• 제목/요약/키워드: Jet impinging

검색결과 440건 처리시간 0.026초

충돌공기분류계(衝突空氣噴流系)에서 난류촉진체(亂流促進體)의 폭변화(幅變化)가 전열증진(傳熱增進)에 미치는 영향(影響) (Effect of Turbulence Promoter Width on Heat Transfer Augmentation in Impinging Air Jet System)

  • 금성민;서정윤
    • 설비공학논문집
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    • 제6권4호
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    • pp.427-438
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    • 1994
  • This experimental study was earned out to examine the heat transfer characteristics of a 2-dimensional impinging air jet on a flat plate with a set of square rods. The objectives of the study were to investigate the flow and heat transfer characteristics caused by the square rods and to find out the optimum rods arrangement. Experiment was carried out first without using the rods to establish the baseline heat transfer performance. Then, rods of different widths and clearances were installed to cause the turbulence on the fluid flow.

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충돌제트의 유동특성에 관한 실험적 연구(1) (An Experimental Study on Flow Characteristics of Impinging Jet (1))

  • 김동균;김정환;배석태;김시범;이영호
    • 한국마린엔지니어링학회:학술대회논문집
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    • 한국마린엔지니어링학회 2000년도 추계학술대회 논문집(Proceeding of the KOSME 2000 Autumn Annual Meeting)
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    • pp.37-42
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    • 2000
  • The flow characteristics of impinging jet flow are affected greatly by nozzle plate to distances. An sharp edge nozzle was used to achieve uniform mean velocity at the nozzle inlet, and its diameter is 10mm(d). Therefore, the flow characteristics on the impinging jet plate can be changed largely by the control of main flow. In the parent study, we investigate the effects of main flow length , its variable is nozle plate to distances( 12d, 10d, 8d, 6d and 4d).

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Impinging jet simulation of stationary downburst flow over topography

  • Mason, M.S.;Wood, G.S.;Fletcher, D.F.
    • Wind and Structures
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    • 제10권5호
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    • pp.437-462
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    • 2007
  • A non-translating, long duration thunderstorm downburst has been simulated experimentally and numerically by modelling a spatially stationary steady flow impinging air jet. Velocity profiles were shown to compare well with an upper-bound of velocity measurements reported for full-scale microbursts. Velocity speed-up over a range of topographic features in simulated downburst flow was also tested with comparisons made to previous work in a similar flow, and also boundary layer wind tunnel experiments. It was found that the amplification measured above the crest of topographic features in simulated downburst flow was up to 35% less than that observed in boundary layer flow for all shapes tested. From the computational standpoint we conclude that the Shear Stress Transport (SST) model performs the best from amongst a range of eddy-viscosity and second moment closures tested for modelling the impinging jet flow.

고속 원형충돌제트의 불안정 특성 (Instabilities of High-speed Impinging Circular Jets)

  • 임정빈;권영필
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 1997년도 추계학술대회논문집; 한국과학기술회관; 6 Nov. 1997
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    • pp.256-262
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    • 1997
  • The characteristics of the unstable impinging circular jet were investigated based on the frequency characteristics and the sound field of the impinging-tones. Two symmetric modes Si and S2, associated with low frequency and high frequency respectively, and one helical mode H have been observed by measuring frequency and phase-distribution around the jet. Radiation characteristics of impinging-tone were studied by measuring axial directivity. It was founded that the radiation patterns of symmetric and helical mode are different and it is toward the plate as the impinging distance increased. By estimating the convection velocity of the unstable jet, it was founded that the convection speed decreases with the frequency and its decreasing pattern varies with unstable modes S1, S2 and H, respectively.

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NUMERICAL ANALYSIS OF INTERACTION BETWEEN SUPERSONIC JET AND PERPENDICULAR PLATE

  • Yasunobu T;Matsuoka T;Kashimura H;Setoguchi T
    • 한국전산유체공학회지
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    • 제10권1호
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    • pp.39-44
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    • 2005
  • The numerical investigation of the interaction between the underexpanded supersonic jet and the perpendicular plate is carried out using the TVD numerical method. The wave structure in the flowfield and the pressure and temperature distributions on the plate surface are obtained by the numerical analysis. Especially, the influence of self-induced flow oscillation caused by the impinging jet and the characteristic of impinging jet are shown. From the result of the numerical analysis, it is concluded that the pressure and the temperature fluctuations on the plate surface strongly depends on the pressure ratio in the flowfield and the position of plate.

벽면제트류가 유입되는 충돌수분류유동에 배플이 미치는 효과에 관한 연구 (A Study on Effects of Baffle on Impinging Water Jet with wall jet inlet flow)

  • 최정식;오우준;조대환
    • 해양환경안전학회:학술대회논문집
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    • 해양환경안전학회 2009년도 춘계학술발표회
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    • pp.87-88
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    • 2009
  • 증발식 담수화 설비에서 증발기로 유입되는 유동의 속도특성은 플래시현상에 중요한 영향을 미친다. 이 연구에서는 벽면제트류가 유입되는 충돌수분류영역과 배플후류영역의 유동 속도에 배플의 높이가 미치는 효과에 관해 PIV계측을 적용해 실험적으로 고찰하였다.

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맥동주파수의 변화에 따른 충돌제트의 열전달 특성 (Heat Transfer Characteristics Of Impinging jet with Pulsating Frequency)

  • 김용일;박복춘;백병준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집B
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    • pp.278-284
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    • 2000
  • The method of Impinging jet was applied lots of part in industrial field as a cooling of as gas turbine blade, a annealing of metal and plastic sheets, drying of textile, veneer paper, X-ray medical devices, laser weapons and electronic components. This study's main factor is reciprocating Jet impingement perpendicular to the heated Surface. We researched the effect of heat transfer and enhancement with pulsating air jet. The pulsating air jet has an improvement in pulsating Frequencies((f= 0.5, 1, 1.5, 3Hz) and nozzle-to-plate distances($l/d=\;2{\sim}4,\;6{\sim}8,\;4{\sim}6,\;8{\sim}10$).

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원형 충돌 제트에서의 유동 및 온도 특성 (Flow and Temperature Characteristics in a Circular Impinging Jet)

  • 김정우;최해천
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.237-240
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    • 2002
  • In the present study, we perform LES of turbulent flow and temperature fields in a circular impinging jet at Re=5000 for two cases of H/D=2 and 6 (H denotes the distance between the jet exit and flat plate, and D does the diameter of the jet exit). In the case of H/D=2, the regular vortical structures observed in free jet do not exist because of the smaller distance than the potential core. The Nusselt number on the wall is largest at $r/D{\cong}10.67$ where vortex rings Impinge. At $r/D{\cong}1.5{\~}2.0$, the vortex rings induce the secondary vortices, resulting in a secondary peak in the Nusselt number there. In the case of H/D=6, the vortex rings change into three-dimensional vortical structures and the small-scale vortices impinge on the flat plate. The increase of turbulent intensity due to small-scale vortices results in the largest Nusselt number at the stagnation point.

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평면제트와 충돌면과의 거리변화에 따른 열전달 특성 (Heat Transfer characteristics of distance between impinging surface and a plane jet)

  • 김동건
    • Journal of Advanced Marine Engineering and Technology
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    • 제22권5호
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    • pp.588-594
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    • 1998
  • Heat transfer characteristics of distance between impinging surface and a plane jet were experi-mentally investigated. The local heat transfer coefficients were measured by a thermochromic liq-uid crystal(TLC) The jet Reynolds number studied was varied over the range from 10,000310 to 30,000310 the nozzle-to-plate distance (H/B) from 4 to 10. It was observed that the Nusselt number increases with Reynolds number the occurrence of the secondary peak in the Nusselt number is within the potential core region the potential core of the jet flow can reach the impinging surface so that the wall jet can a transition from laminar to turbulent flow resulting in a sudden increase in the heat transfer rate.

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충돌분류시스템의 열전달 특성에 관한 수치적 연구 (Numerical Study on Heat Transfer Characteristics in Impinging Air Jet System)

  • 금성민;김동춘
    • 한국태양에너지학회 논문집
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    • 제23권4호
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    • pp.55-61
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    • 2003
  • Heat transfer characteristics for an air jet vertically impinging on a flat plate with a set of hybrid rods was investigated numerically using the RNG k-$\varepsilon$turbulent model. A commercial finite-volume code FLUENT is used. The rods had cross sections of half circular and rectangular shapes. The heating surface was heated with a constant heat flux value of $1020W/m^2$. Parameters investigated were the jet Reynolds number, nozzle -to-plate spacing, the rod pitch and rod-to-plate clearance. The local and average Nusselt number were found to be dependent on the rod pitch and the clearance because installing rods disturbed the flow. Higher convective heat transfer rate occurred in the whole plate as well as in the wall jet region.