• 한국해안해양공학회지
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• 제7권3호
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• pp.248-256
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• 1995

표층밀도분류에 대한 수치계산에서 문제로 되는 것은 자유수면의 처리, 레이놀즈응력/플럭스항, 특히 난류변동성분에 미치는 부력효과 등에 관련된 것이며, 이것에 대한 보다 집중적인 연구가 필요하다. 또한, 농도장이나 온도장에서의 난류변동성분을 측정하는 데 있어서의 어려움으로 인한 실험자료의 부족으로 수치 계산으로부터 얻어진 예측결과의 충분한 검증은 이루어지지 않고 있다. 본 연구에서는 2차원 표층밀도분류에 대한 유동특성을 조사하기 위하여 난류의 비등방성을 고려하여 난류응력을 직접 계산하는 대수응력모델을 적용하여 수치계산을 행하고, 그 결과를 실험결과와 비교ㆍ검토하였다. 검토한 결과 대수응력모델은 전 영역모델은 전 영역에서 2차원 표층밀도분류의 유동특성을 양호하게 재현하였으며, 특히 부력효과로 인한 성층화가 발생하는 부력 탁월영역에서 난류유동장의 흐름특성을 합리적으로 예측함을 입증하였다.

• 한국분말재료학회지
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• 제19권4호
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• pp.247-252
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• 2012

Effect of Cu and $DyF_3$ powder mixing with Cu-free (Nd, Dy)-Fe-B jet-milled powder on the magnetic properties of sintered magnets was investigated. The coercivity of a magnet prepared from the Cu-free (Nd, Dy)-Fe-B powder was about 10 kOe even though the alloy powder already contained some Dy (3.5 wt%). When small copper powder was blended, however, the coercivity of the magnet increased almost 100%, exhibiting about 20 kOe. On the contrary, the coercivity enhancement was moderate, about 4 kOe, when dysprosium content in the sintered magnet was simply increased to 4.9 wt% by the addition of small $DyF_3$3 powder.

• 콘크리트학회논문집
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• 제17권1호
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• pp.77-84
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• 2005

제강 슬래그는 제강 공정에서 발생되는 부산물로서 주로 에이징 한 후 도로용 노반재로 사용된다. 제강 슬래그내에 포함된 free-CaO와 물과의 반응하여 체적팽창을 일으키기 때문에 공기중에 장시간 에이징 하는 것이 필요하다. 이러한 문제 때문에 제강 슬래그를 콘크리트용 골재로 사용하는데 어려움이 있다. 그러나, 본 연구에서는 고온의 용융상태에서 고속공기로 뿜어 급냉시킨 제강 슬래그를 사용하였다. 이와 같이 급냉시키는 방법은 제강 슬래그내의 free-CaO의 생성량을 저감시킨다. 본 연구에서는 통계적 실험계획법 중 일원배치법을 이용하여 급냉 제강 슬래그 대체율이 플로우, 고성능감수제의 첨가율, 물-시멘트비 및 압축강도 등 모르타르의 특성에 미치는 영향을 검토하였다. 또한, 이들 데이터를 분산분석 후 F-검정을 실시하여 급냉 제강 슬래그가 모르타르의 특성에 유의한 영향을 주고 있는 지를 검정하였다. F-검정결과 유의수준 $1\%$내에서 급냉 제강 슬래그 대체율이 증가할수록 모르타르의 플로우 증가, 고성능감수제 첨가율 및 물-시멘트비의 감소, 압축강도의 증진에 크게 영향을 미치는 것을 검정하였다. 또한, 유동성 및 압축강도를 고려할 때 강모래에 대하여 급냉 제강 슬래그 대체율 $75\%$를 사용하는 것이 가장 우수한 유동성과 압축강도 발현하는 것으로 나타났다.

• 한국환경과학회지
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• 제11권5호
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• pp.419-436
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• 2002

The current paper reports on the enhancement of O$_3$, CO, NO$_2$, and aerosols during the Asian dust event that occurred over Korea on 1 May 1999. To confirm the origin and net flux of the O$_3$, CO, NO$_2$, and aerosols, the meteorological parameters of the weather conditions were investigated using Mesoscale Meteorological Model 5(MM5) and the TOMS total ozone and aerosol index, the back trajectory was identified using the Hybrid Single-Particle Lagrangian Integrated Trajectory Model(HYSPLIT), and the ozone and ozone precursor concentrations were determined using the Urban Ashed Model(UAM). In the presence of sufficiently large concentrations of NO$\sub$x/, the oxidation of CO led to O$_3$ formation with OH, HO$_2$, NO, and NO$_2$ acting as catalysts. The sudden enhancement of O$_3$, CO, NO$_2$ and aerosols was also found to be associated with a deepening cut-off low connected with a surface cyclone and surface anticyclone located to the south of Korea during the Asian dust event. The wave pattern of the upper trough/cut-off low and total ozone level remained stationary when they came into contact with a surface cyclone during the Asian dust event. A typical example of a stratosphere-troposphere exchange(STE) of ozone was demonstrated by tropopause folding due to the jet stream. As such, the secondary maxima of ozone above 80 ppbv that occurred at night in Busan, Korea on 1 May 2001 were considered to result from vertical mixing and advection from a free troposphere-boundary layer exchange in connection with an STE in the upper troposphere. Whereas the sudden enhancement of ozone above 100 ppbv during the day was explained by the catalytic reaction of ozone precursors and transport of ozone from a slow-moving anticyclone area that included a high level of ozone and its precursors coming from China to the south of Korea. The aerosols identified in the free troposphere over Busan, Korea on 1 May 1999 originated from the Taklamakan and Gobi deserts across the Yellow River. In particular, the 1000m profile indicated that the source of the air parcels was from an anticyclone located to the south of Korea. The net flux due to the first invasion of ozone between 0000 LST and 0600 LST on 1 May 1999 agreed with the observed ground-based background concentration of ozone. From 0600 LST to 1200 LST, the net flux of the second invasion of ozone was twice as much as the day before. In this case, a change in the horizontal wind direction may have been responsible for the ozone increase.

• Journal of Mechanical Science and Technology
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• 제16권8호
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• pp.1135-1143
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• 2002

The intermittent spray characteristics of the single-hole diesel nozzle (d$\sub$n/=0.32 mm) used in the fuel injection system of heavy-duty diesel engines were experimentally investigated. The mean velocity and turbulent characteristics of the diesel spray injected intermittently into the still ambient were measured by using a 2-D PDPA (phase Doppler particle analyzer) . The gradient of spray half-width linearly increased with time from the start of injection, and it approximated to 0.04 at the end of the injection. The axial mean velocity of the fuel spray measured along the radial direction was similar to that of the free air jet within R/b= 1.0-1.5 regardless of elapsing time, and its non-dimensional distribution corresponds to the theoretical velocity distributions suggested by Hinze in the downstream of the spray flow fields. The turbulent intensity of the axial velocity components measured along the radial direction represented the 20-30% of the U$\sub$cι/ and tended to decrease in the outer region. The turbulent intensity in the trailing edge was higher than that in the leading edge.

• 한국추진공학회지
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• 제8권1호
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• pp.61-69
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• 2004

본 연구는 극초음속 모델 스크램제트 엔진 연소기의 화염지지와 연료-공기 혼합과정의 특성을 살펴보기 위하여 수치해석을 이용하여 수행되었다. 연료분사 방법으로 수소연료가 초음속 유동장에 수직분사되는 경우와 공동내부에 분사되는 두 가지 경우를 채택하였으며 각각 UQ(University of Queensland, Australia)와 ANU(Australian National University, Australia)의 충격파 풍동을 이용하여 실험이 수행되었다. 수치해석을 통하여 수직분사 상류의 박리영역과 공동주변에서 연소현상이 관찰되었다. 수직분사의 박리영역과 공동내부분사의 공동은 재순환 영역을 발생시키며, 이 재순환 영역은 연료-공기의 혼합을 촉진시킨다. 또한 자발점화가 박리영역-자유류, 공동-자유류 경계면에서 발생함을 알 수 있었다.

• International Journal of Automotive Technology
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• 제6권6호
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• pp.579-584
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• 2005

Unsteady state free natural gas jets injected from several types of injectors were numerically simulated. Simulations showed good agreements with the schlieren experimental results. Moreover, injections of natural gas in intake manifolds of a single-valve engine and a double-valve engine were predicted as well. Predictions revealed that large volumetric injections of natural gas in intake manifolds led to strong impingement of natural gas with the intake valves, which as a result, gave rise to pronounced backward reflection of natural gas towards the inlets of intake manifolds, together with significant increase in pressure in intake manifold. Based on our simulations, we speculated that for engines with short intake manifolds, reflections of the mixture of natural gas and air were likely to approach the inlets of intake manifolds and subsequently be inbreathed into other cylinders, resulting in non-uniform mixture distributions between the cylinders. For engines with long intake manifolds, inasmuch as the degrees of intake interferences between the cylinders were not identical in light of the ignition sequences, non-uniform intake charge distributions between the cylinders would occur.

• 한국지하수토양환경학회지:지하수토양환경
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• 제19권5호
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• pp.18-25
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• 2014

Traditional investigation procedures of soil and groundwater contamination are followed by soil gas sampling, soil sampling, groundwater sampling, establishment of monitoring wells, and groundwater monitoring. It often takes several weeks to obtain the analysis reports, and sometimes, it needs supplemental sampling and analysis to delineate the polluted area. Laser induced fluorescence (LIF) system is designed for the detection of free-phase petroleum pollutants, and it is suitable for on-site real-time site investigation when coupling with a direct push testing tool. Petroleum products always contain polycyclic aromatic hydrocarbon (PAH) compounds possessing fluorescence characteristics that make them detectable through LIF detection. In this study, LIF spectroscopy of 5 major fuel products was conducted to establish the databank of LIF fluorescence characteristic spectra, including gasoline, diesel, jet fuel, marine fuel and low-sulfur fuel. Multivariate statistical tools were also applied to distinguish LIF fluorescence characteristic spectra among the mixtures of selected fuel products. This study successfully demonstrated the feasibility of identifying fuel species based on LIF characteristic fluorescence spectra, also LIF seemed to be uncovered its powerful ability of tracing underground petroleum leakages.

• 대한기계학회논문집
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• 제18권11호
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• pp.2954-2966
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• 1994

The characteristics and good corrosion resistance at room and elevated temperatures led to increasing application of Ti-alloys such as aircraft, jet engine, turbine wheels. In forging of Ti-alloy at high temperature, die chilling and die speed should be carefully controlled because the flow stress of Ti-alloy is sensitive to temperature, strain and strain-rate. In this study, the forging of turbine disk was numerically simulated by the finite element method for hot-die forging process and isothermal forging process, respectively. The effects of the temperature changes, the die speed and the friction factor were examined. Also, local variation of process parameters, such as temperature, strain and strain-rate were traced during the simulation. It was shown that the isothermal forging with low friction condition produced defect-free disk under low forging load. Consequently, the simulational information will help industrial workers develope the forging of Ti-alloys including 'preform design' and 'processing condition design'. It is also expected that the simulation method can be used in CAE of near net-shape forging.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2001년도 유체기계 연구개발 발표회 논문집
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• pp.361-366
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• 2001

A mim turbo-shaft engine of 50HP for UAV, which can be easily modified to turbo-prop and turbo-jet engine by sharing the core engine and has many applications to civilian demands and munitions, will be developed This kind of micro gas turbine engine has been developed mostly by the corporations which have special technology but are small in its scale. Especially, the gas turbine engine can be easily applied to other fields and developed by domestic technology, so that the sharing of technology is planed to realize through the cooperations with academies and research institutes. In this paper, the gas turbine engine, which has the compressor ratio of 3.8, the turbine inlet temperature of l180K and the engine speed higher than 100,000 rpm, is composed of centrifugal compressor, combustor, gas generator turbine, free power turbine and gear box. The competitiveness of the gas turbine engine can be obtained from minimizing its cost by the utilization of domestic infrastructure for the performance test and the decisive outsourcing.