• 한국정보통신학회:학술대회논문집
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• 한국해양정보통신학회 2006년도 춘계종합학술대회
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• pp.542-545
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• 2006

RFID는 각종 서비스 산업은 물론 물류, 산업 현장, 제조 공장과 물품의 흐름이 있는 곳이면 어디에서나 적용이 가능하여 사회 여러 분야로부터 큰 관심을 받고 있다. 하지만 현재 900MHz 대역의 RFID에서 사용하는 ISO18000-6의 프로토콜에서는 에러검출을 위한 CRC16만을 사용하고 있으며, 에러정정능력을 갖추지 못해 그 신뢰성이 매우 떨어진다. 본 연구에서는 이러한 RFID 시스템의 신뢰성 향상을 위하여 Reader에서 Tag로의 데이터 전송 시에 대역확산방식과 컨볼루션 부호를 적용하여 시스템의 신뢰성 향상을 목적으로 하고 있으며, 또한, 이러한 방식을 적용했을 때와 적용하지 않았을 때의 에러율을 측정 비교하였다.

• 한국정보통신학회논문지
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• 제17권12호
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• pp.2937-2943
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• 2013

본 논문은 방사기저함수(Radial Basis Function)를 이용한 실시간 군집 시뮬레이션 프레임웍을 제안한다. 제안된 프레임웍에서는 군집이 존재하는 환경을 격자 구조로 모델링 한 후, 격자 구조 각 셀에 하나의 방향 벡터를 할당한 벡터필드를 선형 방사기저함수를 이용하여 실시간으로 합성한다. 방사기저함수를 통한 벡터필드 생성 시, 마우스를 통한 제어라인(Control line)을 이용하며, 이 벡터필드 위에서 군집들은 벡터 필드 흐름에 따라, 자신의 움직임을 결정한다. 방해물과의 충돌회피는 반발벡터필드로 모델링하여, 기존의 벡터필드에 오버레이 하여 이용하고, 다른 캐릭터와의 충돌회피는 lattice-bin 알고리즘에 빠른 충돌회피를 수행한다.

• 대한조선학회논문집
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• 제58권2호
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• pp.90-96
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• 2021

In this study, the method of determining the state of grid points in the adaptable surface particle method based on grid system developed as a free-surface tracing method was improved. The adaptable surface particle method is a method of determining the state of the grid point according to the shape of the free-surface and obtaining the intersection of the given free-surface and grid line where the state of the grid point changes. It is difficult to determine the state of grid points in the event of rapid flow, such as collision or separation of free-surfaces, and this study suggests a method for determining the state of current grid points using the state of surrounding grid points where the state of grid point are known. A grid layer value was assigned sequentially to a grid away from the free-surface, centering on the boundary cell where the free-surface exists, to identify the connection information that the grid was separated from the free-surface, and to determine the state of the grid point sequentially from a grid away from the free-surface to a grid close to the free-surface. To verify the improved method, a numerical analysis was made on the problem of dam break in which a sudden collision of free-surface occurred and the results were compared, and the results were relatively reasonable.

• Journal of Mechanical Science and Technology
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• 제18권8호
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• pp.1435-1450
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• 2004

Experimental data are presented which describe the effects of a combustor-level high free-stream turbulence on the near-wall flow structure and heat/mass transfer on the endwall of a linear high-turning turbine rotor cascade. The end wall flow structure is visualized by employing the partial- and total-coverage oil-film technique, and heat/mass transfer rate is measured by the naphthalene sublimation method. A turbulence generator is designed to provide a highly-turbulent flow which has free-stream turbulence intensity and integral length scale of 14.7% and 80mm, respectively, at the cascade entrance. The surface flow visualizations show that the high free-stream turbulence has little effect on the attachment line, but alters the separation line noticeably. Under high free-stream turbulence, the incoming near-wall flow upstream of the adjacent separation lines collides more obliquely with the suction surface. A weaker lift-up force arising from this more oblique collision results in the narrower suction-side corner vortex area in the high turbulence case. The high free-stream turbulence enhances the heat/mass transfer in the central area of the turbine passage, but only a slight augmentation is found in the end wall regions adjacent to the leading and trailing edges. Therefore, the high free-stream turbulence makes the end wall heat load more uniform. It is also observed that the heat/mass transfers along the locus of the pressure-side leg of the leading-edge horseshoe vortex and along the suction-side corner are influenced most strongly by the high free-stream turbulence. In this study, the end wall surface is classified into seven different regions based on the local heat/mass transfer distribution, and the effects of the high free-stream turbulence on the local heat/mass transfer in each region are discussed in detail.

• 한국항공우주학회지
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• 제32권8호
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• pp.12-19
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• 2004

미소평판 주위의 저속 기체유동장이 기체분자운동론에 근거한 방법으로 조사되었다. 모델충돌적분항으로 단순화된 볼츠만방정식을 Discrete Ordinate 방법과 결합된 유한차분법으로 수치해석 하여 길이가 $20{\mu}m$인 5% 평판 주위의 유동장을 계산하였다. 계산결과가 Information Preservation 방법 및 미끄럼 경계조건을 이용한 연속체 방법에 의한 결과와 비교되었다. 세 가지 서로 다른 방법에 의한 계산결과가 기본적으로 유사한 유동형태를 예측하였으나, 세부적인 변에서는 본 방법의 결과가 다른 두 방법의 결과보다 더 정확함을 보였다.

• 한국대기환경학회지
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• 제18권3호
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• pp.223-230
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• 2002

Titania photocatalytic oxidation reactors were studied to investigate degradation efficiencies of hydrocarbons. In general, it is well known phenomena that thin layered titania oxidizes most of hydrocarbons to carbon dioxide and water under UV light. In this study, degradation efficiencies were measured due to changes in reactor structures, UV sources, the number of titania coatings, and various hydrocarbon chemicals. It was proven that gas degradation efficiencies are related to such factors as UV transmittance of coating substance, collision area of surface, and gas flow rate. For packing type annular reactor, about 98% degradation efficiency was achieved for achieved for propylene of 500 ppm level at a flow rate of 100 ml/min. Several gases were also tested for double-coated titania thin film under the condition of continuous flow of 100 ml/min and 365 nm UV source. It was shown that degradation efficiencies were decreasing in the order: $C_3$ $H_{6}$, n-C$_4$ $H_{10}$, $C_2$ $H_4$, $C_2$ $H_2$, $C_{6}$ $H_{6}$ and $C_2$ $H_{6}$./. 6/./.

• 국제초고층학회논문집
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• 제1권2호
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• pp.87-97
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• 2012

The indoor environments in high-rise buildings are generally well enclosed by defined boundary conditions. Here, a numerical simulation method based on the Lattice Boltzmann method (LBM), which aims to model and simulate the turbulent flow accurately in an enclosed environment, and its comparison with traditional computational fluid dynamics (CFD) results, are presented in this paper. CFD has become a powerful tool for predicting and evaluating enclosed airflows with the rapid advance in computer capacity and speed, and various types of CFD turbulence modeling and its application and validation have been reported. The LBM is a relatively new method; it involves solving of the discrete Boltzmann equation to simulate the fluid flow with a collision model instead of solving Navier-Stokes equations. In this study, the LBM-based scheme of flow pattern and particle dispersion analyses are validated using the benchmark test case of two- and three-dimensional and isothermal conditions (IEA/Annex 20 case); the prediction accuracy and advantages are also discussed by comparison with the results of CFD.

• 설비공학논문집
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• 제22권8호
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• pp.509-514
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• 2010

A numerical simulation of passenger evacuation in a subway station was performed by coupling the passenger flow analysis and the fire simulation. The algorithm of the passenger flow analysis was based on a DEM (Discrete Element Method) using the potential map of the direction vector for each passenger. This algorithm was improved in the present study as to use finer grid smaller than a passenger in order to resolve detailed geometry of the station and to resolve the behavior of passengers in the bottleneck at the ticket gate considering the collision of passengers to a wall or with other passengers. In the fire simulation, the CO distribution predicted by using CFD was used to take into account the effect of toxic gases on the passengers' mobility. The methodology proposed in the present study could be used in designing safer subway station in case of fire occurrence.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 춘계 학술대회논문집
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• pp.83-86
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• 2007

Turbulent flow analysis is conducted around the multi-stage launch vehicle including base region and detachment motion of strap-on boosters due to resultant aerodynamic forces and gravity is simulated. Aerodynamic solution procedure is coupled with rigid body dynamics for the prediction of separation behavior. An overset mesh technique is adopted to achieve maximum efficiency in simulating relative motion of bodies and various turbulence models are implemented on the flow solver to predict the aerodynamic forces accurately. At first, some preliminary studies are conducted to show the importance of base flow for the exact prediction of detachment motion and to find the most suitable turbulence model for the simulation of launch vehicle configurations. And then, developed solver is applied to the simulation of KSR-III, a three-stage sounding rocket researched in Korea. From the analyses, after-body flow field strongly affects the separation motions of strap-on boosters. Negative pitching moment at initial stage is gradually recovered and a strap-on finally results in a safe separation, while fore-body analysis shows collision phenomena between core rocket and booster. And a slight variation of motion is observed from the comparison between inviscid and turbulent analyses. Change of separation trajectory based on viscous effects is just a few percent and therefore, inviscid analysis is sufficient for the simulation of separation motion if the study is focused only on the movement of strap-ons.

• 한국정보통신학회:학술대회논문집
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• 한국해양정보통신학회 2011년도 춘계학술대회
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• pp.336-339
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• 2011

실시간 위치 인식 및 추적 시스템에서 다수의 이동노드가 존재하는 경우 매우 복잡한 데이터 흐름이 발생한다. 단일 게이트웨이가 존재하는 네트워크에서 센서 노드가 수집한 각 종 데이터는 시간이 경과함에 따라 일정한 경로를 따라 전송된다. 멀티게이트웨이가 존재하는 네트워크 구성에서는 수집된 데이터가 단순한 경로가 아닌 다양한 경로를 따라 전송된다. 이러한 데이터는 많은 노드에서 혼잡을 발생시켜 네트워크 성능을 크게 저하 시킨다. 본 논문에서는 기존의 연구와 달리 멀티 게이트웨이를 갖는 수중센서 네트워크 환경에서 효율적인 통신을 위하여 각 노드들 간의 데이터 충돌을 최소화하고 QoS(Quality of Service)를 보장할 수 있는 MAC(Media Access Control) 프로토콜을 제안한다. 제안된 프로토콜에서 데이터 전송을 원하는 소스 노드는 하나의 RTS 패킷을 이용하여 다수의 목적 노드와 한번에 채널 예약을 한다. 소스 노드는 이웃 노드와의 측정된 전파지연 정보를 이용하여 CTS 응답 시간을 스케쥴링(Scheduling) 함으로써 충돌 없이 채널을 예약한다. 예약이 완료된 후 소스 노드는 여러 목적 노드에서 순차적으로 DATA 패킷을 충돌 없이 전송한다. 제안된 프로토콜은 시뮬레이션을 통해 기존 연구에서 제안된 방법과 성능을 비교하고 결과를 분석 및 평가한다. 성능 비교 분석결과, 제안된 방법이 더 좋은 효율과 지여 등의 성능을 가짐을 확인하였다.