• 한국해안해양공학회지
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• 제4권1호
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• pp.45-58
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• 1992

황해 및 동중국해에서 기상학적으로 유발된 연여균 및 계절적 해류 순환을 산정하기 위해 3次元 수치모형이 이용되었는데 수치모형은 불규칙한 연안경계와 실제 수심을 반영할 수 있도록 구성되었다. 본 연구에서는 전회의 동중국해의 3차원 수치모형 (Choi, 1984)을 제붕역에서의 흐름을 좀더 자세히 재현할 수 있도록 세분화하였는데 모형에 사용된 유한격자체계의 해상도는 위도 4분과 경도 5분으로 구성되었으며 황해 및 동중국해상에서 유속의 3차원적 순환 형태가 산정되어 제시되었다. 수치모형에 의해 계산된 기상학적으로 유발된 恒流 유원은 이 해역의 여러 영역에서 수심(표면, 중간수심, 바닥)別 및 전체 水柱에 대해 해수 문체시간을 계산하는데 이용되었다.

• 대한기계학회논문집B
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• 제34권11호
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• pp.999-1004
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• 2010

디젤 엔진은 가솔린 엔진에 비해 열효율이 높고 이산화탄소 배출량이 적다. 그러나 입자상물질(PM)과 질소산화물(NOx)의 배출량이 가솔린 엔진보다 많은 단점을 가지고 있다. 디젤 엔진의 연소 배출물 중 질소 산화물을 저감시키기 위하여 LNT와 Urea-SCR과 같은 후처리 시스템이 최근 활발히 연구되고 있다. Urea-SCR은 Urea 수용액을 공급하기 위한 2차 분사 시스템이 필요하고, 분사된 Urea 수용액의 분무 거동 특성과 균일도에 따라서 촉매의 효율이 크게 달라진다. 본 연구에서는 배기관에 분사된 Urea 수용액의 분무균일도를 향상시키기 위하여 인젝터의 기초 분무 특성을 파악하였고, 모사배기관 시스템과 가시화 장비를 이용하여 배기관내에서의 분무 거동 특성을 파악하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제34권4호
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• pp.485-490
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• 2010

MILD(Moderate and Intense Low Oxygen Dilution)연소는 연소가스의 재순환을 이용하여 화염대의 고온 형성을 최대한 억제하여 질소산화물을 생성 과정에서 저감하는 동시에 연소로의 내부온도를 균일화하여 열 이용 효율을 향상시킬 수 있는 기술이다. 본 연구에서는 MILD 연소로에서 연료 및 공기 유량으로 당량비를 조절하고, 그 변화에 따른 연소로에서 발생되는 배기가스 및 연소로 내부의 온도 계측을 통하여 MILD 연소기의 특성과 MILD 연소 시 최적 조건을 도출하고자 하였다. 본 연구를 통하여 당량비가 0.71~0.73일 때 MILD 연소가 구현되었으며 MILD 연소 조건에서 온도 균일도와 NOx 및 CO 생성 특성을 평가하였다.

• 태양에너지
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• 제18권1호
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• pp.57-67
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• 1998

쾌적한 실내환경을 유지하고, 공기조화 설비에 있어서 냉방동안 에너지를 절약하기 위한 실내로 유입되는 냉기의 열유동 특성에 관한 연구이다. 실물 크기의 모형room에 대하여 실내로 유입하는 냉기의 유속(1, 2, 3m/s)과 실내온도와 유입냉기와의 기준온도차(10, 20, $30^{\circ}C$)를 변화시키고, 또한 유입구 형상을 아네모스형과 베인형으로 하면서 실내의 온도분포를 파악하여 열유동 특성 및 혼합특성에 대하여 고찰하였다. 연구 결과, 아네모스형이 베인형보다 혼합이 빨리 진행되었고 유입속도에 의한 영향이 기준 온도차에 의한 영향보다 지배적이었다.

• Selected Papers of The Society of Naval Architects of Korea
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• 제1권1호
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• pp.76-90
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• 1993

A new propeller series is developed using the newly developed blade section (KH 18 section) which has better cavitation characteristics and higher lift-drag ratio at wade angle-of-attack range than a conventional section. The radial patch distribution of the new series propellers is variable stance they were designed adaptively to a typical wake distribution. Basic geometric particulars of the series propellers. such as chord length, thickness, skew and rake distributions, are determined on the basis of recent full scale propeller geometric data. The series is developed for propellers having 4 blades, and blade area ratios of 0.3, 0.45, 0.6 and 0.75. Mean pitch ratios are varied as 0.5, 0.6, 0.7, 0.95 and 1.1 for each blade area ratio. The new propeller series consists of 20 propellers and is named as the KD(KRISO-DAEWOO)-propeller series. Propeller open-water tests are performed at the towing tank, and cavitation observation tests and fluctuating pressure tests are carried out at the cavitation tunnel of KRISO. $B_{p}-\delta$ curves, which can be used to select the optimum propeller diameter at the preliminary design stage, are derived from a regression analysis of the propeller open-water test results. The KD-cavitation chart is derived from the cavitation observation test results by choosing the local maximum lift coefficient and the local cavitation number as parameters. The cavity extent predicted by the KD-cavitation chart would be more accurate compared to that by an existing cavitation charts, such as the Burrll's cavitation chart, since the former is derived from the cavitation observation test results in a typical ship's wake, while the lather is derived from the test results in a uniform flow.

• 반도체디스플레이기술학회지
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• 제21권4호
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• pp.81-85
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• 2022

Mist-CVD is known to have advantages of low cost and high productivity method since the precursor solution is misting with an ultrasonic generator and reacted on the substrate under vacuum-free conditions of atmospheric pressure. However, since the deposition distribution is not uniform, various efforts have been made to derive optimal conditions by changing the angle of the substrate and the position of the outlet to improve the result of the preceding study. Therefore, in this study, a deposition distribution uniformity model was derived through the shape and position of the substrate support and the conditions of inlet flow rate using the particle tracking method of computational fluid dynamics (CFD). The results of analysis were compared with the previous studies through experiment. It was confirmed that the rate of deposition area was improved from 38.7% to 100%, and the rate of deposition uniformity was 79.07% which was higher than the predicted result of simulation. Particle tracking method can reduce trial and error in experiments and can be considered as a reliable prediction method.

• 전기화학회지
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• 제12권4호
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• pp.329-334
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• 2009

본 연구는 연료전지 운전시 전극 촉매 및 전해질막 내에서 발생하는 연료 및 산화제의 산화/환원 반응 메커니즘, 이동현상, 구성품 열화현상 등을 핵자기 공명 (NMR, Nuclear Magnetic Resonance)을 이용하여 연료전지의 분해나 시료 채취 없이 제자리 (in situ) 분석할 수 있는 진단장치용 연료전지 개발에 관한 것이다. NMR에 사용되는 연료전지는 특수하게 제작된 TCD (Toroid Cavity Detector) 탐침 내부에서 작동하여야 하며, TCD 탐침이 가지는 기하학적 제한 요소들로 인해 일반적인 평판형 연료전지와 달리 원통형으로 제작된다. 이로 인해 반응물의 공급이나 생성물의 제거가 어려우며 누수 현상 및 불균일한 압력 분배가 발생하여 성능이 낮다. 따라서, in situ NMR 분석용 연료전지가 가지는 구조상의 특징인 원통형에 적합한 유로를 설계하고 제작하여 물질 전달 특성을 개선해야 할 필요성이 있다. 본 연구에서는 NMR 장비 내의 자기장에 영향을 미치지 않는 비자성 물질을 이용해 원 통형 공기극 유로를 개발하여, 산소의 공급 및 반응물의 제거를 원활하게 하였다. 또한, 체결 압력을막-전극 접합체에 균일하게 분배하여 누수 및 누액을 차단하였다. 이를 통해, 상온에서 약 $36mW/cm^2$의 우수한 성능을 나타내는 in situ NMR 진단용 직접 메탄올연료전지 시스템을 개발하였다.

• 대한토목학회논문집
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• 제26권5B호
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• pp.447-457
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• 2006

본 연구에서는 2차원 수심 적분된 흐름을 모의하기 위한 수치모델을 개발하였다. 유한요소법의 일종인 Characteristic Dissipative Galerkin(CDG) 기법을 적용시켜 천수방정식의 수치해를 구한다. 모델 검증을 위해서 1차원 도수문제에 적용하였고, 계산결과와 해석해를 비교할 때 만족스러운 결과를 얻었다. 정상파를 보이는 단면축소 수로에서의 흐름을 모의한 결과, 실험결과와 유사한 수면분포를 얻었다. 이러한 검증 과정을 통해서 본 수치모델을 이용하여 흐름영역이 갑작스럽게 변화하는 경우에도 모의 가능함을 알았다. 또한 $180^{\circ}$ 만곡수로에 적용한 결과, 만곡부 내측의 유속이 외측에 비해서 크며, 만곡부 내측의 수심은 외측에 비해서 작은 만곡부 흐름특성을 잘 나타내고 있다. 그러나 만곡수로에서 이차류에 의한 운동량의 횡방향 이송을 고려하지 않는 지배방정식의 한계점으로 인해서, 만곡부 끝단을 제외한 만곡부 전체에 걸쳐서 단면상의 종방향 유속이 일정한 분포를 보이고 있다.

• IUGG한국위원회:학술대회논문집
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• IUGG한국위원회 2003년도 정기총회 및 학술발표회
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• pp.20-20
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• 2003

In the summers of 1997 and 1998 and in February of 2000 we made 570 measurements of the ambient geomagnetic field 120 cm above the pavement surface of State Route 130, south of Pahoa, the island of Hawaii using a three-component fluxgate magnetometer. We measured at every 15.2 m (50 feet) interval covering a distance of 6, 310 m (20, 704 ft) where both historic and pre-historic highly magnetic basalt flows underlie. We also collected 197 core samples from eight road cuts, 489 specimens of which were subject to AF demagnetizations at 5 - 10 mT level up to a maximum field of 60 mT. We observed significant inclination anomalies ranging from a minimum of $31^{\circ}$ to a maximum $40^{\circ}$ where a uniform inclination value of $36.7^{\circ}$ (International Geomagnetic Reference Field, IGRF) was expected. Since the mean of the observed inclinations is approximately $35^{\circ}$ we assume that the study area is slightly affected by the magnetic terrain effect to a systematically shallower inclinations for being located in the regionally sloping surface of the southern side of the island (Baag, et al., 1995). We observed inclination anomalies showing wider (spacial) wavelength (160 - 600 m) and higher amplitudes in the historic lava flows area than in the northern pre-historic flows. Our observations imply that preexisting inclination anomalies such as those that we observed would have been interpreted as paleosecular variation (PSV). These inclination anomalies can best be attributed to concealed underground highly magnetic dikes, channel type lava flows, on-and-off hydrothermal activities through fissure-like openings, etc. Both the within- and between-site dispersions of natural remanent magnetization (NRM) are largest (up to ${\pm}7^{\circ}$) above the flows of 1955, while the area of pre-historic flows in the northern part of the study area exhibit the smallest dispersion. Nevertheless, mean inclinations of each historic flow of 1955 and 1790 are almost identical to that of the corresponding present field, whereas mean of NRM (after AF demagnetization) inclinations for each of the four pre-historic lava flow units is twelve to thirteen degrees lower than the present field inclination. We observed three cases of very large inclination variations from within a single flow, the best fitting curves of which are linear, second and third order polynomials each from within a single flow, whereas no present field variations are observed. This phenomena can be attributed to the notion that local magnetic anomalies on the surface of an active volcano are not permanent, but are transient. Therefore we believe that local magnetic anomalies of an active volcano may be constantly modified due to on going subsurface injections and circulations of hot material and also due to wide spacial and temporal distribution of highly magnetic basaltic flows that will constantly modify the topography which will in turn modify the local ambient geomagnetic field (Baag, et al., 1995). Our observations bring into question the general reliability of PSV data inferred from volcanic rocks, because on-going various geologic and geophysical activities associated with active volcano would continuously deflect and modify the ambient geomagnetic field.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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• pp.1-2
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• 2011

Hybrid rockets have lately attracted attention as a strong candidate of small, low cost, safe and reliable launch vehicles. A significant topic is that the first commercially sponsored space ship, SpaceShipOne vehicle chose a hybrid rocket. The main factors for the choice were safety of operation, system cost, quick turnaround, and thrust termination. In Japan, five universities including Hokkaido University and three private companies organized "Hybrid Rocket Research Group" from 1998 to 2002. Their main purpose was to downsize the cost and scale of rocket experiments. In 2002, UNISEC (University Space Engineering Consortium) and HASTIC (Hokkaido Aerospace Science and Technology Incubation Center) took over the educational and R&D rocket activities respectively and the research group dissolved. In 2008, JAXA/ISAS and eleven universities formed "Hybrid Rocket Research Working Group" as a subcommittee of the Steering Committee for Space Engineering in ISAS. Their goal is to demonstrate technical feasibility of lowcost and high frequency launches of nano/micro satellites into sun-synchronous orbits. Hybrid rockets use a combination of solid and liquid propellants. Usually the fuel is in a solid phase. A serious problem of hybrid rockets is the low regression rate of the solid fuel. In single port hybrids the low regression rate below 1 mm/s causes large L/D exceeding a hundred and small fuel loading ratio falling below 0.3. Multi-port hybrids are a typical solution to solve this problem. However, this solution is not the mainstream in Japan. Another approach is to use high regression rate fuels. For example, a fuel regression rate of 4 mm/s decreases L/D to around 10 and increases the loading ratio to around 0.75. Liquefying fuels such as paraffins are strong candidates for high regression fuels and subject of active research in Japan too. Nakagawa et al. in Tokai University employed EVA (Ethylene Vinyl Acetate) to modify viscosity of paraffin based fuels and investigated the effect of viscosity on regression rates. Wada et al. in Akita University employed LTP (Low melting ThermoPlastic) as another candidate of liquefying fuels and demonstrated high regression rates comparable to paraffin fuels. Hori et al. in JAXA/ISAS employed glycidylazide-poly(ethylene glycol) (GAP-PEG) copolymers as high regression rate fuels and modified the combustion characteristics by changing the PEG mixing ratio. Regression rate improvement by changing internal ballistics is another stream of research. The author proposed a new fuel configuration named "CAMUI" in 1998. CAMUI comes from an abbreviation of "cascaded multistage impinging-jet" meaning the distinctive flow field. A CAMUI type fuel grain consists of several cylindrical fuel blocks with two ports in axial direction. The port alignment shifts 90 degrees with each other to make jets out of ports impinge on the upstream end face of the downstream fuel block, resulting in intense heat transfer to the fuel. Yuasa et al. in Tokyo Metropolitan University employed swirling injection method and improved regression rates more than three times higher. However, regression rate distribution along the axis is not uniform due to the decay of the swirl strength. Aso et al. in Kyushu University employed multi-swirl injection to solve this problem. Combinations of swirling injection and paraffin based fuel have been tried and some results show very high regression rates exceeding ten times of conventional one. High fuel regression rates by new fuel, new internal ballistics, or combination of them require faster fuel-oxidizer mixing to maintain combustion efficiency. Nakagawa et al. succeeded to improve combustion efficiency of a paraffin-based fuel from 77% to 96% by a baffle plate. Another effective approach some researchers are trying is to use an aft-chamber to increase residence time. Better understanding of the new flow fields is necessary to reveal basic mechanisms of regression enhancement. Yuasa et al. visualized the combustion field in a swirling injection type motor. Nakagawa et al. observed boundary layer combustion of wax-based fuels. To understand detailed flow structures in swirling flow type hybrids, Sawada et al. (Tohoku Univ.), Teramoto et al. (Univ. of Tokyo), Shimada et al. (ISAS), and Tsuboi et al. (Kyushu Inst. Tech.) are trying to simulate the flow field numerically. Main challenges are turbulent reaction, stiffness due to low Mach number flow, fuel regression model, and other non-steady phenomena. Oshima et al. in Hokkaido University simulated CAMUI type flow fields and discussed correspondence relation between regression distribution of a burning surface and the vortex structure over the surface.