• Proceedings of the Korean Vacuum Society Conference
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• 2010.02a
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• pp.440-440
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• 2010

$SF_6$ 기체 및 Ar/$SF_6$ 혼합 기체 방전은 실제 반도체 및 디스플레이 공정에서 널리 쓰이고 있지만, 측정상의 어려움으로 인하여 정량적인 데이터 및 기본 연구가 부족한 실정이다. 본 연구는 유도 결합 Ar/$SF_6$ 혼합 기체 플라즈마에서 다양한 압력과 혼합 가스 비율에 따른 전자 에너지 분포 측정을 통한 플라즈마 변수 연구에 관한 내용이다. 낮은 가스 압력에서 $SF_6$ 기체의 혼합 비율이 증가함에 따라서 상대적으로 적은 전자 밀도 감소와 전자 온도의 증가가 보였다. 하지만, 높은 가스 압력에서 $SF_6$ 기체의 혼합 비율이 증가함에 따라 상당한 전자 밀도 감소와 급격한 전자 온도 증가 (~ 9 eV)가 관찰되었다. 이러한 전자 온도와 전자 밀도의 극적인 변화는 $SF_6$ 기체 증가에 의한 전자-중성종 충돌과 음이온 생성으로 인한 것으로 여겨지며, 유체 모델 및 전자 가열 모드를 고려하여 해석하였다.

• Journal of the Korean Society for Marine Environment & Energy
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• v.10 no.4
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• pp.187-192
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• 2007

Impact on cylindrical surface caused by plunging breaking waves is investigated experimentally. The breaking waves are generated in a wave flume by decreasing the wave maker frequencies linearly and focusing the generated wave components at one specific location. The breaking wave packets are based on constant wave steepness spectrum. Three inclination angles of cylinder are applied to examine the effect of contact angle between cylinder and front surface of breaking waves. Also, the effect of cylinder diameter on pressure distribution and its peak value is investigated by adopting three cylinders with different diameters. The longitudinal location of cylinder is slightly moved in eight different points to find out a probable maximum value of impact pressure. The pressures and total force on cylinder surface are measured by piezo-electric pressure sensors and 3-components load cell with 30kHz sampling rate. The variation of peak impact pressures and forces is analyzed in terms of cylinder diameter, inclination angle and location. Also, the pressure distribution on cylindrical surface is examined. The cylinder location and surface position are more important parameters that govern the magnitude and shape of peak pressures, while the cylinder diameter and inclined angle are relatively insignificant. In a certain conditions, the impact phenomenon becomes very unstable which results in a large variation of measured valves in repeated runs.

• Fire Science and Engineering
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• v.12 no.4
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• pp.13-19
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• 1998

We investigated the weight loss according to temperature using Thermal Gravimetric Analysis(TGA) in order to find the thermal hazard of carbon black(Hi-Black 10, Hi-Black 50L) dusts, and the properties of dust explosion in variation of the surface functional groups and specific surface area of their dust with the same particle size. Using Hartman's dust explosion apparatus which estimate dust explosion by electric ignition after making dust disperse by compressed air, dust explosion experiments have been conducted by varying concentration and size of carbon black dust. The explosion pressure of both carbon black increased as the specific surface area increased. The results indicated that Hi-Block 50L of which specific surface area was larger three to four times than that of Hi-Black 10 was much easier of dust explosion.

• Journal of the Korean Society of Propulsion Engineers
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• v.3 no.3
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• pp.53-61
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• 1999

Impinging jets are observed when exhaust gases from missiles or V/STOL aircrafts impinge on the ground, flame deflector, ship deck, etc. The flow shows different patterns according to the nozzle geometry, nozzle-to-plate distance, and plate angle, for example. This paper describes experimental works on the phenomena (pressure distribution, occurrence of stagnation bubble, and so on.) when underexpanded supersonic jets impinge on a perpendicular flat plate using a supersonic cold-flow system, and compares the results with those obtained using a shock tunnel. The flow characteristics for the supersonic cold-flow system were also investigated. Surface pressure distribution of supersonic cold-flow system differed from that of shock tunnel because of water and temperature in the low-pressure chamber. Surface pressure distribution as to underexpanded ratio showed similar patterns together.

• Journal of the Korean Society of Propulsion Engineers
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• v.12 no.5
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• pp.1-8
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• 2008

Dual-mode Phase Doppler Anemometry (DPDA) was used to scrutinize the spatial distribution characteristics of spray emanating from a small Liquid-Rocket Engine (LRE) injector. Droplet size and velocity were measured according to the variation of injection pressure along the plane normal to the spray stream and then the spray characteristic parameters such as Arithmetic Mean Diameter (AMD), Sauter Mean Diameter (SMD), number density, span of drop size distribution, and volume flux were deduced for an investigation of spray breakup characteristics. As the injection pressure increases, the number density, span, and volume flux of spray droplets become higher, whereas the AMD gets smaller.

• Journal of the Korean Society of Marine Environment & Safety
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• v.12 no.4 s.27
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• pp.267-272
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• 2006

Butterfly valves have been used for shut-off and throttling-control application in many industrial fields. Recently, they are frequently used for cooling water, oil system and ballast piping system of many larger vessels. They are especially suited for flow throttling control of heat exchangers in engine room. Measurement by the PIV(Particle Image Velocimetry) was conducted to investigate the flow characteristics of butterfly valve inserted within circular pipe. Flow behaviors such as instantaneous and time-mean velocity vectors are investigated. Furthermore, to reveal systematic performance of the butterfly valve, wall pressure was measured at 6 points along the pipe by digital manometer. As the valve position moves to the closed side, flow separation increases and persists its tendency downstream until smoothly uniform flow developed. The pressure loss is found to be about zero for the disk open angles less than 45 degrees, but is substantially increased for those larger than 60 degrees.

• Journal of the Korean Vacuum Society
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• v.18 no.4
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• pp.272-280
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• 2009

In this study is performed to investigate the pumping characteristics of three-stage disk-type molecular drag pump (DTDP). The experiments are measured using five vacuum pressure gauges in the positions for rotors of DTDP. The experimented DTDP is consisted of three rotors and four stator. In the DTDP, spiral channels of three rotors are cut on the both upper surface and lower surface of a rotating disk, and corresponding stator is a planar disk. The experiments are performed in the outlet pressure range of $0.2{\sim}533\;Pa$. The pressure of each rotors are measured under the various condition of outlet pressure and throughputs, and nitrogen gas is used for test gas. In the numerical study, the pumping characteristics of each rotor are studied for the variation of throughputs in the all rotating channel. Pressure contour and velocity are obtained by the numerical simulation.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1995.11a
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• pp.105-109
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• 1995

본 연구에서는 수치모사로 부터 단위 전지 양극가스내 질소 조성과 각 가스의 순환에 따른 단위전지내의 온도분포 및 성능변화를 구하였다. 양극가스내 질소의 영향은 냉각효과로 나타났고 순환비가 증가할수록 전지내의 온도와 전지의 성능은 감소하였다. 작동압력이 증가할수록 전지의 성능은 증가하였고, 기전력변화 대 압력의 상용대수변화의 직선의 기울기는 문헌상의 실험치와 유사하게 나타났다.

• Proceedings of the Korean Vacuum Society Conference
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• 2010.02a
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• pp.439-439
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• 2010

다양한 가스 방전에서의 전자에너지 분포함수 측정을 통하여 E-H mode 전이에 대한 연구를 하였다. 단원자 가스 방전에서는, 압력이 증가함에 따라 E-mode에서 H-mode로의 전이를 위한 인가 파워는 크게 바뀌지 않았다. 하지만, 다원자 가스에서는 압력이 증가함에 따라 상당히 높은 인가 파워가 필요하였다. 이것은 다원자 가스에서 압력이 증가함에 따라, 해리, 진동 및 회절 운동, 그리고 음이온 생성으로 인한 플라즈마 밀도의 감소에 의한 것이다. 그에 따라, H-mode 전이를 위한 충분한 플라즈마 밀도를 생성하기 위해서 더 큰 인가 파워가 필요하게 된다. 이러한 연구는 혼합가스에서도 측정하였다.

• Proceedings of the Materials Research Society of Korea Conference
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• 2011.05a
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• pp.50.2-50.2
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• 2011

자동차용 CNG 연료탱크의 복합재료 중앙부 표면에 150 kHz 공진형 음향방출센서를 부착하고, 물을 매질로 하여 용기의 내압을 단계적으로 상승시켜 가면서 각 단계에서 일정시간 압력을 유지시키고 그 때 발생하는 음향방출신호를 획득하였다. 이 때 획득한 음향방출신호의 amplitude, count, duration 및 risetime 등과 같은 음향방출 변수들의 분포를 살펴본 결과 복합재료 압력용기의 손상메커니즘을 추정하고 손상정도를 평가하는데 유용하였다.