• Journal of computational fluids engineering
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• v.2 no.1
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• pp.46-53
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• 1997

The flow field around a three dimensional minivan-like body has been simulated. This study solves 3-D unsteady incompressible Navier-Stokes equations on a non-orthogonal curvilinear coordinate system using second-order accurate schemes for the time derivatives, and third/second-order scheme for the spatial derivatives. The Marker-and-Cell concept is applied to efficiently solve continuity equation. A H-H type of multi-block grid system is generated around a three dimensional minivan-like body. Turbulent flows have been modeled by the Baldwin-Lomax turbulent model. To validate present procedure, the flows around the Ahmed body with 12.5° of slant angle are simulated. A good agreement with other numerical results is achived. After code validation, the flows around a mimivan-like body are simulated. The simulation shows three dimensional vortex-pair just behind body. The flow separation is also observed on the rear of the body. It has concluded that the results of present study properly agreed with physical flow phenomena.

• Proceedings of the KSME Conference
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• 2001.11b
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• pp.934-939
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• 2001

In computational study of the flow in piston engines and the flow through moving valves, the use of moving vertices is essential for modelling flows with moving boundaries. The positions of cell vertices in such cases must be allowed to vary with time. To simulate 3-dimensional port-valve and piston-cylinder of HIMSEN 6H21/32 engine, a commercially available code, STAR-CD, was used. Changes in mesh geometry was specified by PROSTAR commands.(i.e. the Change Grid operation in the EVENTS command module.) Control of the intake flow is expected to play an important role as designers seek to obtain better fuel spray characteristics, fuel mixing and mixture preparation, combustion performance, and emissions reductions to meet national standards. As a result of analysis, velocity fields indicate the presence of a structured flow comprised of one pair of counter-rotating vortices under the intake valve during the early induction process. These flow structures remain visible for most of the intake process. As the piston moves towards BDC, these vortices develops into a larger tumbling motion that dominates the flow structure.

• 한국태양에너지학회:학술대회논문집
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• 2012.03a
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• pp.153-159
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• 2012

In photovoltaic system, the characteristic of photovoltaic module such as open circuit voltage and short circuit current will be changed because of cell temperature and solar radiation. Therefore, a boost converter of the PV system connects between the output of photovoltaic system and DC link capacitor of grid connected inverter as controlling duty ratio for maximum power point tracking(MPPT). This paper shows the dynamic characteristic of the boost converter by comparing single-loop control algorithm and two-loop control algorithm using both analog and digital control. The proposed both compensation method has been verified with computer simulation and simulation results obtained demonstrate the validity of the proposed control schemes.

• 한국태양에너지학회:학술대회논문집
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• 2012.03a
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• pp.427-432
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• 2012

This paper proposes efficient operation method of PV system consisted of multi-central which is suitable for large scale system. The multi-central system used switch at a DC-link and applied proposed algorithm can improve the efficiency and the reliability on the existing system. This algorithm, with advantage of Multi-Central system can minimize the effect of different characteristic of each PV array due to a shadow or damaged PV cell. Each system is analysed and maximum power point tracking control, DC-link voltage control and output current control is used commonly. The validity is verified after comparing of the existing system and proposed system by simulation.

• Journal of the Institute of Electronics Engineers of Korea TC
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• v.37 no.9
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• pp.24-29
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• 2000

As a result of the continuing increase in the high capacity and high speed requirement, ATM will be important technology. But previous AAL type cant support service that is variable length, low speed. So AAL2 is the most recently standardized AAL type, which is aimed at providing for the bandwidth efficient transmission of low-rate, short, and variable length packets in delay-sensitive applications. In this paper, we propose the architecture and the behavior of scalable AAL2 switch that are far different from ATM switch. Also, the performance of the designed switch is analyzed by computer simulation.

• Proceedings of the KIEE Conference
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• 2008.07a
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• pp.1283-1284
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• 2008

염료감응형 태양전지는 투명성과 광입사각 둔감성 등의 장점을 바탕으로 미래 태양전지 시장을 주도할 수 있을 것으로 기대되고 있다. 이러한 염료감응형 태양전지의 실용화를 위해서는 고효율 연구뿐만 아니라 대면적화를 통한 용량의 증대 연구도 요구된다. 본 연구에서는 금속 재료로 염료감응형 태양전지 내에 그리드 전극을 삽입함으로써 전자 및 홀의 이동 개선과 확산 이동의 최소화에 의한 손실 감소를 통해 효율 향상을 시도했다. 또한, 투명전극의 레이저 식각을 통해 염료감응형 태양전지의 내부 저항 중 큰 비중을 차지하는 투명전극의 표면 저항도 줄이고자 했다. SEM을 통해 투명전극의 식각 상태를 확인하고, radio frequency 스퍼터를 통해 그리드 전극을 증착한 결과, 기존 셀보다 향상된 출력전류 및 fill factor를 얻을 수 있었고, 약 1%의 효율 증가를 확인할 수 있었다.

• 한국전산유체공학회:학술대회논문집
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• 1999.11a
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• pp.167-173
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• 1999

An Euler-based CFD tool has been developed for the performance evaluation of a thrust reverser mounted on a high bypass ratio turbofan engine. The computational domain surrounded by the ground and non-reflection boundary includes the whole nacelle configuration with a deployed thrust reverser. The numerical algorithm is based on the modified Godunovs scheme to allow the second order accuracy in both space and time. The grid system is generated by using eleven multi-blocks, of which the total cell number is 148,400. The thrust reverser is modeled as if it locates at the nacelle simply in all circumferential direction. The existence of a fan and an OGV(Outlet Guide Vane) is simulated by adopting the actuator disk concept, in which predetermined radial distributions of stagnation pressure ratio and adiabatic efficiency coefficient are used for the rotor type disk, and stagnation pressure losses and flow outlet angles for the stator type disk. All boundary conditions including the fan and OGV simulation are treated by Riemann solver. The developed solver is applied to a turbofan engine with a bypass ratio of about 5.7 and the diameter of the fan cowl of 83 inch. The computational results show that the Euler-based inviscid method is very useful and economical to evaluate the performance of thrust reversers.

• 한국전산유체공학회:학술대회논문집
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• 1996.05a
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• pp.99-104
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• 1996

The jet pump is being used in many fields for several purposes because of its simple construction and easy operation. The characteristics of the geometrical variables, pressure gradient and velocity distribution of the jet pump are studied using the CFD technique. The flow calculations through a bended nozzle. a mixing chamber and a venturi are presented and phenomenological aspects are discussed. This study solve 3-D steady incompressible Navier-Stokes equations using the Iterative time marching scheme. The governing equations are differenced with 1st-order accurate backward difference scheme for the time derivatives and 3rd-order accurate QUICK scheme for the convective terms. The Mark-and-cell concept was applied efficiently to solve continuity equation, which is differenced 2nd-order accurate central differenced scheme. The 4th-order artificial damping is added to the continuity equation for numerical stability. A O-type of grid system is generated inside a nozzle and venturi of the jet pump. It has concluded that the results of present study properly agree with physical flow phenomena.

• Proceedings of the KSME Conference
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• 2000.04a
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• pp.900-907
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• 2000

The three-dimensional turbulent flow in curved pipes susceptible to flow-accelerated corrosion has been analyzed numerically to predict the pressure and shear stress distributions on the inner surface of the pipes. The analysis employs the body-fitted non-orthogonal curvilinear coordinate system and a standard $ {\kappa}-{\varepsilon}$ turbulence model with wall function method. The finite volume method is used to discretize the governing equations. The convection term is approximated by a high-resolution and bounded discretization scheme. The cell-centered, non-staggered grid arrangement is adopted and the resulting checkerboard pressure oscillation is prevented by the application of a modified version of momentum interpolation scheme. The SIMPLE algorithm is employed for the pressure and velocity coupling. The numerical calculations have been performed for two curved pipes with different bend angles and curvature radii, and discussions have been made on the distributions of the primary and secondary flow velocities, pressure and shear stress on the inner surface of the pipe to examine applicability of the present analysis method. As the result it is seen that the method is effective to predict the susceptible systems or their local areas where the fluid velocity or local turbulence is so high that the structural integrity can be threatened by wall thinning degradation due to flow-accelerated corrosion.

• Proceedings of the Korean Vacuum Society Conference
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• 2010.08a
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• pp.319-319
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• 2010

칼코젠계 태양전지의 광흡수층으로 사용되는 CuInSe2은 직접천이형 반도체로 광흡수계수가 $1{\times}105cm-1$로 매우 높고, 전기광학적 안정성이 우수하여 실리콘 결정질 태양전지를 대체할 고효율 태양전지로 각광받고 있다. 광흡수층의 밴드갭 에너지가 증가하면 태양전지의 개방전압(Voc)이 증가하여 광변환 효율을 향상시킬 수 있으므로, CuInSe2에서 In의 일부를 Ga으로 치환하여 에너지 밴드갭의 변화를 주는 연구가 많이 진행되고 있다. 그러나 화합물내의 Ga 조성비가 증가하면 단락전류(Jsc), 충진률(fill factor)이 낮아져 태양전지 효율을 저하시키게 되므로 CIGS 박막의 적절한 화합물 조성비를 갖도록 최적조건을 확립하는 것이 매우 중요하다. 본 실험에서는 광흡수층 형성을 위해 Sputtering법으로 금속 전구체를 증착하고, 고온에서 셀렌화 열처리를 수행하는 Sequential process(2단계 증착법)를 이용하였다. soda-lime glass 기판에 Back contact으로 Mo를 증착하고, 1단계로 CuIn0.7Ga0.3 조성비의 타겟을 이용하여 Sputtering법으로 $0.5{\sim}2{\mu}m$ 두께의 CIG 전구체를 증착하였다. 2단계로 CIG 전구체의 셀렌화열처리를 통하여 CIGS 화합물 구조의 박막을 형성시켰다. 이때 형성된 CIGS 화합물 박막의 두께는 동일하게 함으로써, 열처리온도에 의한 박막의 구조변화를 비교하였다. 증착된 CIGS 박막은 고온 엑스선회절분석을 통해 증착 두께와 온도 변화에 따른 CIGS 층의 구조 변화를 확인하고, 동일한 증착조건으로 Buffer layer, Window layer, Grid 전극을 형성하여 태양전지셀 특성을 평가함으로써 CIGS 태양전지 광흡수층의 결정구조에 따른 광변환 효율을 비교하였다.