• Journal of the Korean Society for Marine Environment & Energy
• /
• v.13 no.2
• /
• pp.91-98
• /
• 2010

The water elevation inside the air chamber and bi-directional air flow in the duct of Oscillating Water Column wave energy converter is one of the most important factors to evaluate the operating performance. The numerical wave tank based on the commercial software Fluent 6.2 in the present paper is employed to generate the incident waves. The numerical wave tank consists of the continuity equations, the Reynolds-averaged Navier-Stokes equations and the two-phase VOF function. The oscillating amplitude of water column in the chamber and bi-directional air flow in the duct installed on the top of the chamber are calculated, and compared with experimental data to verify the validation of the present NWT. The nozzle effects of the chamber-duct system on the relative amplitudes of the inner free water surface and air flow rate in the duct are investigated.

• 한국신재생에너지학회:학술대회논문집
• /
• 2011.05a
• /
• pp.100.2-100.2
• /
• 2011

본 연구과제는 유망상품인 "발전용 MCFC 모듈형 BOP" 중 가습기 내부에 장착되는 연료-물 Mixing 시스템을 개발하는 것이다, 가습기 내부에서 공급된 연료-물은 연료전지 스택(Stack)으로부터 가습기로 유입된 고온의 가스로부터 열을 공급 받아 증발 및 혼합과정을 거치게 되며, 스팀-연료 혼합기로 형성되어 개질기(reformer)로 공급되게 된다. 이때, 물과 연료의 공급 상태에 따라 균일한 스팀-연료 혼합기가 형성되는지가 결정되며, 경우에 따라서는 고온의 가습기 내부의 국부적 온도분포의 큰 차이를 발생시켜 용접부의 균열을 발생시킬 수도 있기 때문에, 가습기의 설계와 함께 중요한 장치로 여겨진다. 본 연구에서는 다양한 가습기에 적용이 가능한 Mixer 모델을 설정하고, Analytic calculation을 통한 노즐설계와 1pass/Full scale 성능 실험 장치를 통해 상용화를 목표로 추진 되었으며, 특히 노즐별 유량분배 변동율은 ${\pm}3%$ 이내로 달성하고, 스팀/연료 공급 비율은 2:1 이내로 달성할 수 있는 시스템을 구축하게 될 것이다. 최종적으로 개발 완료 시 다양한 가습기에 직접 장착하여 운전이 가능할 수 있도록 실용화에 중점을 두고, 보다 안정적인 성능을 나타낼 수 있는 제품 개발이 가능하리라 사려된다.

• Proceedings of the Korean Vacuum Society Conference
• /
• 2011.02a
• /
• pp.160-160
• /
• 2011

I-III-VI족 화합물 반도체인 $CuInS_2$(CIS) 박막은 Cu(In,Ga)$Se_2$에 비해서 독성원소를 사용하지 않으므로 환경 친화적이고 Ga, Se를 사용하지 않아 조성의 조절이 쉬우며 태양전지의 이상적인 밴드갭인 1.5 eV에 근접한 1.53 eV의 직접천이형 에너지 밴드갭을 가지고 있어 태양전지의 광흡수층으로써 유망한 재료이다. CIS 박막 증착에는 다양한 방법이 있으며 본 연구에서는 chamber를 진공으로 만들고 CIS를 구성하는 용액으로부터 미립자화 된 입자를 노즐을 통하여 팽창시켜 에어로졸을 생성하고 입자들의 운동에너지를 증착에 직접 이용 할 수 있는 Aerosol Jet Deposition (AJD)라는 방법을 이용하려고 한다. 이 방법은 높은 증착속도로 우수한 박막을 성장시킬 수 있는 저비용 및 단순공정으로 CIS를 증착 할 수 있는 새로운 방법이다. 물을 용매로 하여 수용액 상태의 $CuCl_2{\cdot}2H_2O$, $InCl_3$, $(NH_2)_2CS$를 혼합하여 CIS 용액을 제조하고 carrier gas를 주입하여 CIS 용액을 노즐로 이동시켜 팽창시킨다. 용액이 팽창되면서 온도가 감소하여 응축이 일어나며 이 응축된 용액이 가열된 기판 위에 충돌하여 용매가 증발하면서 결정화된 CIS가 증착이 된다. CIS의 특성은 용액의 전구체 비율, 기판 온도, 팽창 전 압력, chamber 압력 등의 영향을 받는데 본 연구에서는 기판 온도를 증착변수로 선택하여 CIS 박막을 증착하고 박막의 특성을 고찰하고자 한다.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.23 no.4
• /
• pp.10-20
• /
• 2019

Recently, fluidic thrust vector control has become a core technique to control multifarious air vehicles, such as supersonic aircraft and modern rockets. Fluidic thrust vector control using the shock vector concept has many advantages for achieving great vectoring performance, such as fast vectoring response, simple structure, and low weight. In this paper, computational fluid dynamics methods are used to study a three-dimensional rectangular supersonic nozzle with a slot injector. To evaluate the reliability and stability of computational methodology, the numerical results were validated with experimental data. The pressure distributions along the upper and lower nozzle walls in the symmetry plane showed an excellent match with the test results. Several numerical simulations were performed based on the shear stress transport(SST) $k-{\omega}$ turbulence model. The effect of the momentum flux ratio was investigated thoroughly, and the performance variations have been clearly illustrated.

• KSBB Journal
• /
• v.25 no.4
• /
• pp.379-386
• /
• 2010

In the present study, biocompatible poly (ethylene glycol) (PEG) microparticles containing coriander essential oil were prepared using a supercritical particles from gas saturated solution (PGSS) process to improve the stability of the coriander oil. The effects of various process parameters such as temperature, pressure, and nozzle diameter on the morphology and entrapment efficiency of coriander oil loaded PEG microparticles were then investigated. A positive influence on the formation of spherical microparticles was observed with increasing temperature and decreasing pressure. Furthermore, somewhat more porous microparticles were produced with an increase in pressure. At a given temperature, the highest entrapment efficiency of coriander essential oil in PEG microparticles was observed under the lowest experimental pressure condition.

• Applied Chemistry for Engineering
• /
• v.18 no.3
• /
• pp.227-233
• /
• 2007

Carbon/carbon (C/C) composites as unique materials possess exceptional thermal resistance with light weight, high stiffness, and strength even at high temperature. However, one serious obstacle for application of the C/C composites is their poor oxidation resistance in high temperature oxidizing environments. SiC coating has been employed to protect the composites from oxidation. This study explored combustion characteristics of 4-directional (4D) carbon/carbon composites using liquid fuel rocket engine to investigate ablative motion of the materials. C/C composites were made of coal tar pitch as a matrix precursor, and heat-treated at $2300^{\circ}C$. Throughout repeated densification process, the density of the material reached $1.903g/cm^3$. After machining 4D C/C composites, the nozzle surface was coated by a SiC layer by pack-cementation method to improve oxidation resistance. Erosion characteristics of SiC-coated C/C composites were measured as function of the ratio of oxygen to fuel. The morphological change of the composites after combustion test was investigated using SEM and erosion mechanism also was discussed.

• Journal of the Korea Academia-Industrial cooperation Society
• /
• v.17 no.7
• /
• pp.641-647
• /
• 2016

A drop-on-demand inkjet is used widely for various applications. Therefore, it is important to understand the jetting behavior of the drop from the piezo inkjet. In this study, to predict the jetting behavior, VOF (Volume-of-Fluid) simulation techniques were used and compared with the experimental results. The experimentally measured meniscus movement was used as the input data for the simulation. To verify the simulation, the measured jetting behavior of the mixture fluids of ethylene glycol and IPA (isopropyl alcohol), which has a mixing ratio of 50:50, was used. The numerical simulation of the drop formation using various mixture ratios and its comparison with the measured drop formation confirmed that the proposed method can predict the actual jetting. On the other hand, the satellite drop behavior showed slight differences because the small sized droplet is subject to a more aerodynamic effect during flight because the kinetic energy of the satellite droplet is far smaller than that of the main droplet.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.18 no.5
• /
• pp.54-61
• /
• 2014

In this study, a plume exhausted from rocket nozzle is investigated by using an unstructured 2-dimensional axisymmetirc DSMC code at various altitude. The small back-pressure to total-pressure ratio($P_b/P_o$) and large $P_b/P_o$ represent low and high altitude condition, respectively. At low altitude, the plume shows a typical complicated structure (e.g. Mach disk) of underexpanded jet while the high altitude plume experiences plain expansion. The various features of exhaust plume is discussed including density, translational/rotational temperature, Mach number and Knudsen number. The results shows that even at 20 km altitude where the freestream Knudsen number is small as $1.5{\times}10^{-5}$, the transitional and rarefied flow regimes can occur locally within the plume. It confirms the necessity of DSMC computation at low altitude.

• Progress in Medical Physics
• /
• v.26 no.1
• /
• pp.12-17
• /
• 2015

The purpose of the Monte Carlo simulation study was to provide the optimized nozzle design to satisfy the beam conditions for biomedical researches in the Korean heavy-ion accelerator, RAON. The nozzle design was required to produce $C^{12}$ beam satisfying the three conditions; the maximum field size, the dose uniformity and the beam contamination. We employed the GEANT4 toolkit in Monte Carlo simulation to optimize the nozzle design. The beams for biomedical researches were required that the maximum field size should be more than $15{\times}15cm^2$, the dose uniformity was to be less than 3% and the level of beam contamination due to the scattered radiation from collimation systems was less than 5% of total dose. For the field size, we optimized the tilting angle of the circularly rotating beam controlled by a pair of dipole magnets at the most upstream of the user beam line unit and the thickness of the scatter plate located downstream of the dipole magnets. The values of beam scanning angle and the thickness of the scatter plate could be successfully optimized to be $0.5^{\circ}$ and 0.05 cm via this Monte Carlo simulation analysis. For the dose uniformity and the beam contamination, we introduced the new beam configuration technique by the combination of scanning and static beams. With the combination of a central static beam and a circularly rotating beam with the tilting angle of $0.5^{\circ}$ to beam axis, the dose uniformity could be established to be 1.1% in $15{\times}15cm^2$ sized maximum field. For the beam contamination, it was determined by the ratio of the absorbed doses delivered by $C^{12}$ ion and other particles. The level of the beam contamination could be achieved to be less than 2.5% of total dose in the region from 5 cm to 17 cm water equivalent depth in the combined beam configuration. Based on the results, we could establish the optimized nozzle design satisfying the beam conditions which were required for biomedical researches.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.5 no.4
• /
• pp.83-93
• /
• 2001

A swirler with turbulence generator is designed and manufactured for generating many small-scale eddies in the combustor which contribute to enhancing mixing effect between fuel and air. The method results in not only the disadvantage of pressure loss but also the advantage of promoting combustion and reducing NOx. For the purpose of the study, four kinds of swirler with different turbulence generator area (0%, 3%, 7%, and 12% of reducing flow area) are designed to confirm the effect of mixing according the variation in the area of the turbulence generator. The mixing of combustor in the radial direction is significantly improved and the distributions of flames and temperature are well distributed throughout the cross section of a combustor as area of swirl generator is increased.