• Title/Summary/Keyword: Channel height

Search Result 466, Processing Time 0.025 seconds

The Study about Cooling Effect of a Heated module in a Horizontal Channel with a Variation of Channel Height (수평채널 밑면에 부착된 단일 발열모듈에서 채널높이의 변화에 따른 냉각특성 연구)

  • 이진호;유갑종;장준영;김병하
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
    • /
    • v.13 no.5
    • /
    • pp.348-355
    • /
    • 2001
  • The coupled conduction and convection heat transfer from a protruding heated module in a horizontal channel with a variation of channel height is experimentally investigated. The input power to the module is 3, 7W and thermal resistance of module support is 0.06 , 1.03 and 158K/W. the Reynolds number ranged from 350 to 4500 corresponding to the inlet velocity(0.4~1.3 m/s) and channel height(11~35 mm). The results were obtained that the decrease of thermal resistance of module support reduces the module temperature by redistributing the heat flux and the overall thermal resistance of the module. In the study the effect of channel height is very significant in the adiabatic condition, but negligible in the conjugate condition. Finally, correlations for Nusselt number and $Q_B$/Q with a variation of Reynolds number were developed respectively.

  • PDF

Analysis of laminar forced convection for optimal design of parallel plates with protrusions (돌출부를 갖는 평행평판의 최적 설계를 위한 층류강제대류 해석)

  • 이관수;박철균
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
    • /
    • v.10 no.1
    • /
    • pp.129-136
    • /
    • 1998
  • Pressure drop and heat transfer characteristics of a periodically fully developed flow in the flat channel with protrusions are investigated. The effects of shape and location of protrusion on the pressure drop and heat transfer are numerically analyzed in the present study. Taguchi method is used to optimize these parameters. It is found that the ratio of the height of protrusion to channel height shows larger influence on the pressure drop and heat transfer than the ratio of the length of protrusion to module length. As the height of protrusion increases, pressure drop and heat transfer increase, but if the height of protrusion exceeds 2/3 of the channel height, there is a substantial pressure drop. The results also show that the optimal length and height of protrusion are half of the module length and half of the channel height, respectively.

  • PDF

Effect of Anode Gas Channel Height on Gas Diffusion and Cell Performance in a Molten Carbonate Fuel Cell (용융탄산염 연료전지 연료극 기체 유로 높이에 따른 가스 확산 및 단전지 성능 변화 연구)

  • Lee, Jung-Hyun;Kim, Do-Hyung;Kim, Beum-Ju;Kang, Seung-Won;Lim, Hee-Chun
    • Transactions of the Korean hydrogen and new energy society
    • /
    • v.20 no.6
    • /
    • pp.479-484
    • /
    • 2009
  • The effect of anode gas channel height on gas diffusion and cell performance in a 100 $cm^2$ class molten carbonate single cell is investigated. Single cell separators with three different channel height are used. The effect of the gas channel height on the distribution of the reactive gas concentration is evaluated by the two-dimensional concentration diffusion equation. The overpotential caused by concentration drop with different channel height is estimated by the voltage decay related to diffusion of reactants, well known as concentration polarization, using limiting current density. The estimation could have the possibility to identify the reactant mass transfer polarization in the complicate factors of the overall electrodes.

Investigation of Characteristics of Waves Generated in Two-Dimensional Wave Channel (2차원 조파수조에서의 파 생성 특성 조사)

  • Ahn, Jae-Youl;Choi, Jung-Kyu;Kim, Hyoung-Tae
    • Journal of Ocean Engineering and Technology
    • /
    • v.27 no.4
    • /
    • pp.68-75
    • /
    • 2013
  • This paper investigates the characteristics of waves generated by a flap-type wave maker in a two-dimensional wave channel. Measurements are carried out for various water depths, wave heights, periods, and lengths capacitance-type wave height gages. The experimental results are shown to satisfy the dispersion relation of the linear wave theory. For waves with a small height and long period, the wave profiles agree well with those of the linear wave theory. However, as the wave height and period become higher and shorter, respectively, it is shown that the wave profiles measured in the present experiments are different from the linear wave profiles, and the measured wave heights are smaller than the target wave heights, which may be due to the non-linearity of the waves. As the wave progresses toward the channel end, the wave height gradually decreases. This reduction in the wave height along the wave channel is explained by the wave energy dissipation due to the friction of the side walls of the channel. The performance of the wave absorber in the channel is found to be acceptable from the results of the wave reflection tests.

Effect of Rib Height on Turbulence and Convective Heat Transfer (리브의 높이가 난류 및 열전달특성에 미치는 영향)

  • Nine, Md.J.;Kim, S.J.;Jeong, H.M.;Chung, H.S.;Rahman, M.Sq.
    • Journal of Power System Engineering
    • /
    • v.16 no.6
    • /
    • pp.30-37
    • /
    • 2012
  • Effect of rib heights is found as significant parameter to enhance convective heat transfer performance under laminar and low turbulent regime. Circular ribs with different ribheight to channel height ratios, e/H = 0.05, 0.1, 0.15, are fabricated over the copper substrate respectively in a rectangular duct having 7.5 cross sectional aspect ratio. Only one rib pitch to rib height ratio (P/e = 10) has been chosen for all different height ribs. The result shows that the arithmetic average of turbulence intensity decreases with decreasing roughness height calculated between two ribs under laminar and low turbulent region. It occurs because the area of recirculation and reattachment zone also decreases with decreasing rib height. Optimum thermal enhancement factor is derived by 0.1 rib height to channel height ratio under low turbulent region but 0.15 rib height to channel height ratio gives maximum subjected to laminar flow.

Numerical Analysis in a 1 kWe SOFC Stack for Variation of the Channel Height in Separators (분리판의 채널 높이에 따른 1 kWe 급 고체산화물 연료전지 스택 수치 해석)

  • YIN, HAOYUAN;KIM, YOUNG JIN;YI, KUNWOO;KIM, HYEON JIN;YUN, KYONG SIK;YU, JI HAENG
    • Transactions of the Korean hydrogen and new energy society
    • /
    • v.33 no.5
    • /
    • pp.550-556
    • /
    • 2022
  • In this study, the flow uniformity was analyzed by performing numerical analysis on the 1 kWe internal manifold type solid oxide fuel cell stack according to the channel height of the separator. Also, it was examined by varying the fuel utilization rate and oxygen utilization rate. From the calculation results, we found that as the channel height of the separator decreased, the pressure drop increased exponentially. In addition, it was found that as the channel height of the separator decreased, the gas flow resistance inside the unit cell increased, and the flow resistance increased the pressure drop, thereby improving the flow uniformity inside the stack. Finally, the calculation results showed that as the fuel and oxygen utilization increased, the flow uniformity also improved.

Analysis on Thermal Effects of Process Channel Geometry for Microchannel Fischer-Tropsch Reactor Using Computational Fluid Dynamics (전산유체역학을 이용한 Fischer-Tropsch 마이크로채널 반응기 반응채널구조에 따른 열적 효과 분석)

  • Lee, Yongkyu;Jung, Ikhwan;Na, Jonggeol;Park, Seongho;Kshetrimayum, Krishnadash S.;Han, Chonghun
    • Korean Chemical Engineering Research
    • /
    • v.53 no.6
    • /
    • pp.818-823
    • /
    • 2015
  • In this study, FT reaction in a microchannel was simulated using computational fluid dynamics(CFD), and sensitivity analyses conducted to see effects of channel geometry variables, namely, process channel width, height, gap between process channel and cooling channel, and gap between process channels on the channel temperature profile. Microchannel reactor considered in the study is composed of five reaction channels with height and width ranging from 0.5 mm to 5.0 mm. Cooling surfaces is assumed to be in isothermal condition to account for the heat exchange between the surface and process channels. A gas mixture of $H_2$ and CO($H_2/CO$ molar ratio = 2) is used as a reactant and operating conditions are the following: GHSV(gas hourly space velocity) = $10000h^{-1}$, pressure = 20 bar, and temperature = 483 K. From the simulation study, it was confirmed that heat removal in an FT microchannel reactor is affected channel geometry variables. Of the channel geometry variables considered, channel height and width have significant effect on the channel temperature profile. However, gap between cooling surface and process channel, and gap between process channels have little effect. Maximum temperature in the reaction channel was found to be proportional to channel height, and not affected by the width over a particular channel width size. Therefore, microchannels with smaller channel height(about less than 2 mm) and bigger channel width (about more than 4 mm), can be attractive design for better heat removal and higher production.

Effects of Geometry of a Boot-Shaped Rib on Heat Transfer and Pressure Drop (신발형 리브의 형상변화가 열전달 및 압력 강하에 미치는 영향)

  • Seo, Jae-Won;Kim, Jun-Hee;Kim, Kwang-Yong
    • The KSFM Journal of Fluid Machinery
    • /
    • v.18 no.3
    • /
    • pp.66-73
    • /
    • 2015
  • This paper deals with a parametric study on boot-shaped ribs in a rectangular cooling channel. Numerical analysis of the flow and heat transfer was performed using three-dimensional Reynolds averaged Navier-Stokes equations with the Speziale, Sarkar and Gatski turbulence model. The parametric study was performed for the parameters, tip width-to rib width, tip height-to-rib height, rib height-to-channel height, and rib height-to-width ratios. To assess the cooling performance and friction loss, Numsselt number and friction factor were defined as the performance parameter, respectively. The results showed that the cooling performance and friction loss were seriously affected by the four geometric parameters.

The Temporal Changes of Channel Section in Naeseongcheon River, Kyeongbuk Province (경북 내성천 하도 단면의 시계열적 변화)

  • Lee, Gwang-Ryul;Kim, Dae Sik
    • Journal of The Geomorphological Association of Korea
    • /
    • v.18 no.2
    • /
    • pp.53-63
    • /
    • 2011
  • The changes and causes of channel section in Naeseongcheon River, a tributary of Nakdong River, during the long(1984~2001) and short(2009~2011) periods are analyzed. There are the declines of channel height with a maximum of approximately 2m in the most areas of the lower reaches during the past 20 years. These are thought as the influences of active aggregate collections and river dredging. The size of sand bar within the channel at the NM1 decreases greatly during the past 2 years. This may results from the decrease of sediment supply due to the Yeongju Dam construction in the upper reaches. However, the NM2 and NL2 where the natural channel are preserved experience the slight increase of height during the past 2 years. Therefore, the anthropogenic channel interferences in Naeseongcheon River have greatly influenced on the declines of channel height by the decrease of sediment supply.

Steady Aerodynamic Characteristics of a Wing Flying Over a Nonplanar Ground Surface Part II : Channel

  • Han Cheol-Heui;Kim Hak-Ki;Cho Jin-Soo
    • Journal of Mechanical Science and Technology
    • /
    • v.20 no.7
    • /
    • pp.1051-1058
    • /
    • 2006
  • The steady aerodynamic characteristics of a wing flying over a channel are investigated using a boundary-element method. The present method is validated by comparing the computed results with the measured data. Compared with a flat ground surface, the channel fence augmented the lift increase and induced drag reduction. When the fence is lower than the wing height, the gap between the wingtip and the fence does not affect the aerodynamic characteristics of the wing much. When the fence is higher than the wing height, the close gap increased the lift. The induced drag is reduced when the wing is placed near the ground or at the same height as the fence. It is believed that present results can be used in the conceptual design of the high-speed ground transporters flying over the channel.