• 한국추진공학회지
• /
• 제8권4호
• /
• pp.1-8
• /
• 2004

본 연구에서는 초음속 충동형 터빈 익렬의 유동특성을 알아보기 위해 소형 초음속 풍동을 설계하였으며 Single pass Schlieren system을 이용하여 유동을 가시화하였다. 실험은 3차원 초음속 노즐과 익렬을 조합하여 노즐 설치각에 따라 실시하였다. 실험을 통해 충격파를 포함한 복잡한 유동 형태와 노즐-익렬, 충격파-경계층 상호작용 등을 관찰할 수 있었다.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
• /
• pp.807-812
• /
• 2004

In this paper, a small supersonic wind tunnel was designed and built to study the flow characteristics of a supersonic impulse turbine cascade by experiment. The flow was visualized by means of a single pass Schlieren system. The supersonic cascade with 3-dimensional supersonic nozzle was tested over a wide range of pressure ratio. Highly complicated flow patterns including shocks, nozzle-cascade interaction and shock boundary layer interactions were observed.

• International Journal of Automotive Technology
• /
• 제6권2호
• /
• pp.87-93
• /
• 2005

Spray patterns were visualized using the shadowgraph method, and the droplet size and velocity were measured using PDPA for high-pressure injections up to 2,600 bars. The spray pattern and spray characteristics, such as penetration, spray width, spray angle, droplet size, injection duration, and droplet velocity, were investigated to determine the suitable injection pressure. Spray penetration, width, angle, and velocity increased continuously up to 2,600 bars with the injection pressure in a high-pressure region. The rate of improvement of the above spray characteristics, however, declined rapidly, when the injection pressure reached 2,000 bars. The injection duration and droplet size generally decreased with the increase in the injection pressure, while the rate of improvement decreased abruptly after 2,000 bars. Consequently, the improvement rate of the spray characteristics became blunt at over 2,000 bars. This means that the suitable injection pressure is around 2,000 bars.

• 대한설비공학회지:설비저널
• /
• 제15권2호
• /
• pp.196-203
• /
• 1986

The melting phenomena of horizontal cylindrical ice-bar immersed in water and air concentrically in the cylinder are experimentally investigated for the temperature range from $3.5^{\circ}C\;to\;2.5^{\circ}C$. The shapes of the melting ice-bar are recorded photographically by the shadowgraph method. The shadowgraphs of the melting ice-bar show that water adjacent to the bar flows upward for the temperature range from $3.5^{\circ}C\;to\;5.8^{\circ}C$ while above $5.8^|\circ}C$ the flow is downward direction. The local and average Nusselt numbers are obtoined with the recorded shadowgraphs and comparator. Melting shapes of the ice-bar in the air show the vortex motion in the bottom portion of the bar, whereas no vortex motion appears in the bottom portion when the bar is melted in the water.

• 한국분무공학회지
• /
• 제28권3호
• /
• pp.113-118
• /
• 2023

This study investigates the evaporation characteristics of paired sessile droplets on a heated substrate. In particular, the evaporation time and contact line behaviors were analyzed based on the droplet-to-droplet distance and substrate temperature. The contact line behavior and volume variations were visualized using the shadowgraph method. It was observed that the contact diameter and contact angle exhibited similar behavior for both single and paired droplets regardless of the droplet-to-droplet distance and substrate temperature. The paired droplets demonstrated a longer evaporation time than the single droplet due to the vapor accumulation between the droplets. Furthermore, the scaled lifetime, defined as the ratio of evaporation time between paired and single droplets, increased as the droplet-to-droplet distance decreased and decreased as the substrate temperature increased, attributed natural convection.

• 한국가시화정보학회지
• /
• 제21권1호
• /
• pp.26-30
• /
• 2023

Interaction of a droplet and substrate is important to determine the coating and final deposition pattern in inkjet printing system. In particular, an accurate deposition of the droplet should be guaranteed for high-resolution patterning. In this study, we performed high-speed shadowgraph experiments on droplet train impact in inkjet system. From the high-speed images, we observed an unexpected bouncing phenomenon. We have found two factors affecting bouncing regime; the Weber number and the curvature of deposited droplet. Experimental results indicate that there is a critical curvature diameter of deposited droplet, which splits into bouncing and merging regime. From this result, we obtained a power-law behavior between the Weber number and the curvature. The understanding of bouncing phenomena helps to improve the accuracy and productivity of inkjet printing.

• 한국입자에어로졸학회지
• /
• 제13권4호
• /
• pp.151-158
• /
• 2017

실내 환경 및 산업체 배기가스중의 미세먼지를 제거하는 방법으로서 압력손실이 낮으면서도 집진효율이 높은 전기집진기가 널리 사용되어지고 있다. 그러나 전기집진기는 서브마이크로미터 크기의 먼지에 대한 제거효율이 낮기 때문에, 정전분무법으로 하전액적을 공급하여 먼지와의 충돌을 촉진시켜 하전효율을 높이는 방법이 대안으로 떠오르고 있다. 그러나 먼지의 하전효율은 정전분무된 액적의 크기 및 개수와 밀접한 관계가 있으나, 액적의 크기를 효과적으로 측정하는 방법이 확립되어 있지 않은 것이 현실이다. 본 연구에서는 손쉽게 이용할 수 있는 수돗물로 정전분무를 한 후, 분무된 액적을 다양한 방법으로 가시화하여 고속카메라로 촬영하였다. 그리고 Image J 프로그램으로 액적의 크기분포를 측정하여 가시화방법에 따른 액적의 크기를 상호 비교하였다. 결과적으로, 레이저로 가시화하여 고속카메라로 촬영하면 미세액적의 이미지화가 가능하기 때문에, 그 액적의 크기는 Xenon광으로 가시화하여 측정한 것보다 약 50 % 작음을 알 수 있었다. 또한 레이저로 가시화하여 측정한 액적의 크기가 $Fern{\acute{a}}ndez$ de la Mora and Loscertales (1994)의 예측치와 비교적 잘 일치함을 알 수 있었다.

• 한국자동차공학회논문집
• /
• 제17권2호
• /
• pp.75-81
• /
• 2009

A study was performed to investigate the characteristics of two-phase jet injected into subsonic cross-flow using the external mixed gas blast two-phase nozzle. The shadowgraph method was adopted for the cross-flow jet visualization and PDPA system was used to measure droplet size, velocity, and volume flux. The atomization of two-phase jet is initially determined according to gas to liquid mass flow-rate ratio and the Reynolds number of cross-flows. The highest penetration trajectories of two-phase jet injected into cross-flow are governed by the momentum ratio at subsonic cross-flow. As GLR of two-phase jet injected into cross-flow increases, the droplet size decreases and the distribution area of volume flux increases. The distribution of volume flux that influenced by the counter vortex pair at the downstream of cross-flow is symmetric in shape of horseshoe.

• Journal of Mechanical Science and Technology
• /
• 제17권11호
• /
• pp.1793-1800
• /
• 2003

The present study addresses an experimental investigation of the near field flow structures of supersonic, dual, coaxial, free, jet, which is discharged from the coaxial annular nozzle. The secondary stream is made from the annular nozzle of a design Mach number of 1.0 and the primary inner stream from a convergent-divergent nozzle. The objective of the present study is to investigate the interactions between the secondary stream and inner supersonic jets. The resulting flow fields are quantified by pitot impact and static pressure measurements and are visualized by using a shadowgraph optical method. The pressure ratios of the primary jet are varied to obtain over-expanded flows and moderately under-expanded flows at the exit of the coaxial nozzle. The pressure ratio of the secondary annular stream is varied between 1.0 and 4.0. The results show that the secondary annular stream significantly changes the Mach disc diameter and location, and the impact pressure distributions. The effects of the secondary annular stream on the primary supersonic jet flow are strongly dependent on whether the primary jet is under-expanded or over-expanded at the exit of the coaxial nozzle.

• 한국항공우주학회지
• /
• 제35권2호
• /
• pp.136-142
• /
• 2007

본 연구에서는 초음속 충동형 터빈의 유동특성을 알아보기 위해 소형 초음속 풍동을 설계하였다. 실험은 2차원 초음속 노즐과 익렬을 조합하여 터빈 설계 인자 중의 하나인 터빈 축 간격비에 따라 실시하였으며 단일경로 슐리렌(Schlieren) 시스템을 이용하여 유동을 가시화하였다. 그리고 다채널 압력측정 시스템을 이용하여 터빈 익렬 내의 정압력과 전압력을 측정하였다. 이러한 실험을 통해 충격파를 포함한 복잡한 유동 형태와 유동박리, 충격파-경계층 상호작용 등을 관찰할 수 있었다.