• Journal of the Korean Society of Propulsion Engineers
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• v.21 no.5
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• pp.37-45
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• 2017

Extinguishment of a burning solid propellant is difficult, however, dynamic extinction can be induced by fast depressurization in combustion chamber. This paper describes experimental results for the characteristics of extinguishment for composite solid propellants by rapid depressurization. For various composition of solid propellants, depressurization ratio which can induce extinguishment of combustion was obtained using experimental apparatus with rupture disk. Experimental results showed that particle size of oxidizer, mixing ratio of oxidizers with different particle size and contents of metal fuel can affect on the characteristics extinguishement for solid propellant.

• Journal of Oral Medicine and Pain
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• v.23 no.4
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• pp.433-445
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• 1998

본 연구는 정상인의 저작근에서 지속적인 등척성 수축후 근전도 power spectrum과 압력통각 역치의 회복 특성을 구명하기위해 시행되었다. 악안면 영역의 동통과 긴으장애의 벙력 및 현증이 ㅇ벗고 정상적인 교합관계를 가진 26명의 정상인(남자 14명, 여자 12명) 을 대상으로 최대근활성도의 70% 수준에서 인내가능 할 때까지의 등척성 수축과 수축후 회복기 동안의 근전도 power spectrum과 압력통각 역치를 컴퓨터를 이용한 근전도 시스텀과 전자식 압력통각계를 사용하여 분석한 결과 다음과 같은 결론을 얻었다. 1. 지속적인 등척성 수축 시작 시점의 중간주파수에서 남녀간에는 통계적으로 유의한 차이가 관철되지 않았지만, 근육간 비교에서는 전측두근에서 교근보다 유의하게 높게 나타났다(p<0.05). 2. 지속적인 등척성 수축전 암력통각 역치는 전축두근에서 교근보다 유의하게 높았고(p<0.001), 남성에서 여성보다 유의하게 높게 나타났다(p<0.05). 3. 지속적인 등척성 수축시 중간주파수와 압력통각 역치의 변화량은 성별간, 근육간에 우의한 차이가 관찰되지 않았다. 4. 지속적인 등척성 수축말기 중간주파수는 수축초기에 비하여 유의하게 감소하였으며(p<0.001), 이의 회복은 모든 근육에서 60초와 120초 사이에서 이루어 졌다. 5. 지속적인 등척성 수축후 압력통각역치는 수축전에 비해 유의하게 감소하였으며(p<0.001), 수축전 수준으로의 회복은 여자군의 전측두근과 교근에서는 30분후에 남자구느이 전측두근과 교근에서는 50분 후에 이루어졌다. 6. 지속적인 등척성 수축후 주관적인 동통이 소실된 시각은 여자군의 전축두근에서는 28분, 교근에서는 42분으로 남자군의 전측두근에서는 30분, 교근에서는 40분으로 나타났다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.38 no.10
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• pp.797-805
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• 2014

The purpose of this study was to investigate the drag and lift characteristics of the cavitator of a supercavitating underwater vehicle and the pressure loss due to water intake. These investigations were performed by changing the diameter, velocity, radius of curvature of the intake, and angle of attack of the cavitator. With increasing ratio of the intake diameter to the cavitator diameter ratio($d/D_1$), the drag coefficient and the pressure loss coefficient of the water intake decreased. The greater the increase in the ratio of the intake velocity-to-free stream velocity ratio(S), the smaller was the decrease in the drag coefficient and the lift coefficient. When the intake had a radius of curvature(c), the pressure loss coefficient decreased. On the contrary, the effect of the radius of curvature on the drag coefficient was imperceptible. For angles of attack (${\alpha}$) of the caviatator in the range of $0^{\circ}$ to $10^{\circ}$, the drag coefficient and the pressure loss coefficient changed slightly, whereas the lift coefficient increased linearly with increasing angle of attack.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.363-366
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• 2006

The effectiveness of two passive control techniques for alleviating the pressure oscillation generated in a supersonic cavity flow is investigated numerically. The passive devices suggested in the present research include a triangular bump and a sub-cavity installed near the upstream edge of a rectangular cavity. The supersonic cavity flow characteristics are examined by using the three-dimensional, unsteady Wavier-Stokes computation based on a finite volume scheme. Large eddy simulation (LES) is carried out to properly predict the turbulent features of cavity flow. The results show that the pressure oscillation near the downstream edge dominates overall time-dependent cavity pressure variations. Such an oscillation is attenuated more considerably using the sub-cavity compared with other methods, and a larger sub-cavity leads to better control performance.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.4
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• pp.53-62
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• 2006

Two-dimensional steady flowfields generated by transverse injection jets into a supersonic mainstream are numerically simulated. Fine-scale turbulence effects are represented by a k-${\omega}$ SST two-equation closure model which includes $y^+$ effects on the turbulence model. Solution convergence is evaluated by using Grid Convergence Index(GCI), a measure of uncertainty of the grid convergence. Comparison is made with experimental data and other turbulence models in term of surface static pressure distributions, the length of the upstream separation region, and the penetration height. Results indicate that the k-${\omega}$ SST model correctly predicts the mean surface pressure distribution and the upstream separation length for low static pressure ratios. However, the numerical predictions become less consistent with experimental results as the static pressure ratio increases. All these results are taken within 1% error band of grid convergence.

• Korean Journal of Materials Research
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• v.1 no.4
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• pp.177-183
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• 1991

Change of the properties of selective CVD-W by $SiH_4$ reduction with the variation of deposition time and pressure has been investigated. The lime required for covering the who)to Si substrate by tungsten at $300^{\circ}C$ under the pressure of 100mtorr is approximately 30 seconds. The film thickness tends to increase linearly in the early stage of deposition process and parabolically later, sheer resistance of the film tends to decrease rapidly initially, and slowly later with deposition time. Tungsten grain size does not change much, but grain boundary becomes hazy in the pressure range of 50-300mtorr. Also no ${\beta}-W$ but only ${\alpha}-W$ was found in this pressure range. The deposition rate and electrical resistivity of tungsten tend to increase wish increasing pressure. The results of AES analysis show that pressure does not much affect Si/W ratio of the tungsten film and silicidation at the W/Si interface.

• The Journal of the Korea institute of electronic communication sciences
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• v.19 no.1
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• pp.39-46
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• 2024

In this study, GTZO(Ga-Ti-Zn-O) thin films were deposited at various working pressures (1~7mTorr) by RF magnetron sputtering to examine the structural, electrical, and optical properties. All GTZO thin films exhibited c-axis preferential growth regardless of working pressure, the GTZO thin film deposited at 1mTorr showed the most excellent crystallinity having 0.38˚ of FWHM. The average transmittance in the visible light region (400~800nm) showed 80% or more regardless of the working pressure. We could observed the Burstein-Moss effect that carrier concentration decrease with the increase of working pressure and thus the energy band gap is narrowed. Figure of merits of GTZO thin film deposited at 1mTorr showed the highest value of 9.08 × 103 Ω-1·cm-1, in this case resistivity and average transmittance in the visible light region were 5.12 × 10-4 Ω·cm and 80.64%, respectively.

• Journal of the Institute of Electronics Engineers of Korea SD
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• v.47 no.2
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• pp.15-20
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• 2010

In this study, AZO (Al: 3 wt%) thin films have been prepared on PES Plastic substrates at various working pressure (5~20 mTorr), $O_2$ gas flow rate(0~3%) and the fixed substrate temperature of 200 f by using the RF magnetron sputtering and their optical and electrical properties have been studied. The XRD measurement shows that AZO thin films exhibit c-axis preferred orientation. From the results of AFM measurements, it is known that the lowest surface roughness (3.49 nm) is obtained for the AZO thin film fabricated at 5 mTorr of working pressure and 3% of $O_2$ gas flow rate. The optical transmittance of AZO thin films is measured as 80% in the visible region. We observe that the energy band gap of AZO thin films increases with decreasing the working pressure and the $O_2$ gas flow rate. This phenomenon is due to the Burstein-Moss effect. Hall measurement shows that the maximum carrier concentration ($2.63\;{\times}\;10^{20}\;cm^{-3}$) and the minimum resistivity ($4.35\;{\times}\;10^{-3}\;{\Omega}cm$) are obtained for the AZO thin film fabricated at 5mTorr of working pressure and 0% of $O_2$ gas flow rate.

• Electrical & Electronic Materials
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• v.9 no.5
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• pp.490-497
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• 1996

RF마그네트론 스파터링에 의한 $sSnO_2$ 박막을 증착한 결과 작동조건에 따라 표면에서 막손상이 발생하였는데, 이는 target에서 생성된 높은 에너지의 고속입자가 기판에서 직접 충돌로 일어나며, 마그네트론의 자계분포와도 관계된다. 또한 기판의 위치에 따라 박막의 전기적, 구조적 특성이 급격히 변하는데 본 논문은 중심자석의 세기와 RF power, 가스압력, 그리고 기판온도 등의 스파터링 작동조건을 변화시키면서 박막의 비손상을 검토하였고, 물성특성을 평가하였다. 실험결과로 부터 기판의 외축부에서 제작된 박막은 전반적으로 막손상이 없었고, 특히 target의 중심자석을 Cobalt로 설치하고 15 mTorr의 가스압력과 50 W의 RF power로 한 경우 가장 우수한 특성을 가진 박막을 얻을 수 있었다. 추가로 막손상을 방지하고자, 환원형의 masking glass를 target위에 설치하였는데, 고에너지 입자의 직접 충돌을 확실히 차단할 수 있었으며, 비저항율도 target의 부식부위 (erosion)에 대응하는 부분에서 100배 정도로 개선하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2004.10a
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• pp.113-118
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• 2004

Experiments are conducted to get basic information of under-expanded impinging jet in the near field. Experimental parameters are impinging angle and under-expanded ratio. As the under-expanded ratio increases, the maximum surface pressure decreases and the reducing effect of recovery factor increases. As the impinging angle decreases, the peak of surface pressure is displaced slightly from the geometric center of the plate to the upward region and the cooling region is expanded in the downward region, whereas it is contracted in the upward region.