• 제목/요약/키워드: transient heat transfer

검색결과 431건 처리시간 0.024초

정상상태 방법을 이용한 나노유체의 열전도율 측정 (Measuring Thermal Conductivity of Nanofluids by Steady State Method)

  • 이신표
    • 대한기계학회논문집B
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    • 제30권9호
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    • pp.898-904
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    • 2006
  • A new method measuring thermal conductivity of fluids is proposed in this research. It is based on the steady state heat transfer from a hot central cylinder to a cold outer cylinder located concentrically. This method guarantees more stable measurement than conventional THM(transient hot-wire method) due to its simplicity of theoretical principle. Measurements was made for the three nanofluid samples with different particle concentration of pure, 2% and 4%. Nanofluids are made by mixing the pure transformer oil with AlN nano particles. Design of the sensor module and experimental procedures are explained and comparison of the measuring data between present method and THM was made in detail.

Numerical Prediction of Aviation Fuel Temperatures in Unmanned Air Vehicles

  • Baek, Nak-Gon;Lim, Jin-Shik
    • International Journal of Aeronautical and Space Sciences
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    • 제12권4호
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    • pp.379-384
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    • 2011
  • This paper performs numerical prediction of fuel temperature in the fuel tanks of unmanned air vehicles for both ground static non-operating and in flight transient conditions. The calculation is carried out using a modified Dufort-Frankel scheme. For this calculation, it is assumed that a non-operating vehicle on the ground is subjected to repeating daily cycles of ambient temperature with solar radiation and wind under 1%, with a 20% probability of hot day conditions. The energy conservation equation is used as the governing equation to calculate heat transfer between the fuel tank surface and the ambient environment. Results of the present analysis may be used as the estimated initial values of fuel temperatures in a vehicle's fuel tank for the purpose of analyzing transient fuel temperatures during various flight missions. This research also demonstrates that the fuel temperature of the front tank is higher than that of the rear tank, and that the difference between the two temperatures increases in the later phases of flight due to the consumption of fuel.

Von-Kármán 회전 유동 하에서의 물의 결빙 (Freezing of Water in Von-Kármán Swirling Flow)

  • 유주식
    • 설비공학논문집
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    • 제8권3호
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    • pp.413-422
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    • 1996
  • Freezing of water in von-$K{\acute{a}}rm{\acute{a}}n$ swirling flow is considered. The transient behavior of the temperature distribution in both solid and liquid phases and freezing rate are determined. The fluid flow induced by the rotation of solid strongly inhibits the freezing process. The thickness of frozen layer is inversely proportional to the square root of the angular velocity of solid. As the angular velocity or initial liquid temperature becomes larger, the freezing process is more strongly inhibited by the fluid flow. When phase change is present, the transient heat transfer rate is greater than the case with no phase change.

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PWR 가압기에서 오동작 보조살수 과도시 용기벽의 열적 과도응답 (Thermal Transient Response of a PWR Pressurizer Vessel Wall for the Inadvertent Auxiliary Spray Transient)

  • Jo, Jong-Chull;Lee, Sang-Kyoon;Shin, Won-Ky;Cho, Jin-Ho
    • Nuclear Engineering and Technology
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    • 제23권2호
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    • pp.183-199
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    • 1991
  • 가압수형 원자로 가압기의 오동작 보조살수 과도시 용기벽에서의 온도분포에 대한 과도응답을 해석하였으며, 해석은 분무수적으로 젖게되는 용기벽면에서 나타나는 열응력에 대하여 보수적으로 수행되었다. 수적이 부딪혀서 흘러내리는 용기벽의 내부경계면에서 강제대류열전달계수를 결정하기 위하여, 분무수적들이 살수노즐을 떠나 수증기와 비응축성인 수소기체로 이루어진 혼합기로 채워져 있는 가압기 내부공간을 통하여 비행한 후에 용기내부벽면에 도달할 때의 수적들의 과도온도를 예측하였다. 용기벽에서의 과도온도분포는 유한요소법을 사용하여 구하였으며, 대표적인 결과들을 제시하였다. 열해석의 결과는 입력자료에 대한 묘사와 부합되며, 타당한 물리적 의미를 가짐 이 확인되었다.

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THERMAL AND STRUCTURAL ANALYSIS OF CALANDRIA VESSEL OF A PHWR DURING A SEVERE ACCIDENT

  • Kulkarni, P.P.;Prasad, S.V.;Nayak, A.K.;Vijayan, P.K.
    • Nuclear Engineering and Technology
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    • 제45권4호
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    • pp.469-476
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    • 2013
  • In a postulated severe core damage accident in a PHWR, multiple failures of core cooling systems may lead to the collapse of pressure tubes and calandria tubes, which may ultimately relocate inside the calandria vessel forming a terminal debris bed. The debris bed, which may reach high temperatures due to the decay heat, is cooled by the moderator in the calandria. With time, the moderator is evaporated and after some time, a hot dry debris bed is formed. The debris bed transfers heat to the calandria vault water which acts as the ultimate heat sink. However, the questions remain: how long would the vault water be an ultimate heat sink, and what would be the failure mode of the calandria vessel if the heat sink capability of the reactor vault water is lost? In the present study, a numerical analysis is performed to evaluate the thermal loads and the stresses in the calandria vessel following the above accident scenario. The heat transfer from the molten corium pool to the surrounding is assumed to be by a combination of radiation, conduction, and convection from the calandria vessel wall to the vault water. From the temperature distribution in the vessel wall, the transient thermal loads have been evaluated. The strain rate and the vessel failure have been evaluated for the above scenario.

새로운 응축열전달계수 상관식이 적용된 MARS-KS를 활용한 원자로건물 피동냉각계통 열제거 성능의 수치적 연구 (Numerical Study of the Heat Removal Performance for a Passive Containment Cooling System using MARS-KS with a New Empirical Correlation of Steam Condensation)

  • 장영준;이연건;김신;임상규
    • 에너지공학
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    • 제27권4호
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    • pp.27-35
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    • 2018
  • 피동원자로건물냉각계통(PCCS)은 사고 발생 시 원자로건물로 방출된 열을 제거하여 원전의 건전성을 보장하기 위해 설계되었다. PCCS의 열제거 성능은 증기-공기 혼합물의 응축열전달에 의해 결정된다. 본 연구에서는 응축열전달계수의 예측 정확도를 향상시키기 위해 새로운 상관식을 이식한 MARS-KS 코드를 사용하여 PCCS의 열제거 성능을 평가하였다. MARS-KS 코드에 사용된 새로운 상관식은 압력, 벽면과냉도, 비응축성 기체 질량분율 및 응축튜브의 종횡비와 같은 열전달계수에 영향을 미치는 변수들을 이용하여 개발하였고, 이는 MARS-KS코드의 기본 응축 모델인 Colburn-Hougen 모델을 대체하여 적용되었다. 대형파단 냉각재상실사고 발생 시 PCCS의 운전에 따른 다양한 열수력학적 변수들을 분석하였고, 열제거 성능 평가를 위해 새로운 상관식이 적용된 MARS-KS 코드의 원자로건물 압력거동 계산결과와 기존의 응축모델을 이용한 해석결과를 비교하였다.

화재 및 화재 후 냉각상태의 철근콘크리트 부재 수치해석 (A Numerical Model of Reinforced Concrete Members Exposed to Fire and After-Cooling Analysis)

  • 황주영;곽효경
    • 한국전산구조공학회논문집
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    • 제28권1호
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    • pp.101-113
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    • 2015
  • 이 논문은 화재에 노출된 철근콘크리트 구조에 대한 수치해석 모델을 제시하고, 기존의 자료 및 설계 규준과의 비교를 통해 구조물의 설계 시 고려 사항에 대해 제안하고 있다. 수치해석은 비정상 열전달 해석과 비선형 구조해석의 두 단계로 수행되며, 비정상 열전달 해석을 통해서 얻어진 화재시간에 따른 단면 온도분포를 바탕으로 비선형 구조해석하여 부재의 상태에 대한 정보를 얻게 된다. 이때, 철근콘크리트의 재료모델을 화재진행상태(Under-Fire)와 화재종료 후 냉각상태(After-Cooling)로 나뉘어 해석수행하여 각각의 재료상태에 따른 거동의 변화를 살펴본다. 해석된 결과는 여러 구조물에 대해 기존의 실험결과와 비교하여 검증하고, 설계 규준과의 비교를 통해 화재 시 구조물의 안전성에 대해 고찰하였다.

오목한 표면위에 분사되는 경사충돌제트에 대한 국소열전달계수의 측정 (Local heat transfer measurement from a concave surface to an oblique impinging jet)

  • 임경빈;김학주
    • 설비공학논문집
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    • 제10권3호
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    • pp.324-333
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    • 1998
  • Measurements of the local heat transfer coefficients on a hemispherically concave surface with a round oblique impinging jet were made. The liquid crystal transient method was used for these measurements. This method, which is a variation of the transient method, suddenly exposes a preheated wall to an impinging jet while video recording the response of liquid crystal for the surface temperature measurements. The Reynolds number used was 23,000 and the nozzle -to -jet distance was L/d=2, 4, 6, 8 and 10 and the jet angle was $\alpha$=0$^{\circ}$, 15$^{\circ}$, 30$^{\circ}$and 40$^{\circ}$. In the experiment, the maximum Nusselt number at all region occurred at L/d(equation omitted)6 and Nusselt number decreases as the inclined jet angle increases. For the normal jet the contours of constant Nusselt number are circular and as the jet is inclined closer and closer to the surface the contours become elliptical shape. The decreasing rate of the Nusselt number at X/d> 0(upstream) on a surface curvature are higher than those on a flate plate and the decreasing rate of the Nusselt number at X/d <0(downstream) on a surface curvature are lower than those on a flate plate. And also, the decreasing rate of local Nusselt number distribution at X/d <0(upstream) exhibit lower than with X/d <0(downstream) as jet angle increases. The second maximum Nusselt number occurred at long distance from stagnation point as jet angle increases.

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소듐 분위기에서 물누출에 의한 5Cr-1Mo Ferrite강 구멍의 막힘과 재개방 현상 (Plugging and Re-opening Phenomena of the 5Cr-1Mo Steel Leak Hole by Water Leakage in Sodium Atmosphere)

  • 정경채;김태준;최종현;박진호;황성태
    • 공업화학
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    • 제9권5호
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    • pp.674-679
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    • 1998
  • 액체금속로 증기발생기 전열관 재질로 사용이 예상되는 ferrite steel 시편을 사용해서 소듐분위기에서 미량의 물 누출 실험을 수행하였다. 누출경로는 소듐-물 반응생성물 및 부식생성물에 의한 self-plugging 현상과 열적인 transient 및 전열관의 vibration에 의한 re-opening 메카니즘으로 설명이 가능하였다. 실험결과, 600 Psig의 injection 압력으로 5 g $H_2O$를 소듐분위기 속의 시편으로 누출시킨 경우, 누출초기와 약 70분 경과 후에 약간의 누출 흔적이 보였으나, self-plugging되었던 누출경로는 129분이 경과되자 완전 re-opening된 것으로 확인되었다. 누출시편의 re-opening shape은 2중으로 되어 있었으며, 소듐부위에서 시편 표면에 나타난 re-opening size 약 2 mm의 직경을 나타내었다.

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Yeast 2 $\mu$m 플라스미드 유래 FLP recombinase 유전자의 곤충 배양세포내 발현 (Expression of the FLP recombinase of the 2 $\mu$m plasmid of yeast in the cultured cells of Bombyx mori using a transient expression vector)

  • 강석우;윤은영
    • 한국잠사곤충학회지
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    • 제39권1호
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    • pp.36-43
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    • 1997
  • In order to express the FLP recombinase in B. mori cultured cell line, BmN-4, transient expression system using a heat shock protein gene (hsp70) promoter of Dorosophilla melnogaster was constructed. This vector was designated as pHsSV. Activity strength of the hsp70 promoter was compared with that of immediate early gene (IE-1) and polyhedrin gene of BmNPV employing the E. coli $\beta$-galactosidase gene as a reporter gene. The result showed that the pHs $\beta$-gal plasmid vector expressed the $\beta$-galactosidase at 2nd and 3rd day after the transfer of plasmid DNA into BmN-4 cells, which was similar to that of pIE1 $\beta$-gal vector, but different from that of a recombinant virus, vBm $\beta$-gal. For the construction of FLP recombinase transient expression vector, the FLP recombinase gene was cloned by polymerase chain reaction technique. To express the FLP recombinase, this gene was inserted into pHsSV plasmid vector, under the control of the hsp70 promotor, and tranfected in BmN-4 cells. The expressed FLP recombinase was estimated at 44kDa on a 12.5% SDS-PAGE.

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