• Industrial Engineering and Management Systems
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• 제9권4호
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• pp.294-302
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• 2010

There is a trend toward the world's manufacturing sites moving to East Asia. After manufacture, these products are transported to the advanced nations for their consumption demands. Among such advanced nations, the U.S.A. has the largest demand, and then Japan and European countries follow. It should be noted that the infrastructures of the Asian districts used for the production sites are rather limited, and the volume of products transported from these districts of Asia to the U.S.A is becoming tremendously large. This situation is causing very serious traffic problems. New products are required to be transported swiftly by air. Once the consumption and market demands are stable however, the products should be sent rather slowly, but in larger amounts. However, the airports of China are quite restricted in capacity, while the transportation volume is becoming large. As a result, transportation cost and the time required for transportation are increasing. Now, a third method is appearing. This is the so-called Sea and Air transportation. The cost and time in transit of this mode take mean positions between Air and Ocean services. At present there exists no well-thought-out strategy for how to allocate these three methods of transportation. This paper is an attempt to theoretically describe this mechanism and to discover the optimal way to allocate the three modes. For this purpose, several mathematical properties of value and cost of the products are defined, and on this basis a simulation of the transportation is established.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2003년도 춘계학술대회 논문집 센서 박막재료 반도체 세라믹
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• pp.120-123
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• 2003

To investigate the characteristics of the single dendrimer molecule, we attempt to measure morphology and electrical properties of the self-assembled dendrimer on Au (111)substrate with SPM(scanning probe microscopy). The same self-assembly procedure was used for two different concentrations, $10{\mu}mol/ml$ and $100{\mu}mol/ml$. The case of lower concentration, we can measure the diameter and the height of the single molecule with the tapping mode AFM image. The imaged single molecules were dome shaped and the average diameter and height were 15.6 nm, 1.2 nm respectively. From these sizes, we can calculate the volume of the single molecule. The volume of the single molecule was estimated about $116nm^3$. However, that of higher concentration, it is difficult to obtain obvious image of the single molecule. To add to, I-V characteristics were investigated using STM, on which the phenomenon of negative differential resistance (NDR)was observed between 0.14 V and 0.24 V reproductively.

• 분석과학
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• 제33권6호
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• pp.274-284
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• 2020

액체시료 중 89Sr와 90Sr을 자동핵종분리장치를 이용하여 Sr-resin으로 분리-정제하고, 액체섬광계수기(LSC)로 동시 분석하는 방법을 연구하였다. 액체시료 0.5 kg 중 방사성스트론튬을 탄산염 형태로 농축하고, Sr-resin 2 mL (Bed volume)으로 분리하였다. 유량이 최대 1 mL min-1까지 가능한 중력법과, 유량 2 mL min-1, 4 mL min-1 조건에서, Sr과 방해이온들의 거동을 평가하였다. LSC를 이용해 섬광용액을 혼합하지 않은 Cerenkov mode와, 섬광용액을 혼합한 Scintillation mode에서 측정한 결과를 이용해 정제된 89Sr와 90Sr의 방사능을 동시에 분석하였다. 표준선원을 이용해 90Sr/89Sr의 방사능 비가 1:1, 1:2, 1:5 되도록 탈염수를 이용해 모의시료를 준비하였고, 89Sr 방사능은 0.5~10 Bq kg-1, 90Sr 방사능은 0.5~50 Bq kg-1의 범위이다. Sr의 회수율은 68~94 %이고, 89Sr의 상대편의는 -5~20 %, 90Sr 방사능의 상대편의는 -10~10 %로 나타났다.

• 대한환경공학회지
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• 제27권10호
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• pp.1114-1122
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• 2005

이 연구는 초음파에 의한 1,4-dioxane(1,4-D)의 제거효율과 반응속도의 증가를 위해 초음파의 조사방식, 반응온도와 부피의 효과를 조사하였다. 초음파가 펄스방식으로 주사된 경우가 연속적으로 주사된 경우보다 약 10%의 1,4-D의 감소 효율의 증가를 보였다. 두 경우 모두 1000 mL와 반응온도가 고정되지 않은 조건에서 실시된 것으로 반응곡선은 도입단계, 가속단계, 그리고 안정화단계 등 3단계로 구분될 수 있었다. 실제로 1,4-D의 제거를 보이는 부분은 도입단계와 가속단계로 이들의 속도론적 특징은 도입단계와 가속 단계 각각 0차 반응과 유사일차반응과 부합하였다. 반면에 300 mL의 반응부피에서 온도를 고정한 경우에서는 3단계의 제거 유형을 보이지 않았다. $5^{\circ}C$로 고정한 경우만이 유사일차 반응과 부합하였고 그 이상의 온도에서는 0차 반응과 부합하였다. $20^{\circ}C$로 온도가 고정된 조건에서 반응부피 300 mL의 경우가 1000 mL 반응에서 보다 높은 분해 효율을 보였을 뿐만 아니라 단일한 제거 특성을 보였다. 이러한 반응 온도와 부피의 영향은 초음파 주사에 의해 생성되는 bubble의 강도에 영향을 주며 bubble의 강도가 높을수록 OH 라디칼의 생성이 증가되었다.

• 한국의학물리학회지:의학물리
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• 제24권4호
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• pp.220-229
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• 2013

Respiratory-induced dynamic tumors render free-breathing cone-beam computed tomography (FBCBCT) images with motion artifacts complicating the task of quantifying the internal target volume (ITV). The purpose of this paper is to study the visibility of the revealed ITV when the imaging dose parameters, such as the kVp and mAs, are varied. The $Trilogy^{TM}$ linear accelerator with an On-Board Imaging ($OBI^{TM}$) system was used to acquire low-imaging-dose-mode (LIDM: 110 kVp, 20 mA, 20 ms/frame) and high-imaging-dose-mode (HIDM: 125 kVp, 80 mA, 25 ms/frame) FBCBCT images of a 3-cm diameter sphere (density=0.855 $g/cm^3$) moving in accordance to various sinusoidal breathing patterns, each with an unique inhalation-to-exhalation (I/E) ratio, amplitude, and period. In terms of image ITV contrast, there was a small overall average change of the ITV contrast when going from HIDM to LIDM of $6.5{\pm}5.1%$ for all breathing patterns. As for the ITV visible volume measurements, there was an insignificant difference between the ITV of both the LIDM- and HIDM-FBCBCT images with an average difference of $0.5{\pm}0.5%$, for all cases, despite the large difference in the imaging dose (approximately five-fold difference of ~0.8 and 4 cGy/scan). That indicates that the ITV visibility is not very sensitive to changes in imaging dose. However, both of the FBCBCT consistently underestimated the true ITV dimensions by up to 34.8% irrespective of the imaging dose mode due to significant motion artifacts, and thus, this imaging technique is not adequate to accurately visualize the ITV for image guidance. Due to the insignificant impact of imaging dose on ITV visibility, a plausible, alternative strategy would be to acquire more X-ray projections at the LIDM setting to allow 4DCBCT imaging to better define the ITV, and at the same time, maintain a reasonable imaging dose, i.e., comparable to a single HIDM-FBCBCT scan.

• Journal of Welding and Joining
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• 제16권6호
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• pp.59-68
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• 1998

In this study, effects of solidification modes (primary $\delta$-ferrite, primary ${\gamma}$-austenite) on the pit initiation and propagation in the 304L and 316L austenitic stainless steel weld metals were investigated. The solidification mode of weld metal was controlled by the addition of nitrogen to Ar shielding gas. Through the electrochemical experiments (potentiodynamic anodic polarization and potentiostatic time-current transient test) and metallographic examination (microstructure and elemental distribution), the following results were obtained. The more the volume content of nitrogen in the shielding gas were, the lower critical current density for passivity was observed. In comparison with weldments solidified through the primary $\delta$-ferrite solidification mode and the primary ${\gamma}$-solidification mode, the former showed higher critical pitting potential and a longer incubation time for stable pit initiation than the latter. However, in the pit propagation stage the former exhibited a faster dissolution rate than the latter. These results were believed to ee related to the distribution of alloying elements such as Cr, Mo, Ni and S.

• 한국산업안전학회:학술대회논문집
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• 한국안전학회 1997년도 추계 학술논문발표회 논문집
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• pp.43-48
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• 1997

아트리움 공간에서 화재 발생시 연기 유동에 대하여 두 가지 형태의 화재 모델인 zone 모델과 field 모델을 이용하여 시뮬레이션 했다. 사용된 zone model은 NIST에서 개발된 CFAST(version 1.6) 모델이며 field 모델은 전산유체역학 이론을 바탕으로 자체 개발된 화재 모델이다. 본 연구는 정육면체 모양의 아트리움 공간에서 연기 유동과 온도 분포에 대하여 해석하고자 한다. 화재로 인해 야기된 유동에 대하여 속도장과 은도장을 예측하기 위한 계산 과정은 유한체적법 및 비엇갈림격자계를 이용하여 질량, 운동량, 에너지 및 성분 보존 방정식등에 대한 3차원 비정상상태 지배방정식을 사용했다. 수치해석 결과 zone 모델과 field 모델의 화재 모델에 의해 예측된 연기 층 평균 경계놀이와 상부 더운 연기 층의 평균 온도에 대하여 거의 유사한 결과를 얻었다.

• 한국수소및신에너지학회논문집
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• 제23권2호
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• pp.162-172
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• 2012

This paper presents a research about free piston linear engine (FPLE) fueled with hydrogen, in which, the numerical models are built to simulate the operation during the full stroke of the engine. Dynamic model, linear alternator model and thermodynamic model are used as the numerical models to predict piston velocity, in-cylinder pressure and electric power of FPLE. The spark timing and air gap length are changed to provide information for the prediction. Beside, the heat transfer problem is also investigated in the paper. The results of research are divided by two parts, including motoring mode and firing mode. The result of motoring mode showed that there is validation between simulation and experiment for volume and pressure in cylinder. For firing mode, by increasing spark timing, the velocity of piston, peak pressure and electric power also increase respectively. Beside, when increasing air gap length, the electric power increases accordingly while the motion of piston is not symmetric. The effect of heat transfer also observed clearly by reducing of the peak pressure, velocity of piston and electric power.

• 한국공간구조학회논문집
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• 제15권2호
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• pp.69-77
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• 2015

Ultra High Performance Fiber Reinforced Concrete (UHPFRC) has a outstanding tensile hardening behaviour after a crack develops, which gives ductility to structures. Existing shear strength model for fiber reinforced concrete is entirely based on crack opening behavior(mode I) which comes from flexural-shear failure, not considering shear-slip behavior(mode II). To find out the mode I and mode II behavior on a crack in UHPFRC simultaneously, maximum shear strength of cracked UHPFRC is investigated from twenty-four push-off test results. The shear stress on a crack is derived as variable of initial crack width and fiber volume ratio. Test results show that shear slippage is proportional to crack opening, which leads to relationship between shear transfer strength and crack width. Based on the test results a hypothesis is proposed for the physical mechanics of shear transfer in UHPFRC by tensile hardening behavior in stead of aggregate interlocking in reinforced concrete. Shear transfer strength based on tensile hardening behavior in UHPFRC is suggested and this suggestion was verified by comparing direct tensile test results and push-off test results.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.499-505
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• 2004

A Propulsion System of the CRW(Canard Rotor Wing) type UAV(Unmanned Aerial Vehicle) was composed of the turbojet engine to generate the propulsive exhaust gas, and the duct system including straight bent ducts, tip-jet nozzles, a master valve and a variable main nozzle for three flight modes such as lift/landing mode, low speed transition flight mode and high speed forward flight mode. In this study, in order to operate safely the propulsion system, the dynamic Performance behavior of the system was modeled and simulated using the SIMULIN $K^{ }$, which is the user-friendly GUI type dynamic analysis tool provided by MATLA $B^{ }$. In the transient performance model, the inter-component volume model was used. The performance analysis using the developed models was performed at various flight condition, valve angle positions and fuel flow schedules, and these results could set the safe flight mode transition region to satisfy the inlet temperature overshoot limitation as well as the compressor surge margin. Performance analysis results using the SIMULIN $K^{ }$ performance program were compared with them using the commercial program GSP.m GSP.