• 한국전산유체공학회:학술대회논문집
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• 2008.10a
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• pp.302-307
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• 2008

The development technology for the helicopter is improved by the increasing of computing power and advanced test facilities. The increasing efficiency of fuel consuming by the developing of improved lift-to-drag rotor system is the major issue, the noise reduction for ecology(civil area) and increase of survivability to reduce noise detection(battlefield) also are important. This investigation shows the classification of helicopter external noise and requirements, the noise flight test methods, the numerical modeling method for aero-acoustic of rotor blade and the result of CAA(Computational Aero-Acoustic) for main rotor blade.

• Proceedings of the Korean Vacuum Society Conference
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• 1999.07a
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• pp.247-247
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• 1999

새로운 형태의 고출력 마이크로웨이브 발진장치인 가상 음극 발진기(Virtual Cathode Oscillator)를 이용하여 음극(Cathode)의 크기를 변화시켜 가면서 출력을 측정하였다. 측정된 출력을 전산모사의 결과를 토대로 재해석하였고, 우리가 보유한 천둥 장치에서의 최고출력을 얻을 수 있는 음극 크기를 측정하여 전사모사의 결과와 비교를 하였고, 그에 따른 주파수를 계산을 하고 전산모사를 통해 확인하였다. 본 실험을 하기 위해 본 실험실이 제작한 천둥 장치의 조건(300kV, 20kA)을 사용하였고, 음극은 탄소를 사용하였고, 전자빔의 형탠는 Solid 빔을 사용하였다. 전에 발표했던 전산모사 내용을 실험을 통해 파원(~수 GW)와 에너지 변환효율(~10%), 그리고 주된 동작 주파수등을 계산했다. 본 실험실이 보유한 천등 장치에서 수 GW급의 출력을 얻기 위해 입력 전압에 따른 변화를 전산모사하였다. 이와같은 가상 음극 형성을 위한 다이오드 구조에 따른 Vircator 출력의 경향을 관찰하였다.

• 한국전산유체공학회:학술대회논문집
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• 2011.05a
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• pp.173-178
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• 2011

Nowadays, SELENE-2 is under development for the moon explorer rover in Japan. AXS(Active X-ray Spectrometer) sensor development among the candidated payloads will be on going by the world-wide co-operation. The thermal design, analysis and test will be specially performed by Korean institutes. CFD techniques are used for the conceptual design and analysis. Thin-shell plate meshes being applied by Monte-Carlo Ray Tracing Method are generated for the thermal radiation analysis. Lumped capacity model is employed for the thermal conduction simulation of the AXS payload itself. Various shapes of the payload configuration with thermal boundary conditions are proposed and selected on the purpose of the analysis of the initial design. The results of the analysis are supposed to be used as the baseline for the further detailed design of the AXS payload in the future.

• Computational Structural Engineering
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• v.10 no.2
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• pp.5-12
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• 1997

최근 지진에서 발생한 건물의 손상을 살펴보면, 지진하중을 받는 건물의 3차원 거동에 의해서만 설명할 수 있는 경우가 많이 있다. 특히, 비대칭의 평면을 가지는 건물에서 발생하는 비틀림 거동은 2차원 모델로는 파악하기가 어렵기 때문에 구조물과 개별 부재의 3차원 거동을 보다 정확히 이해함으로써 구조물의 내진능력을 더 정확히 평가할 수 있다. 이를 위해서는 3차원 모델에 의한 비탄성 동적해석이 필요하게 된다. 현재, 전산기의 발달과 더불어 많은 자유도를 요구하는 3차원 구조물의 비탄성해석이 가능해지고, 구조부재의 비탄성거동에 관한 많은 실험으로 다양한 구조부재의 모델이 개발되어 지진에 대한 건물의 설계시 개인용 컴퓨터를 사용하여 이러한 3차원 비탄성 동적해석의 반영이 가능하게 되었다. 실제로 지진이 많이 발생하는 국가에서는 비탄성해석에 대해 많은 연구들이 진행되고 있으며, 일부 국가에서는 건물의 내진설계시 강진에 대한 비탄성해석을 요구하고 있다. 이 글에서는 삼성건설 기술연구소에서 도곡동 102고층 건물의 해석에 사용하였던 3차원 비탄성 동적해석 프로그램인 CANNY-E에 대하여 그 구성과 특징을 소개하고자 한다.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.21 no.6
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• pp.589-596
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• 2008

This study introduces the design of a bi-directional damper using a tuned mass damper(TMD) and a tuned liquid column damper(TLCD) and presents experimental verifications to confirm its control performance. The damper used in this study behaves as a TMD in a specific translational direction and acts as a TLCD in the other orthogonal direction. First, shaking table test is performed to investigate the coupled effect of control forces produced by TMD and TLCD. Then, the parameters that affect to dynamic characteristics of the proposed damper are quantitatively evaluated based on the experimental results. Testing results shows that the damper used in this study produces control forces coupled by TLCD and TMD, as it is excited by waves with an incident angle. Also, it is observed that the damper can be used to reduce bi-directional responses of building structures.

• NEWSLETTER 전기공업
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• no.95-17 s.138
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• pp.34-37
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• 1995

• The KSFM Journal of Fluid Machinery
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• v.11 no.2
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• pp.71-76
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• 2008

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.3 no.1
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• pp.13-17
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• 1974

• Proceedings of the Korean Radioactive Waste Society Conference
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• 2016.10a
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• pp.479-480
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• 2016

• Clean Technology
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• v.21 no.3
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• pp.191-199
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• 2015

The SO_x emission from the ship diesel engines will do a negative influence to the human health and the environment. To reduce the negative environmental effect of the SO_x emission caused by the high traffic of ship movements, the SECA (SO_x emission control area) has been set on several province around world to carry out the severe emissions control and to meet the emissions control standard. To cut down the SO_x emission from the ships, the wet type scrubber is being used widely. In this work, we prepared a numerical model to simulate the spray type scrubber to study the motion of liquid droplets in the flow of the scrubber. For the analysis, the CFD (computational fluid dynamics) method was adopted. As a special topic of the study, we designed the wave plate type of mist eliminator to check the carry over of the uncontrolled water droplet to the exhaust. Numerical analysis is divided into two stages. At the first stage, the analysis was done on the basic scrubber without the mist eliminator, and then the second stage of analysis was done on the scrubber with the mist eliminator on several condition to check and compare with the basic scrubber. On the condition of the basic scrubber, 42.0% of the distributed water droplets were carried over to the exhaust. But by adding the designed droplet eliminator at the exhaust of the scrubber, only 3.4% of the distributed water droplets supplied to the scrubber was emitted to the atmosphere.