• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2007년도 춘계학술대회B
• /
• pp.2579-2584
• /
• 2007

A digital micro holographic particle tracking velocimetry (HPTV) system consisting of a high-speed camera and a single laser with acoustic optical modulator (AOM) chopper was established. The digital micro HPTV system was applied to water flow in a micro curved-tube for measuring instantaneous 3-D velocity field data consecutively. The micro curved-tube is using to reproduce the dorsal aorta or utilize in various lap-on-a-chip. The temporal evolution of a three-dimensional water flow in the micro curved-tube (the curvature, ${\kappa}$=1/${\phi}$, 2/${\phi}$, 4/${\phi}$, 8/${\phi}$) of 100 ${\mu}m$ and 300 ${\mu}m$ inner diameters was obtained and mean velocity field distribution was obtained by statistical-averaging the instantaneous velocity fields.

• 융복합기술연구소 논문집
• /
• 제1권2호
• /
• pp.25-28
• /
• 2011

Void fraction has been measured for the gas-liquid cocurrent slug flow in 8mm vertical acrylic tube using an optical method. Bubble speed, length and period could be measured with the two sets of laser-infrared sensor modules mounted 25mm apart alongside the tube, which were designed to detect variation of light intensities with a time delay when two parallel laser beams were refracted successively by a passing bubble. It was found that the results were in good agreement with the previous studies in the literature suggesting that the method used in this study were sound and accurate.

• 한국가시화정보학회지
• /
• 제8권3호
• /
• pp.41-48
• /
• 2010

A visualization study to evaluate bubble motion in a tab water filled cylindrical tank with a varying flow rate of compressed air is conducted. The flow rate of compressed air varies from 1 to 5 L/min. Time resolved images are acquired by a high speed camera in 10 bit gray level at 100 fps and the measurement volume is irradiated by a 230 W halogen lamp. It is observed that there are three different regions; the bubble formation region, the rising bubble region and the free surface region. During the rise of bubble, the shape is changed as if an elastic body. Based on the binarized bubble image, the mean diameters of rising bubbles are estimated at beneath of the free surface. As the gas flow rate increases, the mean diameter is increased and the rising velocity also increases with buoyancy force.

• 오토저널
• /
• 제10권5호
• /
• pp.42-53
• /
• 1988

The effects of ignition position on combustion in a chamber with swirl flow were investigated by use of hot wire anemometer, high speed schlieren photography, and chamber pressure measurement. In experiments, the closed-constant volume combustion chamber was used, and the swirl was formed unsteadily by suction of external fluid after reducing pressure in the chamber. Results show that the effect of ignition position on combustion depends on the flow state and the flame propagation distance corresponding to each ignition position. Also, the effect of combustion promoting increases as an ignition position moves from the center of chamber to the outside, but maximum burning pressure was obtained at the position that is the shortest flame propagation distance.

• 대한조선학회논문집
• /
• 제43권4호
• /
• pp.422-430
• /
• 2006

The horn and movable parts around the gap of the conventional semi-spade rudder are visualized by high speed CCD camera with the frame rate of 4000 fps (frame per second) to study the unsteady cavity pattern on the rudder surface and gap. In addition, the pressure measurements are conducted on the rudder surface and inside the gap to find out the characteristics of the flow behavior. The rudder without propeller wake is tested at the range of $1.0{\leq}{\sigma}_v\;1.6$ and at the rudder deflection angle of $-8{\leq}{\theta}{\leq}10^{\circ}$. The time resolved cavity images are captured and show strong cavitation around the rudder gap in all deflection angles. As the deflection angle gets larger, the flow separated from the horn surface increases the strength of cavitation. The accelerated flow along the horn decreases its pressure and the separated flow from the horn increases the pressure abruptly. The pressure distribution inside the gap reveals the flow moving from the pressure to suction side. In the negative deflection angle, the turning area on the movable part initiates the flow separation and cavitation on it.

• 한국항행학회논문지
• /
• 제22권6호
• /
• pp.551-556
• /
• 2018

과거에 비해 최근에는 항공기 비행 및 기상정보측정을 위하여 드론을 많이 활용하고 있다. 관련 응용분야로는 저고도 대기자료 측정, 대기미세먼지측정, 대기 오염측정 등이 있다. 그러나 대기자료 측정센서의 장착위치는 드론비행체의 구조적 특징 때문에 프로펠러 유동의 영향, 전자파 영향, 드론의 무게중심의 변화를 고려하여 장착하여야 한다. 이중에서 프로펠러에 의한 기체 상부의 공기유동은 센서의 풍속 및 풍향에 영향을 미치므로 최적 위치를 분석하여 선정해야 한다. 본 연구는 대기자료 측정센서의 적정 높이 선정에 대한 연구로, 유동 해석을 통하여 유동특성을 파악하고 실험 데이터를 비교 분석하여 적정 센서 장착 높이를 제시한다.

• 한국정보전자통신기술학회논문지
• /
• 제15권5호
• /
• pp.349-359
• /
• 2022

본 연구는 자동 조향 트랙터용 비례제어밸브의 국산화를 위한 기초연구로써 다양한 트랙터 조향 조건에 따른 조향 비례제어밸브 동특성 계측 및 분석을 위해 수행되었다. 동특성 데이터는 유량 및 압력 계측 시스템을 통해 수집되었으며, 수집된 유량 및 압력 데이터를 이용하여 동력을 분석하였다. 실험 조건은 트랙터 엔진 회전속도와 조향각을 주요 변수로 선정하였으며, 실험은 우레탄 노면 조건에서 수행되었다. 그 결과, 트랙터 엔진 회전속도 및 조향각이 증가함에 따라 비례제어밸브 유량, 압력, 동력이 모두 증가하는 것으로 나타났다. 특히, 동일한 엔진회전속도에서 조향각이 증가함에 따라, 유량, 압력, 동력은 각각 최대 190%, 172%, 273% 증가하는 경향을 보였으며, 동일한 조향각에서 엔진회전속도가 증가함에 따라, 유량, 압력, 동력은 각각 최대 161%, 122%, 168% 증가하는 경향을 보였다. 이를 통해, 조향각이 엔진 회전속도보다 비례제어밸브의 동특성에 더 높은 영향을 미치는 것을 확인하였다.

• 에너지공학
• /
• 제11권4호
• /
• pp.299-305
• /
• 2002

본 연구에서 실험과 수치해석 검증은 지름비 0.52인 동심환형관내에서 안쪽축이 회전하고 바깥쪽축이 고정된 유동장의 유동특성을 수행하였다. 압력손실과 마찰계수는 안쪽축이 0~600 rpm 회전시 물과 0.2% CMC 수용액을 완전히 발달된 유동장에서 측정하였다. 천이유동은 표면마찰계수(C$_{f}$ )에 대하여 로스비수(Ro)와 레이놀즈수(Re)관계를 나타내기 위하여 압력손실 측정에 의해 확인하였다. 천이발생은 레이놀즈수에 대하여 압력손실과 마찰계수의 구배변화에 의해 조사하였다. 회전으로 인한 마찰계수의 증가율은 천이영역에서 대하여 갑자기 감소함에 반하여 층류영역에서 균일하며, 난류영역에서는 점차적으로 감소함을 알 수 있었다.

• 한국유체기계학회 논문집
• /
• 제6권4호
• /
• pp.14-20
• /
• 2003

In this study an analysis of the flow characteristics in three types of turbo-fans for a vacuum cleaner was performed by using CFD. The characteristics of three models calculated for various rotating speed for flow rates are obtained and compared with measured data. The mixing plane approach is applied to compute the flow between impeller and diffuser. The results show that the model that is modified to reduce fan noise gives stable flow characteristics in operating range than the original model, with both models show similar performance characteristics at the range of high flow rate. Since in the modified model it takes much longer for an impeller blade to pass a diffuser blade than in the original model, and the peak pressure at BPF can be relieved, it is anticipated that the modified model give much lower noise level with similar performance than the original one, which remains to be verified by unsteady computation and measurements. The good agreement between the predictions and measurement results confirms the validity of this study.

• 한국자동차공학회논문집
• /
• 제9권2호
• /
• pp.59-66
• /
• 2001

This experimental study is to investigate the flow characteristics of the multi-hole nozzle used in the fuel injection system of a heavy-duty diesel engine. A multi-hole diesel nozzle with a 2-spring nozzle holder was used in this study and without changing the total orifice exit area, its hole number varied from 3($d_n$=0.42mm) to 8($d_n$=0.25mm). The injection pressure and needle lift were measured and Bosch type injection rates measurement system was used. The discharge flowrates of each orifice in the multi-hole nozzle changed by the flow conditions inside the nozzle sac hole. In case that pump speed and injection quantity were low, the orifice located in the vertex of nozzle tip had a great deal of injection quantity compared with that of others. As the increment of multi-hole number, the injection duration and the mean injection pressure decrease. The mean and peak injection rates, however, increase. Actually, the mean flow coefficient(${C_d}_{(mean)}$) increases, too. The flow coefficient of the multi 8 hole was evaluated as Cd(mean)=0.74 and that is the maximum value among the examined conditions.