• 한국태양에너지학회 논문집
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• 제36권3호
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• pp.63-74
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• 2016

The nanofluids are the fluids with excellent thermal property, it is expected as a working fluid of the next generation. The nanofluids are well known that if it is used in the boiling heat transfer system, the critical heat flux is enhanced up to 200%, and the thermal conductivity is increased up to from 10 to 160%. However, the fouling phenomenon can be occurred that nanoparticles of nanofluids are deposited on the heat transfer surface. Therefore, to investigate relation between nanofluid and fouling, this study is carried out using oxidized graphene nanofluid. Also it compared and analyzed the critical heat flux and the boiling heat transfer coefficient. As the result, in case of oxidized graphene deposition for fouling, the critical heat flux is increased up to 20% more than oxdized graphene nanofluid. However, the boiling heat transfer coefficient is decreased down to about $6kW/m^2K$ at $1,000kW/m^2$ more than pure water.

• 대한기계학회논문집
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• 제14권5호
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• pp.1282-1289
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• 1990

본 연구에서는 원관내에서 동적으로 완전히 발달한 난류맥동유동에서 관벽에 서 균일한 열유속이 주어지는 경우에 대하여 난류모델로서 K-.epsilon. 2방정식 모델을 적용 하여 수학적인 모델을 세운 후 이를 수치적으로 해석하였다. 그 결과 시간평균 레이 놀즈수가 10000인 경우에 대하여 Strouhal수가 0.0005에서 0.05 그리고 맥동속도진폭 이 0.8이하인 맥동류에 대한 열전달 특성을 제시하였다.

• 광물과산업
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• 제29권
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• pp.56-66
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• 2016

열수변질대가 폭넓게 분포하고 있는 우리나라에서 자연사면이나 인공사면에서 열수변질대 내에 산출되는 점토맥이 산사태 발생에 중요한 역할을 할 수 있다. 점토맥이 존재하는 지반에 지표수가 침투되면 점토광물의 팽윤성 때문에 국지적으로 간극수압이 급격히 상승할 수 있다. 간극수압의 상승으로 세립의 점토광물이 침식될 수 있다. 침식된 점토광물은 수두가 큰 곳에서 작은 곳으로 유동하면서 동수경사가 작은 부분에서 유속이 느려져 퇴적된다. 점토광물이 퇴적된 곳에서 국지적인 간극수압의 증가로 인한 지하수의 유출이 사면파괴를 일으킬 수 있다. 이에 본고에서는 열수변질 점토맥과 산사태와 관련한 국내외 자료를 소개하고자 한다.

• Journal of Advanced Marine Engineering and Technology
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• 제26권2호
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• pp.209-218
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• 2002

The temperature field of a counterflow non-premixed flame is investigated using thermocouples of two sizes. A thermal balance is performed on the thermocouple in order to calculate the magnitude of the radiation corrections involved. Both the thermocouple wire and bead are separately considered to be the relevant thermal surface to which convective heat transfer takes place, and from which radiation lasses occur. The flame is also simulated by using a detailed chemical kinetic mechanism in a previously developed computer code. The local thermo-physical properties of the gas mixture, required to calculate the corrections, are determined both from the simulation, and by approximating the properties of the mixture as those of molecular nitrogen at the measured temperatures. It is concluded that the thermocouple wire is the appropriate thermal surface to which radiation corrections apply, in the absence of information about the gas mixture, its properties can be reasonably approximated by those of nitrogen rm ($N_2$), and the radiation corrections are very sensitive to misalignments in the temperature and velocity fields.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 춘계학술대회
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• pp.2094-2099
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• 2004

An experimental study on heat transfer characteristics near the critical pressure has been performed with an internally-heated vertical annular channel cooled by R-134a fluid. Two series of tests have been completed: (a) steady-state critical heat flux (CHF) and (b) heat transfer tests for pressure reduction transients through the critical pressure. In the present experimental range, the steady-state CHF decreases with the increase of the system pressure For a fixed inlet mass flux and subcooling, the CHF falls sharply at about 3.8 MPa and shows a trend toward converging to zero as the pressure approaches the critical point of 4.059 MPa. The CHF phenomenon near the critical pressure does not lead to an abrupt temperature rise of the heated wall because the CHF occurred at remarkably low power levels. In the pressure reduction transient experiments, as soon as the pressure passed through the critical pressure, the wall temperatures rise rapidly up to a very high value due to the occurrence of the departure from nucleate boiling. The wall temperature reaches a maximum at the saturation point of the outlet temperature, then tends to decrease gradually.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 춘계학술대회
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• pp.531-536
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• 2004

In-arm type hydropeumatic suspension unit(ISU) is an equipment of armed tracked vehicle to absorb impact load and vibration from the irregular ground. During the operation of ISU, main piston moves forward and backward and oil flowing through damper transmits the external impact load to floating piston. Heat is generated in ISU by the oil pressure drop through the damper orifice and the friction between cylinder wall and two pistons. On the other hand, internal heat dissipatis outside via heat convection. Occurrence of high temperature can deteriorate durability of major components and basic function of ISU. And, it can cause fatal problem in the ISU life time and the sealing performance of piston rings. As well, the spring constant change of nitrogen gas that is caused by the temperature rise exerts the negative effect to the vehicle stability. Therefore, in this paper, we analyze the heat transfer analysis of the entire ISU unit, by finite element method, with the outside flow velocities 8m/s and 10m/s.

• 설비공학논문집
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• 제10권3호
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• pp.282-291
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• 1998

Heat transfer performance are studied for the turbulent flow of water in 3 smooth tube coils having ratios of coil to tube diameter of 16, 21 and 27, and a corrugated-coiled tube having a ratio of coil to tube diameter of 29, for Reynolds numbers from 8000 to 60000 and is also compared with the limited results available to data. The experiments are carried out for the fully developed turbulent flow of water in tube coils under the condition of uniform heat flux. This work is limited 0 tube coils of R/a between 10 and 30. The tube having a ratio of coil to tube diameter of 27 among the 3 smooth tube coils shows the best heat transfer performance. The performance of coiled tube best transfer performance. The performance of coiled tube with a similar curvature ratio is better for a corrugated-coiled tube(R/a=17) than for a smooth coiled tube(R/a=16). An empirical relation which correlates most of the data within $\pm$25% was also developed. Test result shows that the Nusselt number is found to be affected by a secondary flow due to curvature.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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• pp.150-155
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• 2010

액체로켓 분사기는 추진 성능과 연소 안정성, 그리고 열유속 특성을 지배하는 가장 중요한 요소이다. 그러나 분사기 근방에서 일어나는 고압 연소 현상에 대한 근본적인 이해의 부족으로 분사기의 개발 과정은 대부분 경험적 설계방법과 고비용의 연소시험에 의존해 왔다. 본 연구는 액체로켓 연소 모델링과 관련된 최근 연구 동향들을 토대로 시작되었다. 층류화염편 기반의 난류연소모델을 초임계 압력 조건에서 나타나는 실제유체 거동을 고려할 수 있도록 확장하였으며, 극저온 질소분사, 상압 조건하의 난류제트화염, 그리고 고압의 기체수소/액체산소 동축 분사기에 적용하여 해석모델의 효용성을 확인하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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• pp.54-58
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• 2017

연소불안정은 로켓엔진과 가스터빈을 포함하는 연소장치의 개발에 있어서 가장 심각한 문제 중의 하나이다. 특히, 연소실에서의 연소와 음향섭동과의 공진에 의해 야기되는 고주파 연소불안정은 하드웨어에 심각한 손상을 초래한다. 왜냐하면 고주파 연소불안정은 높은 압력섭동과 연소실 벽면으로의 과도한 열유속을 동반하기 때문이다. 따라서 연소불안정은 액체로켓엔진 개발에 있어서 반드시 해결되어야 하는 문제 중의 하나이다. 본 논문에서는 액체추진과학로켓(KSR-III) 및 한국형발사체(KSLV-II) 엔진 연소기 개발에 있어서 연소불안정의 경험 사례를 소개한다.

• 설비공학논문집
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• 제11권6호
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• pp.835-845
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• 1999

The objective of the present study was to investigate heat and mass transfer characteristics in a vertical falling film type absorber using LiBr-$H_2O$ solution with 6owt%. The experimental apparatus consisted of an absorber with inner diameter of 17.2 mm and length of 1150mm, a generator, an evaporator/condenser, a solution tank, a sampling trap etc. The parameters were solution temperature of 45 and $50^{\circ}C$, coolant temperature of 30 and $35^{\circ}C$, and film Reynolds numbers from 50 to 150. Pressure drop in the absorber increased as solution and coolant temperatures decreased. Pressure drop in the absorber increased up to the film Reynolds number of 90, and then decreased at the further increase of the Reynolds number above 90. The maximum absorption mass flux observed at the film Reynolds number of 90. Absorption mass flukes increased as coolant temperature decreased. Absorption mass fluxes and heat transfer coefficients under subcooled condition were larger than those under superheated condition. Heat transfer coefficients were affected by solution temperature more than coolant temperature. The maximum absorption effectiveness under the subcooled condition was 23% for coolant temperature of $30^{\circ}C$ and 31% for coolant temperature of $35^{\circ}C$ under the present experimental conditions.