• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.3
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• pp.1-7
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• 2002

An experimental study was conducted to investigate the effects of leading edge extension(LEX) on the surface prssure distribution over a delta wing in a subsonic wind tunnel. Freestream velocity was 40m/sec and Reynolds number per meter was 1.7x$10^6$ with total pressure of 101Pa and total temperature of 278K. LEX changed the surface pressure distribution on the wing dramatically. Comparing with the results without LEX, the peak of pressure distribution decreased on the front chordwise location but it turned to increase on the rear chordwise location with increase of the angle of attaci. The spanwise gradient of the pressure distribution also increased in the rear chordwise location. Without LEX, the peak of pressure distribution increased and decreased irregularly with increase of the angle of attack at each chordwise location, but LEX made it increased almost linearly with increase of the angle of attack at all of the chordwise locations.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.814-819
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• 2017

The objective of this paper is to observe effects of an ignition position and time on the ignition transition. A gaseous oxygen and liquid kerosene are used for propellants with the shear-coaxial injector. In order to study the ignition delay time and combustion instability intensity, the pressure transducer was used. The ignition position was changed with the injector spacer. Sequences except the igniter operation time were fixed to compare the ignition time only. Initial pressure peak and ignition delay time increased as the ignition time was delayed. Also, the unstable flame development zone was detected as the igniter was away from the injector.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.253-256
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• 2009

In the present paper, experimental and numerical fundamental analyses of the occurrence of lateral force in overexpanded thrust nozzle were carried out. Investigation of the lateral force fluctuations in an thrust nozzle for the shutdown transient was presented. Wall pressure distribution and Schlieren Photographs as NPR were presented. Pressure peak is observed during transition of RSS to FSS.

• Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.13 no.3
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• pp.34-39
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• 1999

Electron temperature and electron density were rreasured in a radio-frequency inductively coupled plasma (RFICP) using a Langmuir probe method. Measurerrent was conducted in an argon discharge for pressures from 10 mTorr to 40 mTorr and input rf rnwer from 100 W to 600 W. Spatial distribution electroo temperature and electron density were rreasured for discharge with satre aspect ratio (R/L=2). Electron temperature and electron density were discovered depending on both pressure and power. Electron density was increased with iocreasing input power, but saturated at 450 W. Electron density was iocreased with iocreasing pressure. Radial distribution of the electron density was peaked at the rnsition which was a little rmved from center toward quartz window. Normal distribution of the electron density was peaked in the center between quartz plate and substrate. The above results could contribute to understand the Mechanism of Radio-Frequency Inductively Discharge Plasma.Plasma.

• Journal of the Institute of Electronics Engineers of Korea TC
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• v.43 no.1 s.343
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• pp.33-40
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• 2006

This paper presents a novel surface acoustic wave (SAW)-based pressure sensor, which is composed of single phase unidirectional transducer (SPUDT), three reflectors, and a deep etched substrate for bonding underneath the diaphragm. Using the coupling of modes (COM) theory, the SAW device was simulated, and the optimized design parameters were extracted. Finite Element Methods (FEM) was utilized to calculate the bending and stress/strain distribution on the diaphragm under a given pressure. Using extracted optimal design parameters, a 440 MHz reflective delay line on 41o YX LiNbO3 was developed. High S/N ratio, shan reflection peaks, and small spurious peaks were observed. The measured S11 results showed a good agreement with simulated results obtained from coupling-of-modes (COM) modeling and Finite Element Method (FEM) analysis.

• Journal of Drive and Control
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• v.16 no.3
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• pp.59-66
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• 2019

Hydraulic systems are essential for most of the construction equipments due to their various advantages, such as very powerful, quick response speed, precision control and remote control. Moreover, they are necessary to apply the electro hydraulic systems for precise and remote controls. Operating the small electronic joystick of the remote controller for the control of a multipurpose work machine with remote control technology increases the possibility of a sudden operation compared to the use of a conventional hydraulic joystick. When a joystick is suddenly operated, the peak pressure is generated in the system due to the quick response of the system. Then a vibration is generated due to the peak pressure, which causes instability to the operation of the construction equipment. Therefore, in this study, we confirmed the level of reduction of peak pressure occurring in the electro hydraulic system by using AMESim, when the output signal of the step shape generated by the sudden operation of the electronic joystick was changed by using the convolution operation.

• Resources Recycling
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• v.26 no.1
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• pp.22-29
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• 2017

When the ambient air pressure was $0.1kg/cm^2$, there were few spherically formed droplets, which showed very badly fragmented state. The average particle size of the particles constituting the droplet was about 40 nm. When the air pressure increased to $0.5kg/cm^2$, the ratio of the spherical droplet forms increased, but still showed a state of severe disruption. The average particle size of the particles was reduced to about 35 nm. As the air pressure increased to $3kg/cm^2$, the ratio of spherical droplet form significantly increased, the degree of fragmentation even further decreased and the average particle size decreased to 30 nm. When the air pressure increased from 0.1 to $1kg/cm^2$, the XRD peak intensity showed little change, but the specific surface area was decreased. As the air pressure increased to $3kg/cm^2$, the intensity of XRD peaks showed a little decrease, while the specific surface area increased.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2010.06a
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• pp.387-387
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• 2010

최근 ZnO 박막은 투명 박막, 태양전지, LED 등으로의 응용을 위한 새로운 기능성 박막으로 활발히 연구되어 지고 있다. ZnO 기반의 투명 박막 트랜지스터는 상온에서 증착 가능하여 유리기판을 이용한 광학소자와 플라스틱 기판을 이용한 플럭서블 소자 같은 차세대 전자소자를 구현 할 수 있다. 본 연구에서는 RF Magnetron Sputtering System을 이용하여 coming 1737 유리기판 위에 ZnO 박막을 공정압력에 따라 증착하고, 투명 반도체에 적합한 활용을 위한 구조적, 광학적 분석을 실시하였다. 박막 증착 조건은 초기 압력 $1.0{\times}10^{-6}$Torr, RF 파워는 100W, Ar 유량은 100sccm, 그리고 증착온도는 상온이었다. 증착 압력은 $7.0{\times}10^{-3}$, $2.0{\times}10^{-2}$, $7.0{\times}10^{-2}$Torr로 변화시켰다. 표면 분석 (SEM, AFM) 결과 증착압력이 고진공으로 변화함에 따라 결정립들이 감소하였고 RMS roughness값이 낮아졌다. 그리고 XRD 분석을 통해 피크강도는 증가하고 FWHM은 감소함을 보이고 있는데 이는 결정성이 좋아짐을 나타낸다. 그리고 광학 투과도를 통해 가시광 영역에서의 높은 투과도(85% 이상)을 확인하였고, 고진공으로 변화함에 따라 밴드갭이 넓어지는 것을 확인하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.4
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• pp.85-90
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• 2018

The objective of this paper is to observe effects of ignition position and time on ignition transition. A gaseous oxygen and liquid kerosene mixture is used as propellant with a shear-coaxial injector. In order to study the ignition delay time and combustion instability intensity, the pressure transducer was used. Sequences, excepting igniter operation time, were fixed to compare the ignition time only. Initial pressure peak and ignition delay time increased as the ignition time was delayed. Additionally, an unstable flame development zone was detected when the igniter was away from the injector.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2018.06a
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• pp.115-115
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• 2018

철강재는 대량 생산이 가능하며 경제성이 뛰어나고 기계적 성질도 우수하므로 다양한 산업 분야에서 널리 사용되고 있다. 그러나 철강재는 부식 환경에 취약하기 때문에 그 용도에 따라 다양한 내식성을 부여하는 표면처리를 적용하고 있다. 일반적으로 이러한 철강 재료에 대한 내식성 표면처리로는 습식공정을 이용한 아연(Zn)도금 표면처리가 널리 적용되고 있다. 그러나 최근에는 이러한 습식공정으로 인해 발생하는 자원소모 및 환경적인 문제와 더불어 고내식성 표면처리 소재에 대한 수요가 증가함에 따라 이러한 단점을 극복할 수 있는 새로운 소재 및 기술 개발에 대한 관심이 증대되고 있다. 이러한 관점에서 기존의 습식표면처리 공정을 건식으로 대체 또는 병행하고, 현행 아연소재를 대체할 수 있는 코팅소재로써 알루미늄(Al) 이나 마그네슘(Mg)으로 대체하는 방법이 시도되고 있다. 본 연구에서는 강판의 내식성을 향상시키기 위한 방법으로 기존의 습식 표면처리 공정에서 용이하지 않은 마그네슘을 이용하여 건식 PVD 프로세스에 의해 코팅막의 제작을 시도하였다. 그리고 코팅막 제작 조건 중에서 공정압력이 코팅막의 결정배향성에 미치는 영향과 내식성과의 상관관계를 규명하고자 하였다. 즉, 여기서는 강판 및 용융알루미늄 도금강판 상에 스퍼터링법에 의해 Ar 가스에 의한 공정압력을 2, 10 및 50 mTorr로 조절하면서 마그네슘 코팅막을 $2{\mu}m$ 두께로 각각 제작하였다. 이때 제작한 막의 표면 모폴로지 관찰(SEM) 및 결정구조 분석(XRD) 결과에 의하면, 강판 및 용융알루미늄도금강판 상에 제작한 코팅막들은 공통적으로 공정압력이 증가할수록 그모폴로지의 결정립의 크기가 작고 치밀한 구조로 변하였다. 또한 그때 형성된 코팅막의 결정구조는 표면에너지가 상대적으로 높은 Mg(002)면 피크의 점유율이 감소하고 표면에너지가 낮은 Mg(101)면 피크의 점유율이 증가하는 경향을 나타내었다. 그리고 공정압력이 증가할수록 Mg 격자 간 면 간격(d-value)이 증가하는 경향을 나타내었다. 이상에서 제작한 마그네슘 코팅막의 결정성장 과정은 본 진공 플라즈마 PVD 공정중 증착가 더불어 흡착역할을 하는 Ar의 움직임에 따라 설명 가능하였다[1,2]. 코팅막의 양극분극(Polarization)측정 결과에 의하면, 공정압력이 높은 조건에서 제작한 막일수록 부동태 특성이 우수하여 내식성이 향상되는 경향을 나타내었다. 특히, 공정압력이 상대적으로 높은 50 mTorr 조건에서 제작된 코팅막이 표면 마그네슘 결정의 크기가 조밀하고 결정구조는 Mg(002)면과 Mg(101)면의 상대강도 비가 유사하여 내식성 가장 우수하였다.