaust port, is chosen for computational domain. The effects of Reynolds number and geometrical parameters on the heat transfer performance and the flow characteristics are studied. For turbulence, the Abe-Kondoh-Nagano version of the low-Reynolds k-$\varepsilon$ model is employed. The results showed that the local Nusselt number distribution is shifted down and show poor heat transfer performance for small Reynolds number and small ratio of the lateral and axial length of flow cell. The rest of range, except the range of the shift phenomenon, can be classified into three groups by heat transfer characteristics.

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