• 제목/요약/키워드: Adiabatic Wall

검색결과 117건 처리시간 0.025초

휴대용 PC내에 실장된 강제공랭 모듈 주위의 유체유동과 온도분포 (Fluid Flow and Temperature Distribution around a Surface-Mounted Module Cooled by Forced Air Flow in a Portable Personal Computers)

  • 박상희;신대종;이인태
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.729-732
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    • 2002
  • This paper reports an experimental study around a module about forced air flow by blower($35{\times}35{\times}6mm^3$) in portable PC(10mm high, 200mm wide, and 235mm long). The channel inlet flow velocity has been varied between 0.26, 0.52 and 0.78m/s. The power input to the module is 4Wthis report, particular attention is directed to the fluid flow and adiabatic wall temperature($T_(ad)$) around a module which is under fluid mechanical and thermal influences of the module. The fluid flow around a module was visualized using PIV system. Liquid crystal thernography is used to determine the adiabatic wall temperature around a heated module on an acrylic board. Plots of $T_(ad)$ (or F) show marked effects of dispersion of thermal wake near the module.

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CFDS기법에 연계된 특성경계조건에 응용성에 대한 소개 (Applications of Characteristic Boundary Conditions within CFDS Numerical Framework)

  • 홍승규;이광섭
    • 한국전산유체공학회지
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    • 제5권1호
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    • pp.43-59
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    • 2000
  • Characteristic boundary conditions are discussed in conjunction with a flux-difference splitting formulation as modified from Roe's linearization. Details of how one can implement the characteristic boundary conditions which are made compatible with the interior point formulation are described for different types of boundaries including subsonic outflow and adiabatic wall. The validity of boundary conditions are demonstrated through computation of transonic airfoil, supersonic ogive-cylinder, hypersonic cylinder, and S-duct internal flows. The computed wall pressure distributions are compared with published experimental and computed data. Objectives of this paper are thus to give insight of formulation procedure of a flux-difference splitting method and to pave ways for other users to adopt present boundary procedure on their numerical methods.

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The Effect of Non-condensable Gas on Direct Contact Condensation of Steam/Air Mixture

  • Lee, Hanchoon;Kim, Moohwan;Park, Suki
    • Nuclear Engineering and Technology
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    • 제33권6호
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    • pp.585-595
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    • 2001
  • A series of experiments have been carried out to investigate the effects of non-condensable gas on the direct contact film condensation of vapor mixture under an adiabatic wall condition. The average heat transfer coefficient of the direct contact condensation was obtained at the atmospheric pressure with four main parameters ; air-mass fraction, mixture velocity, film Reynolds number, and the degree of water film subcooling having an influence on the condensation heat transfer coefficient. With the analysis of 88 experiments, a correlation of the average Nusselt number for direct contact film condensation of steam/air mixture at an adiabatic vertical wall was proposed as functions of film Reynolds number, mixture Reynolds number, air mass fraction, and Jacob number. The average heat transfer coefficient for steam/air mixture condensation decreased significantly while air mass fraction increased. The average heat transfer coefficients also decreased as the Jacob number increased, and were scarcely affected by the film Reynolds number below a mixture Reynolds number of about 245,000.

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맥동관의 2차원 해석모델 (Two-Dimensional Analysis Model of a Pulse Tube)

  • 백상호;정은수
    • 한국초전도저온공학회:학술대회논문집
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    • 한국초전도저온공학회 1999년도 제1회 학술대회논문집(KIASC 1st conference 99)
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    • pp.157-160
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    • 1999
  • Enthalpy transport in a pulse tube was investigated by two-dimensional analysis of mass, momentum and energy equations of the gas as well as energy conservation of the tube wall. The mean temperature of the gas and the tube wall was obtained directly by assuming that the outer surface of a pulse tube is adiabatic. Effects of operating frequency, tube wall thickness, velocity ratio and velocity phase angle between both ends of a pulse tube on net enthalpy flow were shown.

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오목벽면이 있는 밀폐공간에서 자연대류 (Natural Convection from the Concave Wall in a Square Enclosure)

  • 박태선
    • 한국전산유체공학회지
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    • 제7권1호
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    • pp.28-35
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    • 2002
  • The effect of concave curvature on the natural convection has been numerically studied using the higher-order finite difference method. The heating wall in a enclosure is approximated by a cosine function. The heat transfer coefficient is analyzed for three Rayleigh numbers and five amplitudes. For Ra = 10/sup 8/ the separation and reattachment are observed on the adiabatic walls. The wall heat transfer are slightly changed by the increasing curvatures.

사각공동내 자연대류에서 측면 단열벽에 의한 영향 (Effect of Adiabatic Sidewalls on Natural Convection in a Rectangular Cavity)

  • 허정환;정범진
    • 대한기계학회논문집B
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    • 제34권9호
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    • pp.825-834
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    • 2010
  • 사각공동내 자연대류 열전달 실험에서, 단열벽에 의해 열전달이 저하가 관찰되는 영역을 실험적으로 그리고 수치해석적으로 평가하였다. $Gr_H$$1.53\times10^7$부터 $1.01\times10^{10}$까지 변화시키며, 단열벽이 존재할 때와 그렇지 않을 때를 구분하여 열전달률을 측정하였다. FLUENT 실험의 결과를 예측할 수 있는지 확인하고 실험으로 수행하기 어려운 매우 좁은 영역에 대해 FLUENT를 수행하였다. 실험과 FLUENT의 결과를 다른 연구와 비교한 바 일치함을 보였다. 단열벽이 전체 열전달에 미치는 영향은 예상과 같이 단열벽 근처의 매우 좁은 영역에 국한하여 나타남을 확인하였다. 본 연구는 유사성(Analogy) 원리를 이용하여 열전달계를 전기도금계의 물질전달계로 모사하는 방법론을 개발하는 과정에서 실험을 효율화하고자 하는 방안을 강구하기 위하여 추진되었다. 본 연구를 통하여 단열벽간 거리(전극의 폭)를 매우 줄일 수 있는 이론적 근거를 확보하였다.

1 $Nm^3/h$ 규모 합성천연가스(SNG) 합성 시스템의 운전 특성 (Operating Characteristics of 1 $Nm^3/h$ Scale Synthetic Natural Gas(SNG) Synthetic Systems)

  • 김진호;강석환;류재홍;이선기;김수현;김문현;이도연;유영돈;변창대;임효준
    • Korean Chemical Engineering Research
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    • 제49권4호
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    • pp.491-497
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    • 2011
  • 본 연구에서는 CO, $H_2$가 주성분인 모사합성가스를 이용하여 합성천연가스(SNG, Synthetic Natural Gas) 제조공정을 평가하기 위하여, 3종류의 SNG 합성반응시스템을 제안하였다. 제시된 공정은 다단 단열반응시스템, 재순환이 있는 다단 단열반응시스템 그리고 강제냉각방식의 수냉각반응시스템이다. 3개의 연속된 반응기로 구성된 다단 단열반응시스템에서의 1차반응기에서는 온도가 최대 $800^{\circ}C$까지 상승하였으며, 이로 인한 수성가스전환반응으로 인해 $CO_2$가 다른 시스템에 비해 많이 생성되었으며, SNG 내의 $CH_4$ 농도는 90.1% 정도를 얻었다. 다단 단열반응시스템의 문제점을 해결하기 위해 재순환이 있는 다단 단열반응시스템에서는 반응기의 온도제어를 위해 일부 전환가스를 재순환한 것으로, $CH_4$는 최대 96.3%를 얻었다. 이러한 다수개의 반응기로 구성된 단열반응기의 단점을 해결하여 반응기 개수를 줄일 수 있는 쉘과 튜브 형태의 반응기로 구성된 강제냉각방식의 수냉각시스템에서는 쉘 측으로 냉각수를 공급하여 반응열을 흡수하는 형태로, 공급되는 냉각수의 유량과 압력에 의해 온도를 제어할 수 있다. 이 시스템에서는 최대 $CH_4$는 최대 99.2%를 얻었으며, 1차 반응기인 강제냉각방식의 수냉각반응기 출구에서의 97% 이상의 $CH_4$ 농도를 얻을 수 있음을 확인하였다.

Thermal Analysis of a Film Cooling System with Normal Injection Holes Using Experimental Data

  • Kim, Kyung-Min;Lee, Dong-Hyun;Cho, Hyung-Hee;Kim, Moon-Young
    • International Journal of Fluid Machinery and Systems
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    • 제2권1호
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    • pp.55-60
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    • 2009
  • The present study investigated temperature and thermal stress distributions in a film cooling system with normal injection cooling flow. 3D-numerical simulations using the FEM commercial code ANSYS were conducted to calculate distributions of temperature and thermal stresses. In the simulations, the surface boundary conditions used the surface heat transfer coefficients and adiabatic wall temperature which were converted from the Sherwood numbers and impermeable wall effectiveness obtained from previous mass transfer experiments. As a result, the temperature gradients, in contrast to the adiabatic wall temperature, were generated by conduction between the hot and cold regions in the film cooling system. The gradient magnitudes were about 10~20K in the y-axis (spanwise) direction and about 50~60K in the x-axis (streamwise) direction. The high thermal stresses resulting from this temperature distribution appeared in the side regions of holes. These locations were similar to those of thermal cracks in actual gas turbines. Thus, this thermal analysis can apply to a thermal design of film cooling holes to prevent or reduce thermal stresses.

Application of Characteristic Boundary Conditions

  • 홍승규;이광섭
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1996년도 춘계 학술대회논문집
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    • pp.74-84
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    • 1996
  • Characteristic boundary conditions are discussed in conjunction with a flux-difference splitting formulation as modified from Roe's linearization. Details of how one can implement the characteristic boundary conditions which are compatible with the discrete formulation at interior points are given for different types of boundaries including subsonic outflow and adiabatic wall. The latter conditions are demonstrated through computation of supersonic ogive-cylinder flow at high angle of attack and the computed wall pressure distribution is compared with experiment.

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그린팀버월 패널의 열전달 특성 (Heat transfer of green timber wall panels)

  • 김윤희;장상식;신일중
    • 농업과학연구
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    • 제38권1호
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    • pp.115-120
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    • 2011
  • 20% of total energy use to sustain temperature of building inside. In this reasons, researchers effort to improve the thermal insulation capacity with new wall system. Using appropriate materials and consisting new wall system should considered in energy saving design. OSB(Oriented strand board), Larch lining board used to consist wall system. $2{\sim}6$ Larch lining board has tongue & groove shape for preventing moisture. Comparing with gypsum board and green timber lining board as interior sheathing material, temperature difference of Green timber wall system was bigger than temperature difference of gypsum board wall system. This aspects indicate that Green timber wall system was revealed higher thermal insulation property than gypsum board wall system. Gypsum board portion transfer heat easily because temperature difference gradient of gypsum board wall system was smaller than OSB wall system. Total temperature variation shape of G-4-S and G-6-S show similar model but, temperature variation shape in green timber wall portion assume a new aspect. The purpose of this study was that possibility of thermal insulation variation and new composition of wall system identify to improve thermal insulation performance. In the temperature case, this study shows possibility of improving thermal insulation performance. Humidity, sunshine and wind etc. should considered to determine building adiabatic properties.