• 한국산업융합학회 논문집
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• 제22권2호
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• pp.173-181
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• 2019

This study was carried out numerically to investigate the flow characteristics in the Venturi tube with $90^{\circ}$ T-branch tube and the inflow of condensed water into the Venturi tube from the branch tube. In this study, the diameter of the branch tube(1, 2, 3mm) and the neck diameter of the Venturi tube(0.3, 0.9, 1.5mm) were varied. The flow rate of the water at the Venturi tube inlet is 80cc/min and the water temperature is 288K. The condensed water temperature at the branch tube inlet is 355K. It was found that the velocity and pressure of the fluid near the branch point in the Venturi tube were more dependent on the diameter of the Venturi tube than the diameter of the branch tube. The temperature of the mixed water at the exit of the Venturi tube was the highest when the Venturi tube's neck diameter is 0.9mm and the branch tube diameter is 2mm. This means that the condensed water is flowing well through the branch tube.

• Advances in materials Research
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• 제8권1호
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• pp.11-24
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• 2019

This paper presents a review study for energy-efficient gas turbines (GTs) with cycles which contributes significantly towards sustainable usage. Nonetheless, these progressive engines, operative at turbine inlet temperatures as high as $1600^{\circ}C$, require the employment of highly creep resistant materials for use in hotter section components of gas turbines like combustion chamber and blades. However, the gas turbine obtain its driving power by utilizing the energy of treated gases and air which is at piercing temperature and pushing by expanding through the several rings of steady and vibratory blades. Since the turbine blades works at very high temperature and pressure, high stress concentration are observed on the blades. With the increasing demand of service, to provide adequate efficiency and power within the optimized level, turbine blades are to be made of those materials which can withstand high thermal and working load condition for longer cycle time. This paper depicts the recent developments in the field of implementing the best suited materials for the GTs, selection of proper Thermal Barrier Coating (TBC), fracture analysis and experiments on failed or used turbine blades and several other designing and operating factors which are effecting the blade life and efficiency. It is revealed that Nickel based Superalloys were promising, Cast Iron with Zirconium and Pt-Al coatings are used as best TBC material, material defects are the foremost and prominent reason for blade failure.

• 한국기계가공학회지
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• 제18권6호
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• pp.55-61
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• 2019

The purpose of this study was to numerically analyze the heat flow characteristics of an automotive radiator. Heat flow analyses were conducted on the cooling water and outdoor air of the radiator, as well as the temperature distribution of the cooling water after heat transfer. The results of the study revealed that neither heat transfer nor radiator volume was affected by the position of the inlet of cooling water. However, temperature distribution was affected by the position of both the inlet and outlet. In case of heat transfer, three models underwent about 158 kW of heat transfer. The difference in cooling water temperature was about $10^{\circ}C$. In case of pressure drop, the core external air side was reduced to about 1,375 Pa, and the internal cooling water side about 14,570 Pa.

• 한국수소및신에너지학회논문집
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• 제34권2호
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• pp.196-204
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• 2023

This study performed the numerical analysis of the internal flow phenomena of 1 kWe-class solid oxide fuel cell (SOFC) stacks with internal manifold type and planar cells using commercial computational fluid dynamics (CFD) software, Star-CCM+. In particular, the locations where the turbulent phenomena occur inside the SOFC stack were investigated. In addition, the laminar flow model and the standard k-ε turbulent model were used to calculate the SOFC stack, separately. And, the calculation results of both laminar and turbulent models were compared. The calculation results showed that turbulent phenomena occurred mainly in the cathode flow. Especially, the turbulent phenomena were found in the cathode inlet/outlet region, and local turbulence occurred in the end plate near the inlet pipe.

• 한국추진공학회지
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• 제9권3호
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• pp.25-37
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• 2005

터보펌프 공급방식 발사체 추진기관은 공급 시작 시점에서부터 종료되는 시점까지 산화제 터보펌프 입구에서의 온도 요구조건을 충족시켜야 한다. 이러한 조건이 만족되지 못할 경우 터보펌프 입구에서 캐비테이션이 발생하여 펌핑(pumping) 성능이 저하되고, 심한 경우 펌프의 손상을 초래할 수 있다. 따라서 극저온 액체산소를 사용하는 액체로켓 추진기관에서는 액체산소의 온도 상승에 대한 적확한 예측이 필수적이다 본 논문에서는 탱크 내의 액체산소 온도상승과 관계된 탱크 내 해석 방법을 체계적으로 제시하였고, 부력동기 경계층 이론을 적용하여 터보펌프 공급방식 로켓 추진기관의 충전, 대기, 선가압, 비행 등의 전 과정을 통하여 탱크에 충전된 액체산소의 온도상승을 예측할 수 있는 모델을 제시 하였다.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2008년도 동계학술발표대회 논문집
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• pp.227-232
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• 2008

The present study was investigated the local heat transfer characteristics and temperature distribution on the louver fin by using the expansion model. Heat transfer rate, frost mass and temperature distribution of the louver fin under frosting condition were experimentally investigated. Local heat transfer rate and heat flux on the louver were analyzed by the conduction heat transfer between top and lower part of the louver. The experimental key parameter was brine inlet temperature(-5, -10, $-15^{\circ}C$). The heat transfer performance and frost mass at brine temperature of $-15^{\circ}C$ were increased by maximum 3 time than the brine temperature of $-5^{\circ}C$. At all experimental case, local heat transfer rate and heat flux of the louver were almost symmetry at the louver number of 6. Especially, local heat transfer rate and heat flux were maximum increased on the louver number of 4 and 8.

• 한국기계기술학회지
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• 제13권2호
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• pp.55-61
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• 2011

This study analyzed on the characteristics of temperature distribution in an active regeneration DPF using computer simulation. In order to verify the boundary condition of analysis, results of temperature distribution in DPF are compared between experimental and computer simulation. Using this boundary condition, temperature distribution and filter's durability in DPF analyzed according to various operating conditions. The results of computational analysis are agreed well with experimental ones from the tendency of temperature distribution of axis and radius direction. The temperature increases and the axial temperature gradients in DPF according to velocity of exhaust gas are lowered as the high velocity of exhaust gas. But the temperature gradients of radius direction at exit side in DPF are grown as the high velocity of exhaust gas. The results according to inlet temperature of exhaust gas show that the increase ratios of temperature in DPF are grown as the high temperature of exhaust gas.

• 대한기계학회논문집B
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• 제38권5호
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• pp.389-397
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• 2014

흡수식 냉온수기는 자연에 있는 냉매를 사용함으로 인해 환경오염이 매우 적어 친환경적이다. 흡수식 냉온수기에서 고효율의 배기가스용 고온재생기는 높은 시스템 성능을 얻기 위한 중요한 요소중에 하나이다. 따라서, 본 연구에서는 운전조건에 따른 흡수식 냉온수기의 배기가스용 고온재생기의 성능을 파악하기 위해 실험장치를 제작하고 실험을 실시하였다. 배기가스용 고온재생기에서 흡수액의 입구상태는 성능변화에 매우 큰 영향을 줌으로 여러 가지 흡수액 농도 조건에서 공기측 입구온도와 질량유량을 변화시켜가면서 고온재생기의 성능을 고찰하였다. 실험결과, 공기측 질량유량비가 80%에서 120%로 증가할 때 흡수액 농도가 56%, 55%, 54%, 53%에서의 열교환량은 각각 30%, 33%, 34%, 37% 정도 증가하였다. 또한 고온재생기의 흡수액 입구농도가 56%, 55%, 54%, 53% 일 때 공기측 입구온도가 $170^{\circ}C$에서 $210^{\circ}C$로 증가함에 따라 고온재생기의 열교환량은 각각 140%, 160%, 220%, 224% 정도 증가하였다.

• 한국터널지하공간학회 논문집
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• 제6권1호
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• pp.51-59
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• 2004

본 연구에서는 3차원 전산유체역학 기법을 이용하여 열차터널 내 10MW급 화재발생 시, 대피환경에 대한 1차원 임계속도의 유효성을 평가하였다. 또한 터널의 입구속도가 1m/s, 2m/s (임계속도) 그리고 3m/s일 때의 터널 내 기류분포, 온도분포, 가시거리분포 및 오염물질분포가 대피환경에 미치는 영향을 각각 검토하였다. 그 결과, 세 가지 경우모두, 승객의 안전한 대피환경을 충분하게 제공하지 못할 것으로 예상되어 승객들은 유동방향 하류로 대피하여야 한다. 그러나 3m/s 입구속도의 경우는 1m/s, 2m/s의 경우 보다 승객의 대피환경에 있어서 좀 더 나은 결과를 보인다. 따라서 터널의 방재시스템의 설계 시, 안전한 대피환경을 확보하기 위해서는 임계속도보다 큰 입구속도의 시용이 요구된다.

• 한국분무공학회지
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• 제8권2호
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• pp.1-6
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• 2003

The liquid phase LPG injection (LPLI) system (the third generation technology) has been considered as one of the next generation fuel supply systems for LPG vehicles, since it has a very strong potential to accomplish the higher power, higher efficiency, and lower emission characteristics than the mixer type(the second generation technology) fuel supply system However. when a liquid LPG fuel is injected into the inlet duct of an engine, a large quantity of heat is extracted due to evaporation of fuel. This leads to freezing of the moisture in the air around the outlet of a nozzle, which is called icing phenomenon. It may cause damage to the outlet nozzle of an injector or inlet valve seat. In this work, the experimental investigation of the icing phenomenon was carried out The results showed that the icing phenomenon and process were mainly affected by humidity of inlet air instead of air temperature in the inlet duel. Also, it was observed that the total ice formed around the nozzle weighs at about $150mg{\sim}260mg$ after injection for ten minutes. And some fuel species were found in the ice attached at the front side of a nozzle, while frozen ice attached at the back of a nozzle was mostly' consisted of moisture of inlet air. Therefore, some frozen ice deposit. detached from front nozzle of an injector, may cause a problem of unfavorable air fuel ratio control in the small LPLI engine.