• 한국수산과학회지
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• 제30권5호
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• pp.691-699
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• 1997

본 연구에서는 트롤그물의 유수저항 특성 및 그 저항을 그물의 구조, 규격 등으로 정도 높게 표현해내는 방법을 얻어내는 것을 목약으로 하여, 벽 면적이 $S(m^2)$되는 트롤그물이 유속 $\nu\;(m/sec)$에서 받는 유수저항 R(kg)을 $R=kSv^2$으로 표시하고, 지금까지 행해진 저항실험 결과들을 수집하여 윗 식의 형태로 정리하였으며, 저항계수 $k(kg{\cdot}sec^2/m^4)$를 전보 에서 구한 저항식에 의해 해석하였다. 그 결과, k는 그물 입구의 단면 을 $S_m\;(m^2)$, 흐름에 수직인 평면에 대한 그물의 총 투영면적을 $S_n\;(m^2)$, 그물감의 대표치수를 $\lambda$($={\pi}d^2/2lsin2\varphi;\;d$ : 그물실의 지름, 2l : 그물코의 크기, $2\varphi$ 그물코의 전개각)라 할때, 저층 트롤과 중층 트롤에서 각각 $$k=4.5(\frac{S_n}{S_m})^{1.2}v^{-0.2}$$ in case of bottom trawl nets and as $$k=5.1\lambda^{-0.1}(\frac{S_n}{S_m})^{1.2}v^{-0.2}$$ 및 $$k=5.1\lambda^{-0.1}(\frac{S_n}{S_m})^{1.2}v^{-0.2}$$ 으로 표시할 수 있었고, 이들에서 $S_n/S_m$의 값은 각각의 그물과 벽 면적이 같은 원추형 자루그물로부터 구해도 된다는 것을 알 수 있었으며, 설계 방식이 일반화 되어 있는 그물들의 경우는 유수저항 R(kg)을 저층 트롤과 중층 트롤에서 각각 $$R=1.5\;S\;v^{1.8}$$ 및 $$R=0.7\;S\;v^{1.8}$$으로 표시해도 좋다는 것을 알 수 있었다.

• 한국지반공학회지:지반
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• 제11권3호
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• pp.139-162
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• 1995

WIPP에서 가스로 인한 파괴의 가능성을 해석적 계산과 수치해석 및 실내실첩을 통하여 연구하였다. 우선 본 연구와 관련된 화학반응식을 조사한 결과, 폐기물 내의 철이 산화하면서 다량의 가스가 발생될 수 있음을 알았다. 또한 간단한 지하수 흐름의 계산결과, 투수성이 높은 파쇄영역이 존재하지 않는 경우 이 가스량은 암염 내부와 약한 수평면에 인장균열을 초래하기에 충분히 높은 압력을 야기시킬 것이다. 해석적 계산은 선형탄성파괴역학의 개념을 사용하여 수행하였고, 수치해석은 유한요소법을 사용하여 행하였다. 또한 실내실험은 발생가능한 파괴 메카니즘을 설명하기 위하여 행하였다. 해석결과 약한 경석고층에서 수평으로 균열이 증가된 뒤에 그 균열은 이 층을 뜰고나가 암염 위쪽으로 계속 전폭되어 지표면 쪽의 수평방향과 53$^{\circ}$경사각을 갖고 지표면에 도달된다. 이와 같은 후자의 현상을 방지하기 위하여 경석고는 암염의 인성보다 0.5590배가 적은 파괴인성을 가져야 하는 것으로 나타났다. 실험결과 세 가지 형태의 균열(radial vertical cracks, horizontal circular cracks and cone -shaped cracks)이 관찰되었다.

• Journal of Biosystems Engineering
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• 제10권1호
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• pp.13-23
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• 1985

Spraying method from the paddy-field levee is known to give insufficient penetration of the spray droplets to the rice stem of the densely grown plants, which is generally encountered at the last stage of rice growth. This study was intended to investigate the spraying system to solve this existing problem. As an approach, it was attempted to develop the boom-with-nozzle, between-the-row application system. Several types of nozzles and their different arrangements in the boom were tested in the field to measure the penetration-reaching distance and the uniformity of spray droplet distribution. The results of the study are summarized as follows: 1. Field experiments by the spraying method from the paddy-field levee showed to have practically no penetration of the spray droplets to the portion of the plant stem with the normal flow volume generally applied and thus need for improving present spraying method. 2. It was found that, considering both the uniformity of the spray droplet distribution and performance rate, the most efficient type of nozzle in the between-the-row boom-type spraying system was one that has core-insert hollow-cone with some clearance between the cone and tip. 3. When tested by applying the spraying method of between-the-row, the nozzle pressure did not affect the uniformity of spray droplet distribution. However, the nozzle pressure had a positive effect on the penetrating-reaching distance of the facing side of the rice stem and did not affect much on that of the opposite face of the stem. It was also found that the maximum pressure to affect the penetration-reaching distance was about $10kg/cm^2$. 4. The uniformity of the spray droplet distribution in the between-the-row system was greatly affected by the height and orientation of the nozzles in the boom. Based on experimental work for the different type of the boom-with-nozzle arrangements, it is recommended that the position of nozzle is set at about 0.45 m above the ground and two nozzles in the boom are oriented to be faced with each other with some angle such that the droplet stream from the nozzle would not directly face with each other.

• 한국음향학회지
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• 제37권4호
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• pp.163-173
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• 2018

본 논문에서는 비행 중 비행체 표면에 작용하는 음향하중 예측을 수행하였다. 비행 중 음향하중은 비행체 표면의 압력 변동에 의해 발생한다. 기존의 비행 중 음향하중 예측방법은 반경험적 방법으로 이론과 실험 결과를 기반으로 도출한 경험식을 활용한다. 하지만 경험식의 입력 값으로 사용되는 비행체 주변 유동특성 및 경계층 파라미터를 매번 실험을 통해 얻는 것에는 한계가 있다. 따라서 본 논문에서는 전산유체해석(Computational Fluid Dynamics, CFD) 결과를 반경험적 방법과 혼합하는 하이브리드 방법을 이용하여 비행 중 비행체에 작용하는 음향하중을 예측하였다. Cone-cylinder-flare 형상 비행체에 대해 아음속, 천음속, 초음속, 최대동압도달(Maximum dynamic pressure, Max-q) 시점의 비행 환경에 대한 음향하중 예측을 수행하였다. 하이브리드 방법 적용 시 전산유체해석결과를 기반으로 한 경계층 끝단 영역 판단 방법에 대해 비교하였고 여러 연구자에 의해 제시된 경험식에 따른 음향하중 예측결과를 비교하였다.

• 대한기계학회논문집B
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• 제25권10호
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• pp.1400-1407
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• 2001

The size distributions of electrospray droplets from the Taylor cone in cone-jet mode are directly measured by using a freezing method and a transmission electron microscope (TEM) image processing technique. These results are compared with the data obtained by an aerodynamic size spectrometer (TSI Aerosizer DSP). The use of glycerol seeded with NaI and a freezing method make it possible to sample droplets with their original sizes preserved. Since pictures of droplets are taken with TEM with very low vapor pressure of the solution, evaporation is suppressed by freezing. For liquid flow rates below 1 nl/sec, the measured droplet diameters by the TEM image processing technique and the aerosizer are in the range of 0.25 to 0.32 m add 0.3B to 0.40m, respectively. Comparing the TEM data with the aerosizer measurements, it has been revealed that the TEM image processing technique can afford more accurate values of droplet size distributions in the submicron range of 0.1 to 0.4m.

• 한국추진공학회지
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• 제20권4호
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• pp.68-76
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• 2016

본 연구는 이원추진제 추력기의 핵심부품에 대한 성능평가의 일환으로, 기체메탄/액체산소를 추진제로 사용하는 스월 동축형 인젝터의 리세스 길이 및 분사압력에 따른 분무특성 파악을 목표로 하였다. 분무형상은 슐리렌 가시화 기법을 이용하여 획득하였고, 슐리렌장치는 광원, 오목거울, 초고속카메라 등으로 구성된다. 내부 인젝터에 의한 액체 분무의 경우 hollow cone 형상을 확인하였으며, 내부 인젝터 오리피스 길이의 증가와 함께 스월강도 감쇠의 영향으로 분무각은 줄어들었다. 기체-액체를 함께 분사할 때, 분무각은 리세스 길이가 증가함에 따라 외부혼합영역에서 증가하지만, 내부혼합영역에서는 작아졌는데, 액체분무 분사 압력의 높고 낮음에 무관하다는 사실을 확인하였다.

• 한국자동차공학회논문집
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• 제12권2호
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• pp.32-38
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• 2004

This study was performed to investigate the behavior of liquid and vapor phase of fuel mixtures with different piston cavity diameters in a optically accessible engine. The conventional engine was modified as Central Injected DI gasoline engine with swirl motion. Two dimensional spray fluorescence images of liquid and vapor phase were acquired to analyze spray behavior and fuel distribution inside of cylinder using exciplex fluorescence method. Piston cavity geometries were set by Type S, M and L. The results obtained are as follows. In the spray formation after SOI, the cone angle and width of the spray were decreased at late injection timing. With a fuel injection timing of BTDC $180^{\circ}C$, fuel was not greatly affected in a piston cavity but generally distributed as homogeneous mixture in the cylinder. With a fuel injection timings of BTDC $90{\circ}C$ and $60^{\circ}C$, fuel mixture was widely distributed in near the cavity center. As a injection timing was late in the compression stroke, residual width of fuel mixture was narrow in proportion to piston cavity.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2011년도 정기총회 및 추계학술대회 논문집
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• pp.88-93
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• 2011

The aerodynamic drag characteristics of HEMU-400X which has been being developed for the maximum speed of 430km/h were analyzed experimentally as the variations of the pantograph cover configurations to reduce the acoustic noise and the aerodynamic drag of the pantograph system. The wind tunnel tests were performed with three pantograph cover models upon 1/20 scaled 5-car model of HEMU-400X. Two kinds of wedge shapes which induce up-flow in the vicinity of the pantograph and one cone shape which reduces the whole train drag were used in order to compare the aerodynamic characteristics as the pantograph cover shape changes. The each axial force of 5 each car was measured at a time with the test velocities, 30, 40, 50, 60m/s. Through the wind tunnel test the base drag forces of HEMU-400x model and the forces by the pantograph cover on the train model were investigated and the aerodynamic drag characteristics of the train model by the pantograph cover configurations were analyzed.

• International Journal of Automotive Technology
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• 제2권4호
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• pp.165-170
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• 2001

This study is focussed on the investigation of spray characteristics from the high pressure gasoline injector for the application of gasoline direct injection engine. For the analysis of spray structure of high pressure gasoline injector; the laser scattering method with a Nd-Yag laser and the Phase Doppler particle analyzer system were applied to observe the spray development and the measurement of the droplet size and velocity of the spray, respectively. Also spatial velocity distribution of the spray droplet was measured by use of the particle image velocity system. Experimental results show that high pressure gasoline injector shapes the hollow-cone spray, and produce the upward ring shaped vortex on the spray surface region. This upward ring shaped vortex promotes the secondary atomization of fuel droplets and contributes to a uniform distribution of fuel droplets. Most of fuel droplets are distributed under 31$\mu m$ of the mean droplet size (SMD) and the frequency distribution of the droplet size under 25$\mu m$ is over 95% at 7 MPa of injection pressure. According to the experimental results of PIV system, the flow patterns of the droplets velocity distribution in spray region are in good agreement with the spray macroscopic behaviors obtained from the visualization investigation.

• Tribology and Lubricants
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• 제26권1호
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• pp.21-30
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• 2010

In this research, it is investigated the collecting efficiency of jet oil to several types of piston oil cooling gallery by using recently developed PCJ (piston cooling jet) rig tester. So it will be selected for a better design of piston oil cooling gallery. The collecting efficiencies at each type of piston cooling galleries are measured under conditions of a few piston positions, and several oil jet pressures and oil viscosities. Furthermore, the type of jet cone will be compared for a few jet pressure conditions. The selected type of piston oil cooling gallery is planned to be applied to the target engine which is now developing to satisfy the EURO VI emission regulation.