• 제목/요약/키워드: Low Reynolds Number Flow

검색결과 401건 처리시간 0.031초

난류촉진체에 의한 전자칩의 열전달촉진에 관한 연구 (Heat transfer enhancement in electronic modules using a turbulence promoter)

  • 박시우;정인기
    • 설비공학논문집
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    • 제11권6호
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    • pp.861-870
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    • 1999
  • An experimental study was carried out to investigate the effects of using various shapes of turbulence promoter on the heat-transfer enhancement of 2-D and 3-D arrays of rectangular modules in a rectangular channel for design of noiseless and low-powered cooling fan in the electronic systems. Measurements of heat/mass transfer coefficients were made using a naphthalene sublimation technique, and the friction factors were measured for Reynolds numbers in the range$3.3{\time}10^3$~$1.6{\time}10^4$. Flow visualization was peformed by oil-film method. It was found that heat transfer and pressure drop increased remarkably due to the existence of the promoter. The results of the performance evaluation based on equal pumping power were showed that substantial heat-transfer enhancement was obtained at low Reynolds number range by use of a turbulence promoter.

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환형 캐스케이드 내 고정된 터빈 블레이드 및 슈라우드에서의 열/물질전달 특성 (I) - 블레이드 끝단 인접 표면 - (Heat/Mass Transfer Characteristics on Stationary Turbine Blade and Shroud in a Low Speed Annular Cascade (I) - Near-tip Blade Surface -)

  • 이동호;조형희
    • 대한기계학회논문집B
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    • 제29권4호
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    • pp.485-494
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    • 2005
  • For the extensive investigation of local heat/mass transfer on the near-tip surface of turbine blade, experiments were conducted in a low speed stationary annular cascade. The turbine test section has a single stage composed of sixteen guide vanes and blades. The chord length and the height of the tested blade are 150 mm and about 125 mm, respectively. The blade has flat tip geometry and the mean tip clearance is about $2.5{\%}$ of the blade chord. Detailed mass transfer coefficient on the blade near-tip surface was obtained using a naphthalene sublimation technique. The inlet flow Reynolds number based on chord length and incoming flow velocity is changed from $1.0{\times}10^{5}\;to\;2.3{\times}10^{5}.$ Extremely complex heat transfer characteristics are observed on the blade surface due, to complicated flow patterns, such as flow acceleration, laminarization, transition, separation bubble and tip leakage flow. Especially, the suction side surface of the blade has higher heat/mass transfer coefficients and more complex distribution than the pressure side surface, which is related to the leakage flow. For all the tested Reynolds numbers, the heat/mass transfer characteristics on the turbine blade are the similar. The overall averaged $Sh_{c}$ values are proportional to $Re_{c}^{0.5}$ on the stagnation region and the laminar flow region such as the pressure side surface. However, since the flow is fully turbulent in the near-tip region, the heat/mass transfer coefficients are proportional to $Re_{c}^{0.8}.$

전산유동 해석을 이용한 수동의 유동 균질성 평가 (Estimation of Flow Uniformity in Water Tunnel by Using CFD Analysis)

  • 임영택;장조원;김문상
    • 한국항공운항학회지
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    • 제12권3호
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    • pp.13-24
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    • 2004
  • It is easier to view flow visualization by using a water tunnel rather than a smoke wind tunnel because of low speed at same Reynolds number. Using a water tunnel also produces more definite flow visualization by the use of various color dyes. The flow uniformity in test section is very significant for accuracy of the test because most flow experiments elicit results through the installation of a model in uniform flow. The purpose of small-size desktop-type water tunnel is not to produce quantitative measurements, but rather to give a visualization of the fluid flow phenomenon. However, uniformity in the test section affects the accuracy of the results. Accordingly, this research estimates uniformity in a water tunnel test section by using the commercially available CFD code FLUENT. Results of the CFD analysis show that the flow uniformity of the test section is good.

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An Experimental Study of Developing and Fully Developed Flows in a Wavy Channel by PIV

  • Kim, Sung-Kyun
    • Journal of Mechanical Science and Technology
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    • 제15권12호
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    • pp.1853-1859
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    • 2001
  • An experimental study is presented for a flow field in a two dimensional wavy channels by PIV. This flow has two major applications such as a blood flow simulation and the enhancement of heat transfer in a heat exchanger. While the numerical flow visualization results have been limited to the fully developed cases, existing experimental results of this flow were simple qualitative ones by smoke or dye streak test. Therefore, the main purpose of this study is to produce quantitative flow data for fully developed and developing flow regimes by the Correlation Based Correction PIV (CBC PIV) and to conjecture the analogy between flow characteristics and heat transfer enhancement with low pumping power. Another purpose of this paper is to examine the onset position of the transition and the global mixing, which results in transfer enhancement. PIV results on the Fully developed and developing flow in a wavy channel at Re=500, 1000 and 2000 are obtained. for the case Reynolds Number equals 500, the PIV results are compared with the finite difference numerical solution.

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2차원 파형 채널의 형상변화에 따른 열유동 특성 (Thermo-Hydraulic Characteristics of Two-Dimensional Wavy Channels with Different Shape Parameters)

  • 김기완;김선주
    • 대한기계학회논문집B
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    • 제38권1호
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    • pp.1-8
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    • 2014
  • 본 연구에서는 2차원 파형 채널의 여러 형상($0.5{\leq}{\in}{\leq}1.5$, $0.1{\leq}{\gamma}{\leq}0.4$)에 대한 층류 열유동 수치해석을 수행하고, 형상변화에 따른 열유동특성을 비교 분석하였다. 전자장비 냉각용으로 적용되고 있는 PAO(Polyalphaolefin)를 작동유체로 고려하였고, 균일한 물성치와 주기적으로 발달한 유동 및 채널벽면에서의 등온 조건을 가정하였다. 층류유량조건($1{\leq}Re{\leq}1000$)에서 레이놀즈수에 따른 유선 및 온도 분포, 등온 Fanning 마찰계수, Colburn 계수를 제시하였고, 분석 결과 낮은 레이놀즈(Re<50) 구간에서는 채널주름비가 크고 채널간격비가 작을수록, 높은 레이놀즈($Re{\geq}50$) 구간에서는 채널주름비와 채널간격비가 모두 클수록 열전달이 향상되었다.

인젝터 형상 변화에 따른 Gel 추진제의 유동 특성 연구 (Study of Flow Characteristics of Gel Propellant through Various Injector Geometries)

  • 오정수;전두성;최상태;김덕윤;최양호;이정혁;문희장
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제35회 추계학술대회논문집
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    • pp.300-303
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    • 2010
  • 다양한 형상의 인젝터 내부 젤 추진제 유동을 수치적으로 연구하였다. 모사 젤 추진제의 유변학적물성치를 측정하고 plain-orifice, chamfered-orifice 및 venturi 형상 인젝터의 유동 특성을 분석하였다. Plain-orifice 및 chamfered-orifice 인젝터의 경우 하류방향으로 유동이 진행할수록 점도가 높아지는 특성이 나타났으며 Venturi 형상의 경우 인젝터 내부 유동에서 낮은 점도가 지속적으로 유지됨을 알 수 있었다. Reynolds 수가 증가할수록 이러한 경향이 뚜렷하게 나타나는 것이 확인되었다.

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노즐 형상비가 바이오디젤 연료의 노즐 내부 및 외부 유동 특성에 미치는 영향 (Effects of Nozzle Length-diameter Ratio on Internal and External Flow Characteristics of Biodiesel Fuel)

  • 박수한;서현규;이창식
    • 한국자동차공학회논문집
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    • 제15권4호
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    • pp.94-100
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    • 2007
  • The purpose of this work is to investigate the effect of properties of diesel and biodiesel fuels on the nozzle cavitation and the effect of the length/diameter(L/D) ratio on internal and external flow pattern of nozzle at the various injection conditions. In order to study the effect of the L/D ratio on the nozzle cavitation characteristics of diesel and biodiesel, the characteristics of cavitation flow in the nozzle are visualized and analyzed at the injection pressure of 0.1 MPa to 0.7 MPa by using the visualized images. It was founded that the cavitation was formed in the nozzle orifice at the low injection pressure and the breakup of the issuing liquid jet was promoted at the low L/D ratio. When the L/D ratio decrease, cavitation beginning and growth were affect by cavitation number and Reynolds number.

Numerical Investigation of Cross-Flow Around a Circular Cylinder at a Low-Reynolds Number Flow Under an Electromagnetic Force

  • Kim, Seong-Jae;Lee, Choung-Mook
    • Journal of Mechanical Science and Technology
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    • 제16권3호
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    • pp.363-375
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    • 2002
  • The effect of the electromagnetic force (or Lorentz force) on the flow behavior around a circular cylinder is investigated by computation. Two-dimensional unsteady flow computation for Re=10$^2$is carried out using a numerical method of finite difference approximation in a curvilinear body-fitted coordinate system by solving the momentum equations including the Lorentz force as a body force. The effect of spatial variations of the Lorentz forcing region and forcing direction along the cylinder circumference is investigated. The numerical results show that the Lorentz force can effectively suppress the flow separation and oscillation of the lift force of circular cylinder cross-flow, leading to reduction of drag.

NACA 4412 날개의 지면효과에 대한 2차원 공력 해석 (2-DIMENSIONAL AERODYNAMIC SIMULATION ON THE GROUND EFFECT OF THE NACA 4412 AIRFOIL)

  • 김윤식;이재은;신명수;강국진;권장혁
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2006년도 추계 학술대회논문집
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    • pp.199-205
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    • 2006
  • Two dimensional turbulent flow simulations on the low Mach number - high Reynolds number flow about the NACA 4412 airfoil are carried out as the airfoil approaches a ground. It has been turned out that angle of attack between 2 and 8 is recommended for the airfoil to utilize the benefit of ground effect. For the large angle of attack, the increment of lift due to the ground effect is eliminated and negative aerodynamic effect such as destabilizing aspect in static longitudinal stability are occurred as the airfoil approaches a ground.

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CO concentration distribution in a tunnel model closed at left end side using CFD

  • Peng, Lu;Lee, Yong-Ho
    • Journal of Advanced Marine Engineering and Technology
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    • 제37권3호
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    • pp.282-290
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    • 2013
  • A primary air pollutant as an indicator of air quality released from incomplete combustion is Carbon monoxide. A study of the distributions of CO concentration with no heat source in a tunnel model closed at left end side is simulated with a commercial CFD code. The tunnel model is used to investigate the CO concentration distributions at three Reynolds numbers of 990, 1970, and 3290. which are computed by the inlet velocities of 0.3, 0.6 and 1.0 m/s. The CFD predictive approaches can be useful for a better design to analyze the distributions of CO concentrations. In the case of the tunnel model closed at left end side alone, the concentration changes of x/H=-5 and -2.5 have the similar laminar characteristics like the case of the tunnel model closed at both end sides expecially at low values of Reynolds number. Irregular average CO concentration variations at Re=1790 are considered that the transition from laminar to turbulent flow occurs even in three different tunnel models.