• Journal of Information Display
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• 제3권3호
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• pp.17-23
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• 2002

In this work we report methods of formation of three-dimensional structures of particles in a liquid crystal host. We found that, under the appropriate conditions, the particles are captured and dragged by the moving isotropic/nematic front during the phase transition process. This movement of the particles can be enhanced significantly or suppressed drastically with the influence of an electric field and/or with changing the conditions of the phase transition, such as the rate of cooling. As a result, a wide variety of particle structures can be obtained ranging from a fine-grained cellular structure to stripes of varying periods to a course-grained "root" structures. Changing the properties of the materials, such as the size and density of the particles and the surface anchoring of the liquid crystal at the particle surface, can also be used to control the morphology of the three-dimensional particle network and adjust the physical properties of the resulting dispersions. These particle structures may be used to affect the performance of LCD's much as polymers have been used in the past.

• 한국정밀공학회지
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• 제14권2호
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• pp.102-112
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• 1997

This paper describes the method that can construct kinematically admissible velocity fields for forging of gear-like components which have tooth shape around the cylinder. The kinematically admissible velo- city fields for the various gear-like components, involute spur gear, trapezoidal spline, square spline, ser- ration and trochoidal gear, were constructed by pilling up the velocity components according to the shape of tooth and billet. The billets, of hollow and solid, were Al 2218 and 2024. To verify the method, the analyses and experiments were carried out and compared with each other. For analyses, the half pitches of com- ponents were divided into several deformation regions based on their tooth profile. A neutral surface was used to represent the inner flow of material during forging. Its location varied with the energy optimazation and its contour varied with the number of teeth. In experiment, the contour of material filling up the tooth zone is hyperbolic curve caused by the frictional drag on the interface of die-wall/workpiece but, in the analysis, it is an arc which retains the same contour during all forging operation.

• 에너지공학
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• 제19권2호
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• pp.116-120
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• 2010

국내 집단에너지 사업의 대표적인 지역난방시스템은 전체 배관망이 약 3,000 km에 이르고 있다. 이러한 장거리 배관망을 통한 열수송에서는 마찰 저항으로 인해 많은 펌프동력이 필요하게 된다. 효율적인 장거리 열수송을 위한 연구로서 대표적인 방법 중 하나가 마찰저감제를 투입하는 것이다. 이러한 마찰저감제는 파이프내 표면의 마찰저항을 감소시킴으로써 유체의 유동을 향상시키게 되는 것이다. 본 연구에서는 친환경 계면활성제인 Amine Oxide $C_{18}$을 이용하여 $80{\sim}110^{\circ}C$의 온도범위에서 단기간 동안에 마찰저감 특성을 비교하고, 장기간 동안 퇴화현상을 비교 평가함으로써 향후 지역난방 시스템에서 적용 가능성을 평가하기 위하여 지역 난방시스템을 축소하여 실험장치를 제작하였다. 마찰저감제를 첨가하지 않은 파이프내의 차압과 마찰저감제를 첨가하였을때의 차압을 비교하여 마찰저감율을 측정하였다. 단기성능 실험결과 마찰저감제는 온도의 영향을 받아 유체의 온도가 높아질수록 마찰저감율이 낮게 나타났다. $80^{\circ}C$의 실험에서 최대 30%의 마찰저감율이 나타났으며, $100^{\circ}C$ 이상에서는 마찰저감율이 감소하여 약 15%의 마찰저감율을 보였다. 장기성능 실험결과 $80^{\circ}C$의 실험에서는 1000 ppm 0.8 m/s의 유속에서 마찰저감율의 지속시간이 155시간동안 유지되었으며 온도가 높아질수록 지속시간이 감소하였다.

• 대한조선학회논문집
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• 제34권1호
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• pp.11-23
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• 1997

본 논문은 선박용 프로펠러 날개단면의 개발 과정을 다루고 있다. 2차원 날개단면의 유체역학적 특성은 캠버 및 두께 분포, 앞날 반경 등 기하학적 형상에 따라 달라진다. 2차원 날개단면 주위의 전 유장을 난류로 고려한 후 해석하기 위해 유한 체적법에 의한 Reynoles time averaged Navier-Stockes 방정식을 이용한 수치해석 기법을 개발하였다. 본 연구에서는 날개단aus 표면에 보다 많은 계산점을 주면서도 받음각의 변화에도 격자계 생성이 용이한 O-Type 격자계를 채택하였고, 전 유동장은 k-${\varepsilon}$ 난류 모형을 적용하여 해석하였다. 본 연구에서 개발된 수치해석 기법은 NACA0012의 실험 결과와 비교하여 계산 정도를 확인하였다. 본 연구에서는 낮은 항력을 갖는 고효율 날개단면 개발을 목표로, 항력이 양호한 날개단면은 공동 터널에서 양력, 항력 및 공동 특성 실험을 수행하였으며, 수치 해석 결과와도 비교하였다. 본 연구를 통하여 개발된 2차원 날개단면 해석용 수치 유체역학 코드는 실험 결과와 잘 일치하고 있음을 알 수 있었다. 이상의 과정을 통하여 기존의의 날개단면인 NACA66 두께 분포와 a=0.8 mean line 캠버를 갖는 KH13보다 효율뿐만 아니라 공동 특성도 우수한 단면인 KH28을 개발할 수 있었다. 새로운 날개 단면인 KH28은 선박용 프로펠러에 적용하기 위한 연구가 지속되어야 하며, 한편 낮은 받음각에서 양-항력 추정의 정확도를 높이기 위해서는 개발된 수치해석 코드에 2-경계층 모형이 적용되어야 할 것으로 본다.

• Journal of the korean society of oceanography
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• 제33권3호
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• pp.53-63
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• 1998

The Princeton ocean model (POM) with free surface in sigma-coordinate, governed by primitive equations, is used to examine the response of sea water in Deukryang Bay to a typhoon. The model reproduces reasonably well the main features in the wind-driven dynamics due to passing of a typhoon. In response to the wind, the coastal jet develops and the upwelling(or downwelling) occurs dominantly in both sides of the bay. This result implies that there should be an overturn in the bay water with the passing of typhoons. Numerical results of POM are also compared to those of a depth-averaged model. From the comparison, it is postulated that the bottom drag coefficient conventionally used for the two-dimensional flow models is inadequate due to overestimation of the computed current field.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회B
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• pp.2857-2861
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• 2007

Flow and aerodynamic characteristics were analyzed numerically for a commercial passenger airplane, Boeing 747-400, flying in the cruising condition. The model geometry with 100:1 in scale was obtained by the photo scanning measurement with the maximum error of 1.4% comparing with the real airplane dimension. The three-dimensional inviscid steady compressible governing equations were solved by the finite volume method in the unstructured grid system. The convective terms were treated by the Crank-Nicholson and first-order upwind schemes. In the computational results, the strong wing-tip vortices were clearly observed and the pressure contours on the airplane surface were suggested. The lift and drag forces in the wing with engines increase by 1.49% and 3.9%, respectively compared with the case without engines. The aerodynamic forces were estimated quantitatively for each element which consists of the airplane.

• Journal of Welding and Joining
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• 제13권2호
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• pp.115-121
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• 1995

As the metal transfer in the GMAW process affects the weld quality and productivity, the mechanism of molten formation and detachment has been investigated at various welding conditions. The force balance and pinch instability models have been widely used to analyze the metal transfer in the globular and spray modes, respectively A new approach is proposed in this work by minimizing the energy of molten drop system. Effects of the surface tension, gravity, electromagnetic and drag forces are considered with no presumed molten drop geometry. Effects of various welding conditions on the metal transfer are explained. The results show that the proposed mode can be applied to the globular and spray transfer modes. When compared with other models, results of the proposed model show better agreements with the available experimental data, which demonstrates the validity of the present model.

• 한국세라믹학회지
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• 제25권4호
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• pp.390-398
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• 1988

Effects of atmospheres and adidtives on the grain growth of TiO2 ceramics were investigated. In the range of 1300~140$0^{\circ}C$, grain growth was increased in CO2 as compared with O2 atmosphere and the grain boundary migration activation energy was lower than the diffusion activation energy of oxygen ion in TiO2. Also, in the case of addition of oxides, the grain growth was increased by oxides acting as a acceptor andinhibited by oxides acting as a donor. From the above results, when the oxygen vacancy concentration was increased, the intrinsic grain boundary mobility was increased and the pore drag force was decreased due to the rapid densification. Also it seems that the pore was migrated by the surface diffusion rather than lattice diffusion.

• 한국전산유체공학회지
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• 제4권3호
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• pp.1-11
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• 1999

This paper describes the flow field analysis of an automobile with crosswind effects of 15°, 30° 45° and 60° of yaw angles. The governing equations of the 3-D incompressible Navier-Stokes equations are solved by the iterative time marching scheme. The Chimera grid technique has been applied to efficiently simulate the flow around the side-view mirror. The computated surface pressure coefficients have been compared with experimental results and a good agreement has been achieved. The A- and C-pillar vortex and other flow phenomena around the ground vehicle are evidently shown. The variation of aerodynamic coefficients of drag, lift, side force and moments with respect to yaw angle is systematically studied.

• Journal of Mechanical Science and Technology
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• 제17권10호
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• pp.1485-1495
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• 2003

We investigate the triboelectrostatic separation of polyvinylchloride (PVC) from mixed plastics in the laboratory scale triboelectrostatic separation system. The flow and electric fields in the precipitator are obtained from the numerical solution of finite volume method. Using these flow and electric fields, we solved the particle motion equation considering the inertia, drag, gravity and electrostatic forces acted on the particles. The particle trajectories are obtained using a Lagrangian method as a function of different important variables such as Reynolds number, Stokes number, electrostatic force, electric charge and electric field distribution, inclined angle of plane electrodes, particle rebounding, particle charge decay rate after impact on the electrode surface, etc., in order to determine the optimal design conditions. The present predicted results for the cumulative yield represent well the experimental ones.