• Title/Summary/Keyword: 강 표면류 가시화

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Outlines of Large Scale Particle Image Velocimetry (LSPIV) and its Applications (LSPIV(Large Scale Particle Image Velocimetry)기법의 개요 및 응용분야)

  • Yoon Byungman;Noh Youngshin
    • Journal of the Korean Society of Visualization
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    • v.1 no.2
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    • pp.13-16
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    • 2003
  • LSPIV(Large Scale Particle Image Velocimetry) is widely used in the field of civil and environmental engineering. General aspects of LSPIV are introduced and several applications are introduced in this paper. The difference of LSPIV from the conventional PIV techniques is not to use models for experiments but to use the flow fields in nature. For LSPIV a converting process for the captured images is necessary.

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Visualization of Internal Flows in the Wall-injected Test Model of a SRM (고체로켓모터 표면분사 시험모델의 유동 가시화)

  • Kim, Do-Hun;Lee, In-Chul;Koo, Ja-Ye;Cho, Yong-Ho;Kang, Moon-Jung;Kim, Yoon-Gon
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.3
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    • pp.31-39
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    • 2011
  • The flowfield in a solid rocket motor was simulated at the wall-injection test model, which has a fin-slot grain and submerged nozzle, and visualized by a smoke-wire. The high speed CCD camera captured the visualized images around the nozzle inlet through the grain center port. The vortical tube structure and circumferential flow patterns at the nozzle throat were visualized. The radial momentum transfer caused by the shear-interactions of slot-outlet flow, fin-base flow and grain port flow from upstream worked as the source of these phenomena.

Visualization of Roll Torque Generating Flows in a SRM Submerged-Nozzle by Cold Air-flow Test (내삽노즐 고체로켓모터의 공기 유동모사시험을 통한 롤토크 발생유동 가시화)

  • Kim, Do-Hun;Lee, In-Chul;Lee, Yeol;Koo, Ja-Ye;Kang, Moon-Jung;Kim, Yoon-Gon
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.2
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    • pp.29-35
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    • 2011
  • The behaviors of combustion-induced internal flows of SRM equipped with fin-slot grain and submerged nozzle are very complex and diverse. Cold air-flow tests for 2D and 3D scale models of SRM have been done in order to specify the visualization method to analyze particular internal flow patterns such as roll-torque inducing flow. Swirl flow induced by asymmetric vortical tubes also has been visualized through employing various light source and recording directions.

Visualization for Internal Flow of Submerged-Nozzle SRM by Cold Air-flow Test (내삽노즐 고체로켓의 공기 유동모사시험을 통한 내부유동 가시화)

  • Kim, Do-Hun;Cho, Yong-Ho;Lee, Yeol;Koo, Ja-Ye;Kim, Yoon-Gon;Kang, Moon-Jung
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.181-185
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    • 2010
  • The behavior of combustion-induced internal flow of SRM equipped with fin-slot grain and submerged nozzle is very complex and diverse. Cold air-flow test for 2D and 3D scale models of SRM has been done in order to specify the visualization method to analyze particular internal flow patterns such as roll-torque inducing flow. Swirl flow induced by asymmetric vortical tube also has been visualized through employing various light source and recording directions.

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