• 한국해양공학회지
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• 제16권6호
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• pp.18-24
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• 2002

The vibrational system in this study consists of a cantilever pipe conveying fluid, the moving mass upon it, and an attached tip mass. The equation of motion is derived by using the Lagrange equation. The influences of the velocity and the velocities of fluid flow in the pipe have been studied on the dynamic behavior of a cantilever pipe using a numerical method. While the moving mass moves upon the cantilever pipe, the velocity of fluid flow and the nozzle angle increase; as a result, the tip displacement of the cantilever pipe, conveying fluid, is decreased. After the moving mass passes over the cantilever pipe, the tip displacement of the pipe is influenced by the potential energy of the cantilever pipe and the deflection of the pipe; the effect is the result of the moving mass and gravity. As the velocity of fluid flow and nozzle angle increases, the natural frequency of he system is decreased at the second mode and third mode, but it is increased at the first mode. As the moving mass increases, the natural frequency of the system is decreased at all modes.

• 자원리싸이클링
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• 제13권6호
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• pp.16-25
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• 2004

인듐 성분을 포함하는 원료용액을 분무열분해 시켜서 평균 입자크기 100 nm 이하의 인듐 산화물 나노 분말을 제조하였으며, 용액의 농도, nozzle tip 크기 및 공기의 유입속도 변화에 따른 생성된 분말들의 특성 변화를 파악하였다. 본 연구는 폐 ITO로부터 나노 크기의 ITO 분말을 제조하기 위한 전 단계 연구로 수행되었다. 원료용액 내의 인듐 성분의 농도가 40 g/l로부터 350 g/l로 증가됨에 따라 생성된 분말의 평균 입자크기는 20~30 nm로부터 50~60 nm로 점점 증가하는 반면 입도분포는 더욱 불균일하게 나타나고 있었으며, XRD peak의 강도는 점점 증가하고 비표면적은 감소되었다. Nozzle tip의 크기가 1 mm로부터 5 mm로 증가함에 따라 분말들의 평균 입자크기는 40 nm 정도로부터 100 nm 정도까지 점점 증가하고 입도분포는 더욱 불균일하게 나타나고 있었으며, XRD peak 강도는 증가하는 반면 비표면적은 감소되었다. 반응로 내로 유입되는 공기의 압력이 0.1 kg/cm$^2$로부터 0.5 kg/cm$^2$로 증가되는 경우, 분말의 평균 입자크기는 90~100 nm로 현저한 변화를 나타내지 않았다. 반면 공기압력이 1 kg/cm$^2$ 및 3 kg/cm$^2$로 증가하는 경우에는 평균 입자크기가 50~60 nm 정도까지 감소하였으며, XRD peak 강도는 감소하고 비표면적은 증가되었다.

• 항공우주기술
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• 제6권2호
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• pp.197-204
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• 2007

터번로터 팁 형상의 변화에 따른 터보펌프 터빈의 성능변화에 대하여 실험적 연구를 수행하였다. 한국항공우주연구원에서 개발중인 30톤급 터보펌프용에 장착된 초음속 충동형 터빈을 기본 모델로 하여 터번로터 슈라우드 유무 및 팁간극 크기에 따른 터빈성능변화를 측정 비교하였으며, 이와 더불어 노즐-로터 오버랩에 따른 터빈성능 변화 연구도 함께 이루어졌다. 시험 수행 결과, 로터 슈라우드 유무에 따라 터빈성능의 절대량은 크게 변화하나 팁간극의 변화에 따른 터빈효율의 민감도는 초음속 충동형 터빈의 경우 고효율 아음속터빈에 비해 크게 작은 것으로 나타났다. 아울러, 최적 효율을 나타내는 노즐-로터 오버랩 값이 존재하는 것을 실험을 통해 확인하였다.

• International Journal of Automotive Technology
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• 제6권1호
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• pp.9-14
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• 2005

An experimental investigation has been carried out to reveal the atomization process of the diesel fuel spray. The spray injected through a single hole nozzle was taken by a camera on the opposite side of a stroboscope for macroscopic observation or a nanolite for microscopic observation. The effect of nozzle aspect ratio was analyzed with disintegration phenomena of the diesel spray. Based on the enlarged spray photograph, atomization process was observed in detail and further the spray cone angle was measured under various ambient pressures. The result shows that atomization of diesel spray in early stage of injection is mainly progressed in the vicinity of spray periphery region except the region close to the nozzle exit and spray head region. The spray cone angle is nearly constant under the pressurized condition, while it decreases with elapsing time under the atmospheric condition.

• Journal of Mechanical Science and Technology
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• 제18권12호
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• pp.2294-2302
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• 2004

The objective of this study is to obtain detailed information for the micro fabrication of lead frames by applying spray technology to wet etching process. Wet etching experiments were performed with different etching parameters such as injection pressure, distance from nozzle tip to etched substrate, nozzle pitch and etchant temperature. The characteristics of single and twin spray were measured to investigate the correlation between the spray characteristics and the etching characteristics. Drop size and velocity were measured by Phase-Doppler Anemometer (PDA). Four liquids of different viscosity were used to reveal the effects of viscosity on the spray characteristics. The results indicated that the shorter the distance from nozzle tip and the nozzle pitch, the larger etching factor became. The average etching factor had good positive correlation with average axial velocity and impact force. It was found that the etching characteristics depended strongly on the spray characteristics.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.160-163
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• 2010

부분흡입형 초음속 터빈의 노즐과 1단 로터 사이의 축방향 간극이 터빈의 단 성능과 유동장에 어떤 영향을 미치는지 알아보기 위해 터빈에 대한 3차원 유동해석을 수행하고 그 결과를 분석하였다. 상용 유동해석 프로그램 $FLUENT^{TM}$를 사용하였으며 다섯 가지 경우의 축간극에 대해 계산을 하였다. 노즐-로터 축간극이 팁 누설 유량의 증가와 로터 출구의 유동각에 영향을 주는 것을 확인하였다.

• 한국분무공학회지
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• 제10권1호
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• pp.10-16
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• 2005

To investigate the effect of shockwave on diesel spray characteristics under ultra high pressure injection, the velocity of spray tip and shock wave were investigated using the visualization of spray by schlieren method. Spray characteristics such as the spray radius, height, and droplets size were analyzed. It is found in this study that shock wave, produced by ultra high injection pressure, propagates faster than spray tip. Spray radius of right side of nozzle tip was shorter than that of left side and spray height of right side of nozzle tip was thicker than that of left side. Droplets sue was increased at 414MPa in injection pressure because of pressure gradient between inner and outer of tile spray caused by shockwave.

• 대한용접접합학회:학술대회논문집
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• 대한용접접합학회 1999년도 특별강연 및 추계학술발표대회 개요집
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• pp.146-149
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• 1999

To develope the high speed gas cutting tip, consists of 3 pieces, supersonic axisymmetric jets issuing from various kinds of nozzles with a throat diameter of a few milimeters were experimentally investigated. The nozzle inlet pressure was varied from 4 to 8 kgf/$\textrm{cm}^2$. The parameters in nozzle design were throat diameter, throat length, taper angle, outlet diameter. The total pressure variation was measured by the pilot tube, 0.5mm outer diameter, along the center of the free stream jet. Also color Shilieren system was used to visualize the flowfield.

• 열처리공학회지
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• 제5권3호
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• pp.171-178
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• 1992

The effect of nozzle characterristics on the mist-cooling heat transfer was investigated under the various flow conditions. Two different types of twin fluid nozzle were used, one is a $90^{\circ}$ angle tip nozzle with needle and the other is a $90^{\circ}$ angle tip non-needle nozzle. The cooling rate from the heated surface was measured and obtained the boiling curve as a function of surface temperature. An immersion sampling was employed for the measurement of droplet size of the spray. As a result of this experiment, the liquid sheet type nozzle shows better atomization when the mass ratio Mr>2.0, and collects more liquid droplets on the heated surface that results in better cooling effect. It was found that the maximum heat flux and heat transfer coefficient increased with increase in the volumetric flow rate, whereas the maximum heat flux decreased with increase in spray distance. The cooling effect depends upon the amount of collected droplet and droplet size, but it strongly depends upon the amount of collected droplet.

• 한국안전학회지
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• 제18권4호
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• pp.51-56
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• 2003

The goal of this study is to show the way to decrease the noise from air nozzles. The variables of this test are the shapes of air nozzles, air flow rate and the distance between a reflection plate and a nozzle tip. This experiment is aimed to find the most appropriate condition to minimize the noise. These are the results. If diameter ratio is more than 12:8, noise level increases by over 10 dB(A) regradless of the distance between a reflection plate and a nozzle and the existence of a reflection plate. And when $L_2$ of a nozzle is 5mm long, noise level rise relatively highly. So, it is strongly recommended that $L_2$ should be manufactured more than 10mm. The reason for a high intensity noise is that when diameter ratio is more than 12:8, the diameter of a nozzle tip($D_2$) turns small drastically, which increases the air velocity. It is assumed that when the vortes is great around the spots where a nozzle hole is suddenly smaller, great turbulent flow increases much noise.