In this study, numerical analysis was performed for the purpose of analyzing the flow characteristics and performance according to the change in the inflow hydrogen temperature and differential pressure of the receptacle of the hydrogen charging system. The pressure distribution and turbulent kinetic energy in the filter area were analyzed by changing the outlet pressure condition under the inlet hydrogen temperature condition, and the flow velocity change at the outlet was compared and analyzed. As a result of the analysis, as the differential pressure decreased, the flow rate at the outlet of the receptacle decreased by up to about 70% at the 2.86 MPa condition compared to the 1.86 MPa condition, and the mass flow rate decreased by about 56.5% at the maximum. It was found that the standard CV performance was not satisfied when the differential pressure at the inlet and outlet was 1.12 MPa or less under the 363K temperature condition.

In this study, the cooling performance change according to the arrangement of the fin-tube heat exchanger using a single tube and the cooling performance change according to the air flow rate were studied. The arrangement of basic heat exchanger was set to 4 columns and 4 rows, and the performance change was studied while changing the columns and rows. In addition, the performance change was investigated by changing the air flow rate of the basic heat exchanger.

본 연구에서는 80k Bulk carrier의 저항성능 향상을 목적으로 선미부에 1개의 핀을 부착해 선미 유동을 제어하였고, 저항성능 및 반류의 변화를 분석하였다. 부착된 핀은 직사각형 단면을 가지며, 길이와 폭, 두께는 고정된 채 길이 및 흘수 방향 부착 위치와 유선에 대 한 각도만 변화가 있었다. 나선 및 핀이 부착된 선체에 대한 모형 스케일에서의 CFD 해석이 수행되었고, 그 결과를 실선 확장 후 비교하 였다. 핀은 프로펠러로 유입되는 빌지 볼텍스의 경로를 선미 트랜섬 쪽으로 변화시켰고, 이는 프로펠러 상부와 선미부의 압력을 증가시켰 다. 이로 인해 선체의 압력저항 및 전 저항이 감소되었으며, 감소율은 핀의 부착 위치가 선미 및 선저와 가까울수록 높았다. 또한 핀은 공 칭반류를 감소시켰는데 핀의 각도가 커질수록 반류의 변화가 컸고, 전 저항 저감률은 최대가 되는 특정 각도까지만 비례하였다. 대상 선 박에 단일 핀을 부착했을 시의 최대 전 저항 저감률은 약 2.1 %였고, 선미로부터 수선간장의 12.5%, 선저로부터 흘수의 10 % 위치에 14 의 각도로 부착됐을 때이다.

In this study, the flow rate at the drone and the pressure around the drone were investigated by carrying out the flow analysis due to the wing shape of drone. At models 1, 2 and 3, the positions of areas with the maximum flow rate around the drone according to the shape of the wing were seen to be same at the rear wing of drone. Model 2 has the fastest flow rate, followed by model 1 and model 3. At the distribution of flow pressure by model around the drone according to the wing shape of drone, models 1, 2 and 3 had the same highest pressures at the center of drone. In comparison with the maximum pressures of models near the wing shape of the drone, the flow pressure at model 2 was higher compared with models 1 and 3. At the wing shape of the drone, model 2 is considered to carry the flow performance better than models 1 and 3. So, the result of this study is thought to be useful for designing the wing shape of the drone. Without the test of flow performance due to the shape of drone wing, the flow performance can be seen as the flow rate and pressure are investigated through the flow analysis.

In this study, by analyzing the flow rate and the pressure applied to the fan for the flow of air with room temperature into the fan in desktop computer, it was investigated which model was suitable for flow resistance. When comparing the speed distribution of air flow by model according to fan shape, model A was able to confirm that the fan performance was not good but the external flow was widely distributed. And model B was able to know that the performance was good but the external flow was smaller. Model C was found to have good performance and a wide distribution of outer flow. In cases of three models, it was equally shown that the pressure was highest on the blade side of the inlet where the air enters. Model B receives more pressure than models A and C when the same air flow rate is applied, so models A and C are considered more efficient cooling fans than model B. When considering the flow rates and the pressures acting on the model, model C is thought to have relatively good performance. By utilizing this study result, the flow rate and pressure are investigated without flow experiment by the shape of fan in desktop computer, and the flow capacity can be seen.

In this theoretical study, a design and performance analysis theory of a micro flowrate and high pressure air-compressor is developed. The governing equations are from the gas state equation and fluid dynamic theories because the working fluid in the air compressor is in a gas phase. A case study was conducted to design a reciprocating type of air compressor which the target performance was 0.6liter/min in the volume flowrate with 5atg in air pressure at 1,600rpm rotational speed. Geometrical size of the model air compressor designed is 10mm in stroke, 20mm in bore with 4.79 compression ratio. From the performance analysis of the model compressor, it was found that the air volume flowrate produced was 0.6liter/min with 5.81atg in pressure. The design theory of a micro-size high-pressure air compressor developed in this study is expected to be very useful design tools in NANO technology industry.

Polyphenylene sulfide(PPS) is a hydrocarbon polymer which has resistance to heat, chemicals and generality due to its low cost. To produce cationic exchange polymer, PPS was blended with sulfonation process and Polyvinylidenedifluoride(PVdF) was also applied for membrane-flexibility. After production of sulfonated-PPS (sPPS)/PVdf blend membrane, membrane property evaluation is concomitant. Water uptake and Dimensional change were highly enhanced by the incorporation of PVdF in blend membrane. Also stability of sPPS/PVdF blend membrane in VO2+ solution was highly improved. When the amount of PVdF is increasing, however, proton conductivity shows a slightly downward tendency. Consequently, the optimization of PVdF Content in sPPS/PVdf blend membrane is an important factor for the realization of VRFB system.

Recently, reverse osmosis (RO) is the most common process for seawater desalination. A common problem in both RO and thermal processes is the high energy requirements for seawater desalination. The one energy saving method when utilizing the osmotic power is utilizing pressure retarded osmosis (PRO) process. The PRO process can be used to operate hydro turbines for electrical power production or can be used directly to supplement the energy required for RO desalination system. This study was carried out to evaluate the performance of both single-stage PRO process and two-stage PRO process using RO concentrate for a draw solution and RO permeate for a feed solution. The major results, were found that increase of the draw and feed solution flowrate lead to increase of the production of power density and water permeate. Also, comparison between CDCF and CDDF configuration showed that the CDDF was better than CDCF for stable operation of PRO process. In addition, power density of two-stage PRO was lower than the one of single-stage. However, net power of two-stage PRO was higher than the one of single-stage PRO.

In this study, the ventilation of duct is simulated by CFD and thermal changes on the seat surface are measured experimentally. These models are the improved duct and the existing one installed at the real seat in order to test the thermal change 1 minute later. The seat with the existing duct has the temperatures of 26℃ and 25℃ on lumber and femoral parts respectively. However, the seat with the improved duct has the temperature of 1℃ lower than the seat with the existing duct. This result contributes to develop the improved duct. Hereafter, the methods used in this study are expected to be useful at checking the flow resistance loss of the ventilation seat duct and assessing the flow channel design

This research is to investigate the performance analysis of fuel cell for flow channel with four different types of the channel (Serpentine I, II, Inter-digitated, Parallel) in the fuel cell stack. Velocity, pressure. and temperature distributions of fluid over the flow domain of the flow channel are numerically calculated for the optimum design of flow channel with unifrom inlet velocity. According to the calculations of low pressure drop between inlet and outlet in the flow channel, Serpentine I type is of highest performance of the flow channel shapes in the present fuel cell model.

A numerical analysis was performed to study PEMFC performance characteristics depending on the flow direction of cathode reactant gas, cathode relative humidity, and porosity of gas diffusion layer. As cathode relative humidity decreases and porosity increases, current density increases due to better diffusion of reactant gas to cathode surface. As current density increases, power density increases initially and then decreases with its maximum located around current density value of 2.2 Amperes per square centimeter. From the analysis of current density distribution inside membrane, the counter-flow cases show more uniform profile across the membrane than the co-flow cases due to more uniform reactant gas supply.

A numerical analysis was performed to study PEMFC characteristics depending on the flow direction of reactant gas in cathode gas channel using the Fluent. As cathode relative humidity increases, water mass fraction increases due to back diffusion from cathode. For the both of co-flow and counter-flow cases, water mass fraction is higher near the hydrogen inlet region where the chemical reaction rate is high. In overall, counter-flow case gives higher current density compared to co-flow case for the same operating conditions. However, the difference in the current density is not high. The temperature is also higher near the hydrogen inlet region due to the chemical reaction rate for the both of co-flow and counter-flow cases.

Material flow control mechanism is a kind of operational policy in manufacturing. It is very important because it varies throughput, throughput time, and work-in-process (WIP) under the same manufacturing resources. Many Researchers have developed various

실리카 콜로이드 용액의 한외여과에서 중력 방향에 대한 막모듈의 위치(경사각) 변화에 따라 발생되는 자연대류 불안정 흐름이 막오염 형성 감소에 미치는 효과를 규명하였다. 막표면에 케이크 층을 형성함으로써 막투과 플럭스의 감소를 발생시키는 실리카 입자(평균 크기 = 7, 12, 22, 50 및 78 nm)가 함유된 5가지 종류의 콜로이드 용액을 사용하여 중력 방향에 대한 막모듈의 위치(경사각 = 0~180℃)에 따른 막투과 플럭스 변화를 교반이 없는 회분식(dead-end) 한외여과 실험을 통해 측정하였다. 자연대류 불안정 흐름 발생이 막성능에 미치는 효과는 플럭스 향상도(Ei)로서 평가하였다. 상대적으로 크기가 작은 실리카 입자(7, 12 및 22 nm)가 함유된 콜로이드 용액의 한외여과에서는 막모듈의 경사각이 커짐에 따라 자연 대류 불안정 흐름 발생의 강도가 증가하였으며, 동일한 경사각에서 실리카 입자의 크기가 작을수록 자연대류 불안정 흐름의 발생 정도가 더 크게 나타났다. 자연대류 불안정 흐름의 발생은 막표면에 형성된 실리카 케이크층의 벌크 용액으로의 역이동(back transport)을 유발시킴으로써 플럭스 향상의 막성능 개선 효과를 나타내었다. 그러나 상대적으로 크기가 큰 실리카 입자(50 및 78 nm)가 함유된 콜로이드 용액의 한외여과에서는 자연대류 불안정 흐름 발생이 나타나지 않았다. 이 결과로부터 실리카 입자의 크기가 자연대류 불안정 흐름의 발생 강도에 영향을 미치고 있음을 알 수 있었다.

분구의 구경과 액분산기의 구조가 각각 다른 12종의 미니스프링클러를 대상으로 살수량과 살수강도분포를 실험하여 얻은 주요 결과는 다음과 같다. 미니 스프링클러의 살수량은 분구의 이론 유출량 산출 수식에 의해 예측할 수 있었다. 실험한 스프링클러의 유량계수는 분구구경 증가에 따라 감소하여 그 크기는 분구구경 0.8, 1.2, 1.6mm의 경우 각각 0.90-30.95, 0.80-0.82, 0.76-0.79의 범위로 나타났다. 스프링클러의 살수 분포는 동일한 구조의 스프링클러의 경우 분구구경이 작을 수록 그리고 살수압력이 낮을 수록 균일한 것으로 나타났다. 이러한 스프링클러의 살수분포는 분구구경이나 살수압력 외에도 액분산기의 구조에 따라 크게 영향을 받으므로 액분산기의 구조를 변화하므로서 살수입자의 최대 도달거리나 살수의 균일도를 높일 수 있음을 알 수 있었다.