• Journal of Advanced Marine Engineering and Technology
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• v.33 no.2
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• pp.272-281
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• 2009

The effect of swirl on the flow characteristics in a sudden expansion tube was examined experimentally by using 3D PIV(particle image velocimetry) to capture the velocity profiles. The swirling flow of water through a sudden 1:2 axisymmetric expansion has previously been studied experimentally within a horizontal round tube. A kind of tangential slot is used as a swirl generator for swirling flow and a honey comb is used for without swirl flow. The work with the swirl and without swirl results are compared to each other at the same Reynolds number. Liquid crystal was employed to measure temperature profiles and heating coil used for heat transfer with and without swirl flow. And then the Nusselt number ratoes(Nu/Nudb) are calculated along the test section.

• Journal of Korean Electronics
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• v.2 no.8
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• pp.32-36
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• 1982

• Proceedings of the KSEE Conference
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• 2004.08a
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• pp.127-149
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• 2004

건설교통부 표준발파패턴 중 암파쇄굴착공법(pattern-1)에 해당하는 구간에서 적용할 수 있는 공법중의 하나로서 새로운 물질과 반응촉발장치를 이용하는 파암공법이다. 본 공법에 대한 이해를 돕기 위해 새로운 물질의 특성시험, 파암진동과 발파진동과의 비교 고찰하고, 각종 화약류와의 폭발소음을 비교분석 하였으며, 본 공법을 파암현장에 적용함에 있어 암질에 따른 설계기법 및 시공방법 등에 대해 연구하였다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.13 no.10
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• pp.4884-4890
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• 2012

In this dissertation, the shrinkage and durability of shotcrete were examined. Analysis and comparison of shrinkage against the strength of shotcrete was investigated after performing actual shotcrete shooting for each mix of different percentage of expansive agent. The research on restrained shrinkage with different percentages of expansive agent used (3%, 7%, 11% and 15%) shows that the maximum shrinkage in all samples occurred in between 13-15 hrs after shotcrete shooting. And it is noticed that increasing the percentage of expansive agent can lower the shrinkage. And hence, the 15% of expansive agent not only lowered the shrinkage But it also lowered the strength.

• Journal of the Korean Society of Propulsion Engineers
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• v.23 no.1
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• pp.61-70
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• 2019

A primary investigation on the underexpanded flow generated in a 0.4 MW class high enthalpy supersonic arc-heated plasma wind tunnel is conducted experimentally. The diameter and the position of the Mach disk from the nozzle exit is measured for overall pressure ratios ranging from 200 to 30. The empirical correlations for Mach disk diameter and position are determined which show very good agreement with experimental results.

• Proceedings of the Korean Vacuum Society Conference
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• 2012.02a
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• pp.221-221
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• 2012

최근 진공 산업은 반도체 산업의 급속한 발전과 더불어 진공 산업이 핵심기술로 부각되고 있으며, 진공 산업의 발전이 고부가가치를 창출하는 산업으로 발전하고 있는 추세이다. 이에 (유)우성진공 기술연구소에서는 국내에서 개발이 전무한 소형급 600l/min. 급의 배기속도를 가지는 공랭식 건식진공펌프 개발과 더불어 중소기업 혁신기술 개발사업의 성공적인 수행으로 인해 상용화 단계에 있다. 본 연구에서는 소형(600l/min. 급) 공랭식 건식진공펌프에 개발 과정 및 성능에 대해 소개하고자 한다. 우선, 여타 건식진공펌프와는 달리 냉각방식이 수냉식이 아니라 공랭식 이라는 점에서 에너지 절감 및 설치 공간 제약이 없으며, 유지 비용을 절감할 수 있는 장점을 가지며, 국내에서는 소형급의 건식진공펌프가 없는 관계로 시장성을 높게 평가하고 있다. 소형급 공랭식 건신진공펌프의 냉각효율을 고려하여 하우징을 알루미늄 합금으로 제작을 하였으며, 냉각핀을 적절하게 배치하여 압축열을 효과적으로 방출하기 위한 구조가 될 수 있도록 설계하였고, 냉각팬에 의한 공랭효과를 극대화하기 위해 펌프 스킨을 사용하여 공기 유로를 형성토록 하였다. 또한, 루츠의 형상 및 각 단의 압축효율을 고려한 최적의 로터를 설계하기 위해 Involute Curve를 이용한 3-Lobe형 로터를 설계하였으며, 로터와 로터간의 Clearance를 유지 할 수 있도록 설계하였다. 향후 최적화된 로터 설계기술과 이형재질(알루미늄과 주철)간 열팽창이 고려된 적절한 clearance 유지기술을 적용하여 안정적인 배기속도 600l/min.와 도달진공도 0.005 torr를 가지는 소형 공랭식 건식드라이펌프를 상용화 하고자 한다. 또한 성공적인 과제 종료 및 기술 개발에 따라 건식진공펌프 시장에 신기술 개발 확산에 따른 기업들 간의 기술 경쟁력 촉진을 통한 국가 기술력 향상을 기대해 볼 수 있다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.11a
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• pp.137-142
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• 2008

Ignition characteristics of combustion chamber with LOx lead cyclogram for liquid rocket engine were described. The combustion chamber has chamber pressure of 60 bar, propellant mass flow rate of 89 kg/s, and nozzle expansion of 12. Cold flow test to determine the filling time of propellant for cyclogram with LOx lead supply, ignition test to check the ability to ignite starting fuel from the ignitor, low pressure combustion test to check the propagation of flame into main fuel-oxidizer mixture from starting fuel and the main combustion stage, and design point combustion test to check the combustion performance were performed. Ignition and combustion tests with LOx lead supply were successfully performed and the stable cyclogram of start sequence for combustion chamber was developed.

• Restorative Dentistry and Endodontics
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• v.33 no.2
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• pp.115-124
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• 2008

The purpose of this study was to measure the polymerization shrinkage and hygroscopic expansion of resin-based temporary filling materials and to evaluate microleakage at the interface between the materials and cavity wall. Five resin-based temporary filing materials were investigated: Fermit (Vivadent), Quicks (Dentkist), Provifil (Promedica), Spacer (Vericom), Clip (Voco). Caviton (GC) was also included for comparison. Polymerization shrinkage of five resin-based temporary filling materials was measured using the bonded disc method. For the measurement of hygroscopic expansion, the discs of six cured temporary filling materials were immersed in saline and a LVDT displacement sensor was used to measure the expansion for 7 days. For estimating of microleakage, Class I cavities were prepared on 120 extracted human molars and randomly assigned to 6 groups of 20 each. The cavities in each group were filled with six temporary filling materials. All specimens were submitted to 1000 thermocycles, with temperature varying from $5^{\circ}C/55^{\circ}C$. Microleakage was determined using a dye penetration test. The results were as follows: 1. Fermit had significantly less polymerization shrinkage than the other resin-based temporary fill ing materials. Fermit (0.22%) < Spacer (0.38%) < Quicks (0.64%), Provifil (0.67%), Clip (0.67%) 2. Resin-based temporary filling materials showed 0.43-1.1% expansion in 7 days. 3. Fermit showed the greatest leakage, while Quicks exhibited the least leakage. 4. There are no correlation between polymerization shrinkage or hygroscopic expansion and microleakage of resin-based temporary filling materials.

• Transactions of the Korean Society of Mechanical Engineers
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• v.18 no.4
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• pp.903-911
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• 1994

This study addresses the phenomena of bubbling, icing, eruption, component varieties of the evaporated natural gas, and volumetric heat transfer coefficients obtained during the operation of a proposed LNG evaporator between LNG and water in direct contact. In the present investigation, the explosive and eruption phenomena within the water column were not observed during the entire operation of the heat exchanger. Compared with the natural gas produced by conventional LNG evaporator, the analysis of the gas produced by the direct contact LNG evaporator shows that nitrogen, methane, and ethane components were reduced by 0.002~0.007mol%(4~14%), 1.6~1.92mol%(1.9~2.3%) and 0.17~1.28mol%(1.1~8.4%) respectively, while the moisture content was rather increased by 0.51~0.76mol%. The maximum volumetric heat transfer coefficient of the direct contact heat exchanger was found to be $21, 800kW/m^3\cdotK$.

• Journal of Advanced Marine Engineering and Technology
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• v.18 no.4
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• pp.94-101
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• 1994

실험 데이터는 급확대비 3:1 팽창의 시험관에서의 실험결과를 나타내고 있으며, 실험에 이용된 동작유체로써는 공기가 사용되었다. 입구관에서 레이놀즈수는 60,000으로부터 120,000까지 변하게 하였고, 스월강도는 0으로부터 16까지 변화되게 하였다. 균일한 열 플럭스 경계조건이 사용되었는데, 그 결과 관벽온도 및 체적온도는 24$^{\circ}C$로부터 71$^{\circ}C$까지에 걸쳐 나타났다. 플롯상에 국소 Nusselt수는 최대 열전달점에서 정점을 이루는 모습을 보여 주고 있다. 스월강도가 0으로부터 최대값으로 증가 되었을때, 최고 Nusselt수의 위치는 시험관에서 4로부터 1스텝 하이트로 변경되는 것이 조사되었다. 이러한 최대 Nusselt수의 상류부 이동은 완전 발달된 유동에서의 값보다 2.2배에서 8.8배나 많은 그의 크기를 증가시킨다고 할 수 있다.