• Proceedings of the KAIS Fall Conference
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• 2008.05a
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• pp.299-301
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• 2008

본 논문은 세정용 노즐의 기하학적인 형상을 변화시킴으로써 물과 공기를 이용한 비데용 분사노즐의 세정효과를 극대화하기 위한 연구이다. 세정효과와 절수를 목적으로 과거 물만을 공급되었던 비데노즐에 공기를 물을 혼합한 혼합류를 주입하면서 형성되는 노즐 내부 유동현상을 상용코드인 CFD-ACE+을 이용하여 가시화하고자 했다.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2007.04a
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• pp.97-98
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• 2007

$SiH_4-Ar-O_2$ ICP-CVD에서 증착된 $SiO_2$막의 두께 균일도를 개선시키기 위해 반응가스 주입구의 위치가 두께 균일도에 영향을 주었을 것으로 예상하고, CFD-ACE를 이용하여 2차원 모델링을 하여 최적데이타를 도출하였다.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2012.05a
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• pp.147-147
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• 2012

스퍼터링을 이용한 증착 시스템은 인가된 전력의 대부분이 타겟의 가열에 사용되어 에너지 효율이 낮다는 단점이 있고, 저항 가열을 이용한 증발 증착 시스템은 대전류를 필요로 하고 증발 물질이 보트 물질과 반응하지 말아야 한다는 제약이 있고 질화물을 형성하는 반응성 프로세스에서 증발량을 일정하게 조절하기 어렵다. 두 가지 공정의 장점을 살린 스퍼터-승화 시스템을 고안하고 이를 위한 수치 해석을 CFD-ACE+를 이용하여 실시하였다.

• Journal of Biosystems Engineering
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• v.31 no.4 s.117
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• pp.342-348
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• 2006

Aerial application using an unmanned agricultural helicopter became necessary for both labor saving and timely spraying. In the previous paper, a rotor system was developed and lift capability was evaluated. The experimental results were compared with simulated predictions using the CFD-ACE program. From the simulation, the relative velocity on the top surface of the blade airfoil increased, resulting in the pressure drop. The CFD analyses were revealed that a drag resistance on the leading edge of the airfoil, a wake at the trailing edge, and a positive pressure underneath the bottom surface were observed. As the results of the simulation, total lifts of 56.8, 74.4 and $95.0kg_f$ were obtained at the 6, 8 and $10^{\circ}$ of AAT (angle of attack), respectively. The simulation results agreed reasonably up to $10^{\circ}$ of AAT. However, at a greater AAT $(<12^{\circ})$ the simulated total lift continuously increased to $105kg_f$, comparing with a decreasing experimental total lift due to the lack of engine power. At a stiff angle of $18^{\circ}$ AAT, a wake was observed at the trailing edge of the airfoil. A rated operating condition determined from the previous paper was also verified through the simulation.

• Proceedings of the Korean Vacuum Society Conference
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• 2011.02a
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• pp.280-280
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• 2011

유도결합 플라즈마를 이용한 식각 장치에서 플라즈마 균일도 향상에 대한 수많은 연구가 이뤄지고 있다. 안테나의 디자인, 인가 전력과 주파수, 안테나와 기판간의 거리, 기판과 챔버 외벽간의 거리 등 다양한 변수들이 변화되어 왔다. 또한, 최근에는 식각 균일도뿐만 아니라 식각 속도 향상에도 많은 관심이 모아지면서 유동에 영향을 주는 GDP 구조가 다시 중요해지고 있다. 본 연구에서는 300 mm 식각장치를 형상화하고, GDP의 구조와 유량비에 따라 플라즈마의 균일도에 어떻게 영향을 끼지는지 사용 유체역학 전산모사 프로그램인 CFD-ACE+를 이용하여 예측해 보았다. 안테나는 2중 직렬방식으로 안쪽과 바깥쪽의 안테나에 각기 다른 전력을 인가 할 수 있는 구조를 사용했으며, 압력은 10에서 60 mTorr까지 변화시켰다. GDP의 구조는 안쪽 입구와 바깥쪽 입구가 있으며 역시 따로 유량을 조절할 수 있도록 설계하였다. 안쪽 입구는 수직방향을 향하고 있으며, 바깥쪽 입구는 90도 이내의 각을 갖도록 꺾여 있는 것과 수평방향으로 주입할 수 있는 구조, 두 가지를 사용하였다. 유량 비율은 안쪽 입구와 바깥쪽 입구를 2:8, 5:5, 8:2로 고정하였다. 우선 GDP의 구조가 90이내의 각을 갖도록 주입되는 구조에서는 어떤 유량비율에서도 약간의 vortex가 발생했다. 수직방향의 유량이 감소될수록 기판에서 멀리서 발생했으며 강도 또한 감소했다. 기판 표면에서의 압력분포 균일도도 8:2에서 2.8%, 2:8에서 0.6%로 향상되었다. 2:8의 유량 비율에서 압력을 10에서 60 mTorr까지 향상시키면 vortex 효과는 감소되나 기판에서의 압력 균일도가 0.8%까지 약간 나빠졌다. 여기서 발생되는 vortex는 GDP 구조를 수평방향으로 주입되기 함으로서 해결할 수 있었으며, 압력 균일도도 0.2%까지 향상시킬 수 있었다. 또한, 강한 수직방향의 유량은 중심에 발생하는 플라즈마의 중앙을 밀어내는 효과를 확인했으며, 실험적 증명이 추후 연구단계로 진행될 예정이다. 식각 균일도나 식각 속도를 예측하려면 CF계열의 복잡한 가스를 사용해야하기 때문에 유량이 플라즈마에 미치는 영향을 보기 위해서 본 연구에서는 단일종인 Ar 가스만을 사용하였다. 첫 단계로 이와 같이 최적화시킨 유동조건에서 복잡한 식각가스를 이용한 플라즈마 계산은 다음 단계로 준비 중에 있다.

• Journal of Sensor Science and Technology
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• v.8 no.4
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• pp.320-326
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• 1999

A small cartridge, with a nozzle system for washing off the dirt from the surfaces of sensing gates, was fabricated. The proposed nozzle structure was designed for cartridge by using the simulation tool of fluid (CFD-ACE). Whole size of the fabricated cartridge by using micromachining techniques is about $2.6\;cm{\times}1.5\;cm$, the size of the washing nozzle is $0.2\;mm{\times}0.6\;mm$ and its dead volume is only about $20\;{\mu}l$. A micro-reference electrode was achieved by employing a differential system with ISFETs/QRE (quasi-reference electrode)/REFET (reference field-effect transistor). Metal electrodes was deposited at both ends of blowing channel were used to check the presence of bubble in the microchannel. The pH-ISFET was inserted into the fabricated cartridge and the washing effect of the nozzle system in cartridge was invested.

• Journal of the Korea Society of Computer and Information
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• v.22 no.1
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• pp.63-69
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• 2017

In this paper, we propose a method to optimize the geometry and installation position of the mixer in the selective catalytic reduction (SCR) system by computational fluid dynamic(CFD). Using the commercial CFD software of CFD-ACE+, the flow dynamics of the flue gas was numerically analyzed for improving the injection uniformity of the reduction agent. Numerical analysis of the mixed gas heat flow into the upstream side of the primary SCR catalyst layer was performed when the denitrification facility was operated. The characteristics such as the flow rate, temperature, pressure loss and ammonia concentration of the mixed gas consisting of the flue gas and the ammonia reducing gas were examined at the upstream of the catalyst layer of SCR. The temperature difference on the surface of the catalyst layer is very small compared to the flow rate of the exhaust gas, and the temperature difference caused by the reducing gas hardly occurs because the flow rate of the reducing gas is very small. When the mixed gas is introduced into the SCR reactor, there is a slight tendency toward one wall. When the gas passes through the catalyst layer having a large pressure loss, the flow angle of the exhaust gas changes because the direction of the exhaust gas changes toward a smaller flow. Based on the uniformity of the flow rate of the mixed gas calculated at the SCR, it is judged that the position of the test port reflected in the design is proper.

• Applied Chemistry for Engineering
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• v.30 no.1
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• pp.95-101
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• 2019

The cremation rate of Korea in 2016 was 82.7% which is four times greater than 20.5% in 1994. As increasing the cremation rate gradually, it cause a shortage of cremation facilities resulting in building more cremation facilities to meet the increasing inquiries on cremation or a large amount of fuels for the longer operation of the crematory. In this study, the crematory system optimizing its thermal efficiency characteristics and also responding to increasing inquiries on cremation was proposed in order for solving such problems, In particular, the heat flow characteristics including a heat transfer coefficient by performing a simulation using computational fluid dynamics (CFD) was investigated. The CFD model was validated with on-site experiments for a cremation facility. As a result of the simulation, the fuel consumption decreased nearly 25% and residence time increased in the main combustor. Also, the improved crematory was constructed with an expanded combustor, heat exchanger, second combustion air system, refractory and insulation material. From on-site experiments, the energy consumption was saved to approximately 54.4%, while the burning time reduced nearly 20 minutes.

• Journal of Biosystems Engineering
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• v.37 no.1
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• pp.1-10
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• 2012

Purpose: The most important element of an agricultural helicopter is the rotor blade realizing lift force. In order to improve the performance of the rotor blades, two types (KA152313 and KB203611) of airfoils were designed and compared. Methods: The nose shape of the KB203611 airfoil was 'drooped' and 'sharp' compared to the leading edge of the KA152313 airfoil. The performance of the experimental airfoils was simulated using CFD-ACE program, and lifts were measured in situ using the 'AgroHeli-4G', a prototype helicopter. Results: Simulated lifts of the blade with the KA152313 airfoil showed proper values for a wide range of angles of attack between $14^{\circ}{\sim}18^{\circ}$, while the simulated lift of the KB203611 blade exhibited maximum values near $13^{\circ}{\sim}14^{\circ}$. In the lift measurements, the range of operable angles of attack was a collective pitch angle at the grip (GP) of $12^{\circ}{\sim}18^{\circ}$ for the KA152313 blade. On the other hand, the range of angles of attack for the KB203611 blade was a GP of $12^{\circ}{\sim}14^{\circ}$. Conclusions: The blade of KA152313 performed well over a wide range of AoAs and the blade of KB203611 performed better at low AoAs. In this study, a variative airfoil blade, gradually emerging from grip to tip using the two different airfoils, was suggested.

• 한국전산유체공학회:학술대회논문집
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• 2007.10a
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• pp.115-119
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• 2007

In this paper, a flow visualization analysis has been carried out on an oscillating square section cylinder, numerically, using a commercially available code CFD-ACE. In this study, the square cylinder is forced to oscillate at different frequencies of excitation, viz., fe/fo=0.5, 1.0 and 2.0 (where, fe is the excitation frequency provided to the cylinder and fo is the natural vortex shedding frequency from the stationary cylinder at a particular Reynolds number (=5200). In all the cases, the peak-to-peak amplitude of oscillation is kept at 32% of the side dimension of the square cylinder. These studies are conducted to understand the influence of frequency of oscillation on the flow field features around the cylinder, particularly the mode of vortex shedding. Results indicate that, the flow field around a square cylinder is very much influenced by the excitation frequency, in particular the vortex shedding mode. It is also found that, the vortex street parameters are significantly influence by the oscillation frequency. Comparison with earlier reported experimental studies has also been attempted in this paper. In appears that, such a numerical exercise (as performed in this paper) is first of its kind. It is believed that, these studies would enable one to understand the mechanisms underlying the flow-induced vibrations of a square section cylinder.