• Electric Engineers Magazine
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• s.125
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• pp.29-35
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• 1993

• Electric Engineers Magazine
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• s.131
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• pp.26-29
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• 1993

• KIPE Magazine
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• v.8 no.2
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• pp.21-26
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• 2003

• Journal of Drive and Control
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• v.13 no.1
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• pp.89-93
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• 2016

• Tunnel and Underground Space
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• v.22 no.1
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• pp.54-59
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• 2012

Deformation of Lead plate blast pressure meter were measured after they were exposed to surface blasting. Blasting pressure was determined by comparing the data with calibration graph which was drawn from the laboratory experiments with gas gun of Hopkinson bar tester. The results were compared with calculated values from the equations of CONWEP (Conventional Weapons Effects Program) and DDESB (Department of Defence Explosives Safety Board). Measured values were lower than calculated values in near field. Gradual decaying tendency of the pressure was observed. It means that estimated blasting pressure of very near field with theoretical equations can be uncertain.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2005.11a
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• pp.220-223
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• 2005

System design parameters of gas generator cycle liquid rocket engines were investigated and compared in the present study. Characteristic velocity of combustor, pressure drop of combustor injector, exit pressure of pump, pump efficiency and specific power of turbine were considered as a system design parameter. The result shows the characteristic velocity is in the range of 1700-1770 m/s, pressure drop of combustor injector, 4-10 bar, pump exit pressure ratio to combustion pressure, 120-230%, pump efficiency, 60-80%, specific power of turbine, $0.28-0.58MW{\cdot}s/kg$.

• Korean Journal of Materials Research
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• v.10 no.1
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• pp.83-89
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• 2000

$Si_3N_4$ powder with 2wt% $Al_2O_3$ and 6wt% $Y_2O_3$ additives was sintered by gas pressure sintering (GPS) technique. The variations in the unlubricated wear behavior depending on sintering time were compared. Tribological properties depending on sintering time are associated with fracture toughness as well as flexural strength of materials. When increasing the sintering time, the larger elongated grains were formed as a result of exaggerated grain growth. As the fracture toughness and flexural strength decreased, the wear volume increased. On the basis of these experimental results, the unlubricated wear properties of silicon nitride were found to be governed mostly by both the fracture toughness and the flexural strength of the material.

• Proceedings of the KIEE Conference
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• 2008.07a
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• pp.1358-1359
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• 2008

HC(hydrocarbon)센서는 최근 내연기관의 과도상태의 연소 효율 및 배기가스 저감 효율을 높이기 위하여 산소센서와 함께 연소제어 분야에서 많이 사용되고 있다. 현제 HC센서는 전기화학식 및 current limiting 방식을 많이 사용하고 있으며 이는 HC가스의 이온화를 유도하는 촉매를 매질로 하는 전기화학식 센서이다. 이러한 촉매의 경우 장기 사용 시 촉매의 열화 및 변형 등으로 신뢰도가 떨어지게 된다. 본 논문에서는 촉매를 이용하지 않고 HC 가스의 이온화를 위하여 고전압 하전방식의 hydrocarbon센서를 고안하였으며[1], 여러 배출가스를 통한 센서의 전기화학적 성능을 분석하였고 온도 및 HC성분에 따른 전류치 변화를 이용하여 이론적 계산식을 제안하였다.

• Aerospace Engineering and Technology
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• v.9 no.1
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• pp.93-97
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• 2010

The analysis of specific impulse of the liquid rocket engine employing gas generator cycle with LOx/kerosene as propellant has been performed. The relative error of performance of 300 ton level engine is 0.1%s for specific impulse and 12% for optimal combustion pressure comparing with the published data. The difference of the performance model and the material property models of gas generator product gas are the presumed major reason of discrepancy. The optimal condition of 30 ton level engine is combustion pressure of 68 bar and mixture ratio of 2.2 for maximum specific impulse. This optimal condition can be changed by performance models.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.05a
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• pp.173-176
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• 2010

A subscale gas generator was designed and manufactured to understand a reason for increased pressure drop of liquid oxygen injectors observed in a technology demonstration model of a 75 ton-class gas generator. A total of 6 hot-firing tests were successfully performed including experimental conditions of design and off-design points. The hot-firing results showed that discharge coefficients of fuel and liquid oxygen remained constant as the mixture ratio varied at a fixed chamber pressure. At a fixed mixture ratio, it was also found that discharge coefficients of fuel and liquid oxygen was constant as the chamber pressure was increased.