• Bulletin of the Korean Chemical Society
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• 제7권3호
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• pp.194-196
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• 1986

The effect of the non-Coulombic long-range forces and the next nearest neighbor interactions on the lattice properties of alkali halide crystals is calculated using the Electron Gas model and Electron Gas Drude model. It is found that these often neglected interactions make changes in the lattice properties that are indeed small, but by no means negligible.

• 한국도로학회논문집
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• 제12권4호
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• pp.11-16
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• 2010

보행교통류를 주제로 다양한 연구들이 진행되었지만 초기의 보행연구는 차량의 교통류이론을 그대로 적용하여 해석하기도 하였다. 최근 보행교통류에 대한 다양한 모형들이 제시되고 있으며, 특히 CA모형은 보행교통류를 위한 시뮬레이션 모형으로 빈번하게 사용되고 있다. 대표적인 CA 모형으로 가스입자의 움직임을 이용하여 양방향의 보행교통류를 설명하기도 하였는데 초기에는 정방형의 Gas-lattice 모형이 제안되었으며 이후에 정육방 Gas-lattice 모형을 이용하여 보행자의 움직임과 회피를 묘사하기도 하였다. 하지만 이러한 모형들은 보행자의 움직임을 편의임의보행으로 가정하였기 때문에 단일방향으로의 움직임만을 설명할 수 있었다. 본 연구에서 제시된 MLPM(the Multi-Layer Pedestrian Model)은 어떤 공간에서 복수개의 기종점을 가진 경우에도 현실적인 보행자의 움직임을 설명할 수 있는 모형이다.

• 한국해양환경ㆍ에너지학회지
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• 제12권3호
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• pp.197-201
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• 2009

다상유동의 상분리 시뮬레이션 기법으로 Lattice-Boltzmann방법(LBM)을 이용하였다. 기체와 액체상사이의 경계면에서 마이크로한 상호교환을 LBM의 등가함수에서 취급하고 있으며, Van-der-Walls의 free energy를 도입하였다. 표면에너지에 따라 상경계면의 기울기의 변화, 온도에 따른 상분리 특성등을 조사하고, 일정 온도상에서 기체와 액체의 상분리 시뮬레이션을 수행하였다.

• 전기화학회지
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• 제5권2호
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• pp.79-85
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• 2002

열역학적 관점에서 몬테 카를로 방법의 전기화학적 리튬 인터칼레이션에로의 응용에 대하여 다루었다. 우선 통계 열역학의 앙상블, Ising 및 lattice gas 모델의 기본 개념을 간단히 소개하였고, lattice gas 모델에 근거한 몬테카를로 방법을 사용하여 전이금속 산화물내로의 리튬 인터칼레이션의 열역학을 해석하였다. 특히 $LiMn_2O_4$전극에 대해 전극 포텐셜 곡선과 리튬 이온의 부분 몰 내부에너지와 엔트로피와 같은 열역학적 특성을 다루었고, 이로부터 리튬 인터칼레이션의 전기화학분야에서 몬테 카를로 방법의 유용성을 확인하였다

• 한국해양환경ㆍ에너지학회지
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• 제19권2호
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• pp.111-119
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• 2016

기체-액체 이상유동의 거동 시뮬레이션을 위해 Lattice Boltzmann방법(LBM)을 이용하였다. 기체-액체사이의 경계면에서 상호포텐셜 모델인 Shen-Chan방식과 Carnahan-Starling 상태방정식을 도입하였다. 또한 외력항의 처리는 Exact Difference Method를 사용하였다. 개발된 코드를 통하여 상태방정식 특성파악, 기체-액체의 상분리, 표면장력 및 기체 액체 경계면 거동 특성, Homogeneous와 Heterogeneous 캐비테이션, 기포 붕괴등의 시뮬레이션을 수행하였다.

• Journal of Mechanical Science and Technology
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• 제16권10호
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• pp.1327-1335
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• 2002

The shock wave process represents an abrupt change in fluid properties, in which finite variations in pressure, temperature, and density occur over the shock thickness which is comparable to the mean free path of the gas molecules involved. This shock wave fluid phenomenon is simulated by using the finite difference lattice Boltzmann method (FDLBM). In this paper, a new model is proposed using the lattice BGK compressible fluid model in FDLBM for the purpose of speeding up the calculation as well as stabilizing the numerical scheme. The numerical results of the proposed model show good agreement with the theoretical predictions.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 춘계학술대회
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• pp.1827-1832
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• 2003

In this research, the simulation method for acoustic sounds by a uniform flow around a two-dimensional circular cylinder by using the finite difference lattice Boltzmann model is explained. To begin with, we examine the boundary condition which determined with the distribution function $f_i^{(0)}$ concerning with density, velocity and internal energy at boundary node. Very small acoustic pressure fluctuation, with same frequency as that of Karman vortex street, is compared with the pressure fluctuation around a circular cylinder. The acoustic sound' propagation velocity shows that acoustic approa ching the upstream, due to the Doppler effect in the uniform flow, slowly propagated. For the do wnstream, on the other hand, it quickly propagates. It is also apparently the size of sound pressure was proportional to the central distance $r^{-1/2}$ of the circular cylinder. The lattice BGK model for compressible fluids is shown to be one of powerful tool for simulation of gas flows.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집B
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• pp.468-474
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• 2001

The shock process represents an abrupt change in fluid properties, in which finite variations in pressure, temperature, and density occur over a shock thickness which is comparable to the mean tree path of the gas molecules involved. The fluid phenomenon is simulated by using finite difference lattice Boltzmann method (FDLBM). In this research, the new model is proposed using the lattice BGK compressible fluid model in FDLBM for the purpose of shortening in calculation time and stabilizing in simulation operation. The numerical results agree also with the theoretical predictions.

• 한국해양공학회지
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• 제18권2호
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• pp.10-17
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• 2004

In this research, a numerical simulation for the acoustic sounds around a two-dimensional circular cylinder in a uniform flaw was developed, using the finite difference lattice Boltzmann model. We examine the boundary condition, which is determined by the distribution function concerning density, velocity, and internal energy at the boundary node. Pressure variation, due to the emission of the acoustic waves, is very small, but we can detect this periodic variation in the region far from the cylinder. Daple-like emission of acoustic waves is seen, and these waves travel with the speed of sound, and are synchronized with the frequency of the lift on the cylinder, due to the Karman vortex street. It is also apparent that the size of the sound pressure is proportional to the central distance to the circular cylinder. The lattice BGK model for compressible fluids is shown to be a powerful tool for the simulation of gas flaws.

• 한국마린엔지니어링학회:학술대회논문집
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• 한국마린엔지니어링학회 2006년도 전기학술대회논문집
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• pp.269-270
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• 2006

A finite difference lattice Boltzmann model which allows us to simulate gas-liquid two-phase flows with large density difference, for instance, 800 times for air and water is considered. Two-particle model is used and the density difference is introduced by changing the acceleration according to the fluid density. Numerical measurement of surface tension agrees well with theoretical predictions. Simulations of two-phase phenomenon for phase-transition is carried out, showing applicability of the model for two-phase flows. The two-dimensional cavitating flow around a board set up in the fluid way is also simulated. As a result, it was confirmed that the FDLB method with two-particle model was effective in numerical simulation of cavitating flow and the bubble periodically grew up at the low pressure area behind the board, in which the fluid condition was influenced by the cavitation number.