• Title/Summary/Keyword: Pulsating Fiow

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Behavior and flow characteristics of pulsating flow in the jetflow region through cylindrical chokes (유압관로내 원통형 초크의 분류영역에서 맥동유동의 거동과 유동특성에 관한 연구)

  • ;;Moh, Y. W.
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.19 no.11
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    • pp.3041-3053
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    • 1995
  • Cylindrical chokes are used widely as components of hydraulic equipments. The dynamic characteristics between flowrate and pressure drop through the cylindrical chokes were discussed by the frequency characteristics of the chokes. It was assumed no pressure recovery occurred near the downstream of the choke. The pulsating jetflow from the outlet of cylindrical chokes show very complex behaviours which are quite different from the steady jet flow but it's not clarified quantitatively. In order to utilize the chokes as a flowmeter, it is indispensable to discuss the estimation of the dynamics of pressure drop in the downstream jetflow region of cylindrical chokes. In this experimental study, it is clarified that the reattachment length depended on pressure wave is compared with it depended on velocity wave. A pulsating flow is verified by visualization method. In the present study, the flow characteristic variables of laminar pulsating flow are investigated analytically and experimentally in a circular pipe. Characteristic parameters of the ratios of inertia(.PHI.$_{t,1}$) and viscous(.PHI.$_{z,1}$) term to pressure term are introduced to describe the flow pattern of laminar pulsating flow. flow.low.

Numerical Analysis of Heat Transfer in Pulsating Turbulent Pipe Flow (원관내 맥동난류유동에서의 열전달 수치해석)

  • 박희용;이관수;김창기
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.14 no.5
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    • pp.1282-1289
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    • 1990
  • A numerical solution for heat transfer of pulsating turbulent pipe flow was presented under the condition of fully developed dynamic regime and uniform well heat flux. The k-.epsilon. turbulent model was adopted to describe turbulent characteristics. The results were given at following conditions ; Time-averaged Reynolds number equal to 10000 ; Strouhal number ranged from 0.0005 to 0.05 ; The peak velocity fluctuation varied from 20 to 80 percent of the mean velocity. It was found that the effect of pulsation on local heat transfer rate is greater at downstream than upstream and the heat transfer was increased or decreased according to the pulsating conditions.