• 상하수도학회지
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• 제25권4호
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• pp.503-510
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• 2011

Ammonia in water which is toxic to human, its concentration is regulated below 0.5 mg/L in drinking water. Current study aimed to develop appropriate models for ammonia stripping using hollow fiber membrane contactor. Two different models were developed during the study. Model 1 was assumed only free ammonia ($NH_3$) transfer in stripping process, whereas the Model 2 was assumed with total ammonia ($NH_3+{NH_4}^+$) transfer. Ammonium chloride ($NH_4CI$), sodium hydroxide(NaOH) were used to make ammonia solution, which was concentration of 25 mg as N/L at a pH of 10.5. The experimental conditions were such that, the liquid flow was in tube-side in upward direction and t he gas flow was on shell-side in downward direction a t room temperature. The experimental and modeling results showed that marginal difference were observed at low gas flux. However the difference between the both models and experimental value were increased when the gas flux was increased. The study concludes that the Model 1 with free ammonia is more appropriate when both models were compared and useful in ammonia stripping process at low gas flux.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 춘계학술대회
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• pp.2070-2075
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• 2004

Performance of a solid oxide fuel cell (SOFC) can be enhanced by converting thermal energy of its high temperature exhaust gas to mechanical power using a micro gas turbine (MGT). A MGT plays also an important role to pressurize and warm up inlet gas streams of the SOFC. In this study, the influence of performance characteristics of the tubular SOFC on the hybrid power system is discussed. For this purpose, detailed heat and mass transfer with reforming and electrochemical reactions in the SOFC are mathematically modeled, and their results are reflected to the performance analysis. The analysis target is 220kWe SOFC/MGT hybrid system based on the tubular SOFC developed by Siemens-Westinghouse. Special attention is paid to the ohmic losses in the tubular SOFC counting not only current flow in radial direction, but also current flow in circumferential direction through the anode and cathode.

• 전기화학회지
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• 제8권4호
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• pp.155-161
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• 2005

상용 CFD 프로그램인 FLUENT v5.3을 이용하여 용융탄산염 연료전지 스택의 수치 모사를 행하였다. FLUENT에 포함되어 있는 보존식들을 이용하면서, 사용자 정의함수를 이용하여 포함시킨 코드를 통해 전기화학적 반응과 부반응인 수성가스전이반응에 의한 질량과 가스 조성 변화 및 열이동을 고려하여 정확한 계산 결과를 얻고자 하였다. 모사에 사용된 스택은 6kW급과 25kW급 스택으로 각각 20개와 40개의 단위전지를 수직으로 적층한 형태이며 스택내로 주입되는 가스는 coflow형태로 각각의 채널을 흘러가게 설계되어 있다. 모사를 통해 알아본 스택 내 압력분포는 가스 흐름방향으로 압력강하가 일어나며 anode 채널보다 cathode 채널에서의 압력차가 더 크게 나타났다. 채널 내 속도분포는 전극 반응에 의한 질량 및 부피변화로 인해 anode 채널에서는 가스흐름 방향으로 속도가 증가하는 반면 cathode 채널에서는 속도가 감소하는 경향을 보였다. 스택 내 온도분포는 가스 흐름방향으로 증가하는 경향을 보였고, 계산결과와 실험결과가 대체로 일치함을 확인할 수 있었다. 수성가스전이반응을 포함한 모델과 그렇지 않은 모델을 비교한 결과 가스의 주입구 부분에서는 수성가스전이반응에 의해 흡열 반응이, 출구 부분에서는 발열반응이 일어나고, 이로 인해 입구와 출구의 온도차가 더 커짐을 확인하였다. 따라서 상용화 스택인 수백 kW급 이상의 대형 스택을 모사하기 위해서는 수성가스전이반응을 고려해야할 것으로 생각된다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.1084-1089
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• 2000

The basic equations are derived for the analysis of a stepped labyrinth gas seal which are generally used in high performance compressors, gas turbines, and steam turbines. The Bulk-flow is assumed for a single cavity control volume and the flow is assumed to be completely turbulent in circumferential direction. Moody's wall-friction-factor formula is used for the calculation of wall shear stresses in the single cavity control volume. For the reaction force developed by the seal, linearized zeroth-order and first-order perturbation equations are developed for small motion about a centered position. Integration of the resultant first-order pressure distribution along and around the seal defines the rotordynamic coefficients of the stepped labyrinth gas seal. The leakage and rotordynamic characteristic results of the stepped labyrinth gas seal are presented and compared with Scharrer's theoretical analysis using Blasius' wall-friction-factor formula.

• Tribology and Lubricants
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• 제18권1호
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• pp.24-33
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• 2002

The basic equations are derived for the analysis of a staggered labyrinth gas seal which are generally used in high performance compressors and steam turbines. The Bulk-flow is assumed for a single cavity control volume and the flow is assumed to be completely turbulent in circumferential direction. Moody's wall-friction-factor formula is used for the calculation of wall shear stresses in the single cavity control volume. For the reaction force developed by the seal, linearized zeroth-order and first-order perturbation equations are developed for small motion about a centered position. Integration of the resultant first-order pressure distribution along and around the seal defines the rotordynamic coefficients of the staggered labyrinth gas seal. Theoretical results of leakage and rotordynamic characteristics for the staggered labyrinth gas seal are compared with those of the plain seal and see-through labyrinth seal.

• 한국가스학회지
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• 제22권3호
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• pp.7-12
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• 2018

화석연료를 연소할 때 연소로 내의 고온의 온도 분위기에서 열적 질소산화물이 발생하게 된다. 연소기기에서 질소산화물을 저감하기 위한 여러 가지 방법 중에 배기가스 재순환 방법이 널리 쓰이고 있다. 본 연구에서는 배기가스 재순환 배관에 코안다 노즐을 사용하고 양쪽 출구가 트인 재순환하는 버너에 대하여 냉간 유동 특성을 전산유체해석을 통해 살펴보았다. 재순환 배관이 원통 버너의 접선방향으로 설치되어 있어서 버너 내부에서 선회유동이 형성되어 원통 버너 중심 부분에 역류가 생기는 현상을 관찰하였으며 이는 한쪽이 막힌 재순환 버너와 유사한 경향임을 확인 하였다. 본 연구로부터 양쪽 출구가 트인 재순환 버너에서 재순환 유입량은 한쪽이 막힌 버너보다 약 5% 증가하는 것을 확인하였고 양쪽 트인 버너에서 배기가스 재순환 배관의 유입구 위치의 출구에서는 전체 영역에서 유입 유동이 형성되고 반대편의 출구에서는 총 유량은 배출되지만 원통의 가운데 부분은 역류가 일어나는 것을 확인하였다. 배출되는 출구에서 배출되는 유량은 유입되는 출구에서의 유입량보다 3~5배 유량이 크게 나타났다.

• 한국분무공학회지
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• 제26권1호
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• pp.33-39
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• 2021

Y-jet nozzle has a wide fuel flow rate range and turn-down ratio, thus, it is used in industrial boilers, furnace and agricultural atomizer. However, it has asymmetrical spray characteristics due to the nozzle design factors. Therefore, in this study, asymmetric spraying characteristics of the elliptical Y-jet nozzle was studied by using the lab-scale spray apparatus. As a result, the elliptical Y-jet nozzle had lower gas mass flow rate than circular Y-jet nozzle at same gas pressure, because of bigger shear stress due to the wider inner surface at the elliptical Y-jet nozzle. Larger SMD was measured on the elliptical Y-jet nozzle than the circular Y-jet nozzle. When SMD was measured in the X_Axis direction at the same gas mass flow rate, the elliptical Y-jet nozzle with an aspect ratio of 2:1 showed greater asymmetry than the others.

• 한국진공학회:학술대회논문집
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• 한국진공학회 2009년도 제37회 하계학술대회 초록집
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• pp.92-92
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• 2009

• 대한조선학회 특별논문집
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• 대한조선학회 2011년도 특별논문집
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• pp.63-69
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• 2011

Exhaust gases of a vessel from a main engine, a diesel generator and an incinerator contain very harmful substances like soot, $SO_2$ and NOx. Careful design of funnel shape is required to prevent those harmful exhaust gases from influencing on accommodation and a fan room. Meanwhile, the exhaust gases are also hot enough to damage electronic devices like radar. Therefore the funnel design should be considered so that electronic devices are not directly exposed to the exhaust gas in the strong stern wind. This study may propose guidelines of optimum design criterion for the anti-thermal damage design of the electronic devices and anti-recirculating design of harmful exhaust gas near the accommodation. From CFD analyses, we can understand that the major factors affecting the exhaust gas dispersion are the large scale mixing by separation vortices and the sluggish flow in the recirculation region. We hope that the funnel flow analysis around ship's funnel is used for practical optimum funnel design to minimize the exhaust gas dispersion by adjusting the funnel shape, the position of the exhaust pipe, the shape of bulwark, the exhaust direction of air ventilated an engine room and the angle of the exhaust pipe.

• 한국유체기계학회 논문집
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• 제18권5호
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• pp.49-53
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• 2015

Thrust vector control is the method which generates the side force and roll moment by controlling exhausted gas directly in a rocket nozzle. TVC is classified by mechanical and fluid dynamic methods. Mechanical methods can change the flow direction by several objects installed in a rocket nozzle exhaust such as tapered ramp tabs and jet vane. Fluid dynamic methods control the flight direction with the injection of secondary gaseous flows into the rocket nozzle. The tapered ramp tabs of mechanical methods are used in this paper. They installed at the rear in the rocket nozzle could be freely moved along axial and radial direction on the mounting ring to provide the mass flow rate which is injected from the rocket nozzle. TVC of the tapered ramp tabs has the potential to produce both large axial thrust and high lateral force. We have conducted the experimental research and flow analysis of ramp tabs to show the performance and the structural integrity of the TVC. The experiments are carried out with the supersonic cold flow system and the schlieren graph. This paper provides to analyze the location of normal shock wave and distribution of surface pressure on the region enclosed by the tapered ramp tabs.