• Nuclear Engineering and Technology
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• 제51권4호
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• pp.996-1007
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• 2019

We investigated the influence of the aspect ratio (H/R) of the oxide layer on the reactor vessel heating in three-layer configuration. Based on the analogy between heat and mass transfers, we performed mass transfer experiments to achieve high Rayleigh numbers ranging from $6.70{\times}10^{10}$ to $7.84{\times}10^{12}$. Two-dimensional (2-D) semi-circular apparatuses having the internal heat source were used whose surfaces of top, bottom and side simulate the interfaces of the oxide layer with the light metal layer, the heavy metal layer, and the reactor vessel, respectively. Multi-cell flow pattern was identified when the H/R was reduced to 0.47 or less, which promoted the downward heat transfer from the oxide layer and possibly mitigated the focusing effect at the upper metallic layer. The top boundary condition greatly affected the natural convection of the oxide layer due to the presence of secondary flows underneath the cold light metal layer.

• 대한기계학회논문집B
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• 제37권4호
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• pp.367-375
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• 2013

본 연구는 타원형 핀-튜브 열교환기에 대해 AR, 피치, 와류발생기의 위치, 튜브 표면의 돌기형상에 따른 열전달계수 및 압력강하 특성을 수치해석으로 분석하였다. CFD해석시 경계조건으로는 튜브표면의 온도는 348 K이고, 입구공기속도는 1~5 m/s 범위로 가정하였고, 수치해석시 사용된 모델로는 민감도를 고려하여 RSM 7차 난류모델을 하였다. 해석결과로는 AR 및 세로피치가 작을수록 열전달률이 향상되는 것으로 나타났으며 가로피치에 대한 영향은 근소한 차이를 나타냈으며, 와류발생기의 설치는 튜브 전방에 위치할수록 열전달특성상 양호한 것으로 나타났다. 또한 튜브표면의 돌기형상은 톱니형보다 원형이 압력강하나 열전달특성이 유리한 것으로 나타났다.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2010년도 춘계학술대회 초록집
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• pp.225.1-225.1
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• 2010

Within recent years attention has been focused on the method of hydrogen storage using metal hydride reactor due to its high energy density, durability, safety and low operating pressure. In this paper, a numerical study is carried out to investigate the coupled heat and mass transfer process for absorption in a cylindrical metal hydride hydrogen storage reactor using a newly developed model. The simulation results demonstrate the evolution of temperature, equilibrium pressure, H/M atomic ratio and velocity distribution as time goes by. Initially, hydrogen is absorbed earlier from near the wall which sets the cooling boundary condition owing to that absorption process is exothermic reaction. Temperature increases rapidly in entire region at the beginning stage due to the initial low temperature and enough metal surface for hydrogen absorption. As time goes by, temperature decreases slowly from the wall region due to the better heat removal. Equilibrium pressure distribution appears similarly with temperature distribution for reasons of the function of temperature. This work provides a detailed insight into the mechanism and corresponding physicochemical phenomena in the reactor during the hydrogen absorption process.

• Journal of the Korean Society for Industrial and Applied Mathematics
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• 제20권4호
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• pp.333-354
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• 2016

The present investigation deals, heat and mass transfer characteristics with the effect of slip on the hydromagnetic pulsatile flow through a parallel plate channel filled with saturated porous medium. Based on the pulsatile flow nature, exact solution of the governing equations for the fluid velocity, temperature and concentration are obtained by using two term perturbation technique subject to physically appropriate boundary conditions. The expressions of skin friction, Nusselt number and Sherwood number are also derived. The numerical values of the fluid velocity, temperature and concentration are displayed graphically whereas those of shear stress, rate of heat transfer and rate of mass transfer at the plate are presented in tabular form for various values of pertinent flow parameters. By increasing the slip parameter at the cold wall the velocity increases whereas the effect is totally reversed in the case of shear stress at the cold wall.

• 한국산학기술학회논문지
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• 제16권5호
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• pp.2985-2992
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• 2015

본 연구에서는 엇갈린형 관군에 대해 ANSYS FLUENT v.14의 SST 난류모델을 적용하여 가로피치, 튜브표면, 와류발생기위치 등의 변화에 따른 열전달 및 압력강하 특성을 이론적으로 해석하였다. CFD 해석시 튜브표면의 온도는 363 K, 입구측 공기온도는 313 K이고 입구측 속도는 5 m/s에서 10 m/s까지 가정하였다. 그 해석결과로서 열전달계수는 가로피치에 대한 영향은 큰 차이가 없었고, 튜브표면의 돌기형상은 열전달 및 압력강하 특성에서 원형이 톱니형보다 적절하게 나타내었으며, 와류발생기의 설치 경우에는 열전달특성이 튜브의 전방부 위치가 후방부 위치보다 약 4.6% 정도로 우수함을 보였다.

• 한국추진공학회지
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• 제26권2호
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• pp.1-11
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• 2022

일반적인 축소 확대형 초음속 노즐에 대한 열해석에서 경계조건으로 사용되는 벽면의 열전달 계수는 노즐 전체의 열해석 정확도에 영향을 미친다. 이에 많은 열전달계수 도출 방법이 제안되어 왔으며, 본 연구에서는 각각의 기법들을 실제 실험 조건에서 열전달 계수를 계산하고 비교하고자 하였다. 이를 위해 기 수행된 벽면 등온 노즐의 열전달실험에 대해 이론 기반의 analogy 기법과 반경험식, 유체전산해석을 통해 열전달 계수를 도출하고 실험결과와 비교하였다. 해석 결과는 반경험식들은 전반적으로 다른 방법에 비해 대류 열전달 계수를 과도하게 예측하고, Prandtl-Taylor analogy 기법과 k-ω SST 모델을 적용한 전산해석 결과가 실험결과와 비교적 잘 일치하는 경향성을 보였다.

• 한국태양에너지학회 논문집
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• 제29권4호
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• pp.7-14
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• 2009

Nucleate pool boiling experiments with constant heat flux condition were performed using pure R11 and R113 for various surface angles under saturated pool condition. A circular heater of 1 mm diameter, with artificial cavity in the center, fabricated using MEMS technique and the high-speed controller were used to maintain the constant heat flux. Images of bubble growth were taken at 5,000 frames per second using a high-speed CCD camera. The bubble geometry was obtained from the captured bubble images. The effects of surface angles on the bubble growth behaviors were analyzed as dimensional scales for the initial and thermal growth regions. The parameters for the bubble growth behaviors were bubble radius, bubble growth rate, sliding velocity, bubble shape and advancing and receding contact angles. These phenomena require further analysis for various surface angles, but this study will provide good experimental data with constant heat flux boundary condition for such works.

• 대한기계학회논문집
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• 제19권7호
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• pp.1675-1683
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• 1995

A numerical study of the fluid flow and heat transfer characteristics of the two-dimensional impingement jet with a confinement plate has been carried out. The fluid flow was calculated by solving the full Navier-Stokes equation. In doing that, the well known SIMPLER algorithm was used and the trouble making convection term was discretized according to QUICKER scheme. The energy equation was simply solved by using the SOR method. For the Reynolds number of 10000, two channel heights, say 1.5 and 3.0 times the jet exit width, and two thermal boundary conditions constant wall temperature and constant wall heat flux were considered. Discrete heat sources were flush mounted along the impingement plate at a distance of 0, 2, 3, 4, 5, 6, 10, 12, times the jet exit width from the stagnation point. The length of each heat source is 4 times the jet exit width long. The Nusselt number averaged over each heat source was compared with experiment. Comparison shows that both calculations and experiment have the secondary peak of Nusselt number at downstream of stagnation point, even though there is a little quantitative difference in between. The difference is believed due to abscure thermal boundary condition in experiment and also accuracy of turbulence model used. The secondary peak is shown to be caused by rigorous turbulent flow motion generated as the wall jet flow is retarded and developes into the channel flow without flow reversal.

• 대한기계학회논문집B
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• 제21권4호
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• pp.579-588
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• 1997

The heat transfer and flow measurements from a convex curved surface to a circular impinging jet have been made. The flow at the nozzle exit has a fully developed velocity profile. The jet Reynolds number (Re) ranges from 11,000 to 50,000, the dimensionless nozzle-to-surface distance (L/d) from 2 to 10, and the dimensionless surface curvature (d/D) from 0.034 to 0.089. The results show that the stagnation point Nusselt number (N $u_{st}$ ) increases with increasing value of d/D. The maximum Nusselt number at the stagnation point occurs at L/d .ident. 6 to 8 for all Re's and d/D's tested. For larger L/d, N $u_{st}$ dependency on Re is stronger due to an increase of turbulence in the approaching jet as a result of the more active exchange of momentum with a surrounding air. The local Nusselt number decreases monotonically from its maximum value at the stagnation point. However, for L/d=2 and Re=23,000, and for L/d.leq.4 and Re=50,000, the stream wise Nusselt number distributions exhibit secondary maxima at r/d .ident. 2.2. The formation of the secondary maxima is attributed to an increase in the turbulence level resulting from the transition from a laminar to a turbulent boundary layer.ndary layer.

• 대한기계학회논문집B
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• 제37권10호
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• pp.941-951
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• 2013

축방향으로 벽면에서 일정한 열 유속의 경계조건을 갖는 곡관 유동에서 유동장 및 온도장에서의 Dean 수와 곡률의 영향을 알아보기 위한 층류 유동 및 열전달에 관한 3차원 수치모사를 수행하였다. 연구에서 수행된 레이놀즈 수의 범위는 100~4000이며 Prandtl 수는 0.71이다. 곡률 비는 0.01, 0.025, 0.05 그리고 0.1이다. 본 연구에서 계산된 축방향 속도 및 온도 분포, 국소 Nusselt 수는 기존의 수치 및 실험 결과들과 잘 일치하였다. 유동 및 열전달에 대한 곡률의 영향을 알아보기 위하여 저항계수 및 열전달 계수가 계산되었고 기존의 이론 및 실험 연구의 결과들과 비교하였다. Dean 수와 Prandtl 수에 의한 평균 Nusselt 수의 관계식을 유도하였다. 또한 곡률의 변화에 따른 난류 유동으로 천이하는 임계 레이놀즈 수의 변화를 알아보았다.