• 제목/요약/키워드: Heat fluxes

검색결과 367건 처리시간 0.022초

중력방향과 대향류인 저속 원형노즐 제트충돌에 의한 원형평판에서의 열전달 현상 (The Study of Heat Transfer on a Heated Circular Surface by an Impinging, Circular Water Jet with the Low Velocity Against the Direction of Gravity)

  • 김기태;엄용균
    • 대한기계학회논문집B
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    • 제33권12호
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    • pp.983-991
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    • 2009
  • The heat transfer phenomenon was investigated in this study when a circular water jet with low velocity flows to the downward facing heated circular plate and against the direction of gravity. Data are presented for jet flow rate between 0.23 and 2.3 l/min, jet fluid temperature of 24$^{\circ}C$, heat fluxes between 345 and 687 W/m$^2$, H/D=1, 2 and 3 with a single round jet diameter 2mm. The effects of heat flux, jet velocity and H/D on the local heat transfer are investigated in for the various regions of jet impingement. The local heat transfer distributions are analyzed based on the visualization of jet flow field. Data from experimental results are correlated by expressions of the form Nu=0.01$Re^{0.58}{\cdot}Pr^{0.4}$.

혼합냉매 R-407C의 증발 열전달과 압력강하 (Evaporation Heat Transfer and Pressure Drop of Mixture Refrigerant R-407C)

  • 노건상;오후규;손창효
    • Journal of Advanced Marine Engineering and Technology
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    • 제32권4호
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    • pp.542-549
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    • 2008
  • The evaporation heat transfer coefficient and pressure drop of R-22 and R-407C in a horizontal copper tube were investigated experimentally. The main components of the refrigerant loop are a receiver, a compressor, a mass flow meter, a condenser and a double pipe type evaporator (test section). The test section consists of a smooth copper tube of 6.4 mm inner diameter. The refrigerant mass fluxes were varied from 100 to $300\;kg/m^2s$ and the saturation temperature of evaporator were $5^{\circ}C$. The evaporation heat transfer coefficients of R-22 and R-407C increase with the increase of mass flux and vapor quality. The evaporation heat transfer coefficients of R-22 is about $5.68{\times}46.6%$ higher than that of R-407C. The evaporation pressure drop of R-22 and R-407C increase with the increase of mass flux. The pressure drop of R-22 is similar to that of R-407C. In comparison with test results and existing correlations, correlations failed to predict the evaporation heat transfer coefficient of R-22 and R-407C. therefore, it is necessary to develope reliable and accurate predictions determining the evaporation heat transfer coefficient of R-22 and R-407C in a horizontal tube.

Comparative study of constitutive relations implemented in RELAP5 and TRACE - Part II: Wall boiling heat transfer

  • Shin, Sung Gil;Lee, Jeong Ik
    • Nuclear Engineering and Technology
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    • 제54권5호
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    • pp.1860-1873
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    • 2022
  • Nuclear thermal-hydraulic system analysis codes have been developed to comprehensively model nuclear reactor systems to evaluate the safety of a nuclear reactor system. For analyzing complex systems with finite computational resources, system codes usually solve simplified fluid equations for coarsely discretized control volumes with one-dimensional assumptions and replace source terms in the governing equations with constitutive relations. Wall boiling heat transfer models are regarded as essential models in nuclear safety evaluation among many constitutive relations. The wall boiling heat transfer models of two widely used nuclear system codes, RELAP5 and TRACE, are analyzed in this study. It is first described how wall heat transfer models are composed in the two codes. By utilizing the same method described in Part 1 paper, heat fluxes from the two codes are compared under the same thermal-hydraulic conditions. The significant factors for the differences are identified as well as at which conditions the non-negligible difference occurs. Steady-state simulations with both codes are also conducted to confirm how the difference in wall heat transfer models impacts the simulation results.

원통형상에서의 표면복사 역해석에 관한 연구 (A Study on the Inverse Analysis of Surface Radiation in a Cylindrical Enclosure)

  • 김기완;백승욱;유홍선
    • 대한기계학회논문집B
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    • 제28권6호
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    • pp.705-712
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    • 2004
  • An inverse boundary analysis of surface radiation in an axisymmetric cylindrical enclosure has been conducted in this study. Net energy exchange method was used to calculate the radiative heat flux on each surface, and a hybrid genetic algorithm was adopted to minimize an objective function, which is expressed by sum of square errors between estimated and measured or desired heat fluxes on the design surface. We have examined the effects of the measurement error as well as the number of measurement points on the estimation accuracy. Furthermore, the effect of a variation in one boundary condition on the other boundary conditions was also investigated to get the same desired heat flux and temperature distribution on the design surface.

액체로켓엔진의 막냉각에 관한 실험적 연구(III) (Experimental Study of Film Cooling in Liquid Rocket Engine(III))

  • 유진;최영환;박희호;고영성;김유
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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    • pp.203-207
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    • 2005
  • 본 연구는 액체산소와 케로신을 추진제로 하는 액체로켓엔진에 막냉각 링을 장착하여 추진제의 혼합비의 변화 및 막냉각제의 종류, 유량 그리고 분사위치에 따라 추력실 길이방향으로 외벽온도를 측정하였다. 연소실험을 위하여 thin wall 연소실과 노즐을 제작하였으며, 측정된 온도를 이용하여 추력실에 발생하는 열유속을 계산하였다.

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국부적인 발열부분을 가진 표면에서의 잠김 비등열전달 -전자부품 액침 냉각에서의 응용- (Boiling Heat Transfer from a locally Heated Surface -A Simulated Electronic Device under Liquid Immersion Cooling-)

  • 하광순;최상민
    • 대한기계학회논문집
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    • 제15권2호
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    • pp.685-692
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    • 1991
  • The pool boiling behavior of a heated surface has been investigated experimentally, focusing on the cases when only a part of the contact surface is heated. Characteristic boiling curves are obtained with circular metal surface test pieces heated below while immersed in Refrigerant-113. Locally heated test pieces are fabricated by inserting a heating block at the center inside a larger conducting block. Overall heat transfer rates are measured while the experimental conditions are systematically varied. The local temperature profiles along the radius are measured for conducting blocks. It is found that the conjugated boiling condition exists and the total heat fluxes should be correlated to a suitably defined temperature difference.

고온용 SiCf/SiC 복합재료개발 기술과 활용방향 (Application and Technology on Development of High Temperature Structure SiCf/SiC Composite Materials)

  • 윤한기;이영주;박이현
    • 대한기계학회논문집A
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    • 제32권11호
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    • pp.1016-1021
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    • 2008
  • The development of the first wall whose major function is to withstand high neutron and heat fluxes is a critical path to fusion power. The materials database and the fabrication technology are being developed for design, construction and safety operation of the fusion reactor. The first wall was designed to consist of the plasma facing armor, the heat sink layer and the supporting plates. and Porous materials are of significant interest due to their wide applications in catalysis, separation, lightweight structural materials. In this study, the characteristics of the sintering process of SiC ceramic, $SiC_f$/SiC composite and porous $C_f$/SiC composite have been introduced order to study of the fusion blanket materials and heat-exchange pannel.

가열 수직 평판과 마주보는 전자모듈의 복사 및 대류 냉각에 대한 실험적 고찰 (Experimental Study on the Radiative and Convective Cooling of Electronic Modules opposed to a Heated Vertical Plate)

  • 최인수
    • 한국산업융합학회 논문집
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    • 제8권2호
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    • pp.105-112
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    • 2005
  • The characteristics of natural convection heat transfer combined with radiation in a vertical parallel plates has been investigated experimentally. The vertical channel is consisted with a heated wall and three protruding heating sources attached on the opposite wall. The cooling of modules has been experimented with heating the wall as well as modules themselves at different aspects ratios and heating fluxes. As the location of module is higher, the temperature becomes higher, but the increasement is smaller. When the aspect ratio is lower than 26, its effect on the temperature is not significant rather than that of the radiation heat transfer. Furthermore, the correlation of Nusselt number with the Rayleigh number are attempted, but additional treatment is needed to accomodate the cases of heating module and/or opposite wall.

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유한요소법을 이용한 Super-ROM 디스크 구조의 열 분포 해석 (Simulations of time dependent temperature distributions of Super-ROM disk structure using finite element method)

  • 안덕원;유천열
    • 정보저장시스템학회논문집
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    • 제1권2호
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    • pp.132-136
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    • 2005
  • It is widely accepted that the reading mechanism of Super-RENS(super-resolution near field structure) and Super-ROM(super-resolution read only memory) is closely related with non-linear temperature dependent material properties such as refractive indices, phase change. Furthermore, the dynamic change of the temperature distribution also an essential part of reading mechanism of Super-RENS/ROM. Therefore, the knowledge of the temperature distribution as a function a time is one of the important keys to reveal the physics of reading mechanism in Super-RENS/ROM. We calculated time-dependent temperature distribution in a 3-dimensional Super-ROM disk structure when moving laser beam is irradiated. With a help of commercial software FEMLAB which employed finite element method, we simulated the temperature distribution of ROM structure whose pit diameter is 120-nm with 50-nm depth. Energy absorption by moving laser irradiation, time variations of heat transfer processes, heat fluxes, heat transfer ratios, and temperature distributions of the complicate 3-dimensional ROM structure have been obtained.

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R407C의 온도구배와 과열도가 증발기 성능에 미치는 영향 (Effects of the Temperature Glide and Superheat of R407C on the Performance of Evaporator)

  • 김창덕;전창덕;이진호
    • 설비공학논문집
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    • 제15권10호
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    • pp.852-859
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    • 2003
  • R407C is considered as an alternative refrigerant of R22 for air conditioners. An experiment was carried out to investigate the characteristics of the evaporation heat transfer and pressure drop for refrigerant R407C flowing in a fin-and-tube heat exchanger used for commercial air-conditioning unit. The experimental data were useful in analyze the effects of the temperature glide and superheat for R407C. Test were conducted at the conditions of inlet refrigerant evaporation temperature of 7$^{\circ}C$, inlet air relative humidity of 50%, and refrigerant mass fluxes varying from 150 to 250 kg/m$^2$s. Representative results show that the heat exchanger performance for R407C evaporation is significantly affected by the change of the flow pattern from two-phase to super-heated vapor flow.