• Proceedings of the Korean Society of Precision Engineering Conference
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• 1993.04b
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• pp.310-314
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• 1993

본 연구에서는 전기유동체의 전기장 부하 변화에따른 역학적특성을 고찰하였다. 유체에 가해지는 전기장은 0 .approx. 2.5 kV/mm 까지 변화시켰고, 외부에서 가해지는 회전력은 0 .approx. 500 rpm 까지의 범위로 하였으며, 용매의 종류를 달리하고 각각의 용매에 대한 중량비를 달리하여 자체 조성한 5종류의 전기유동유체에 대하여특성 고찰하였다. 각각의 전기유동유체는 부하되는 전기장에 대하여 전단력과 전단비의 관계가 선형적으로 증가하였고, 전기유동유체의 항복응력도 부하되는 전기장의함수로 증가함을 알 수 있었다. 또한 부하되는 전기장의 크기뿐만 아니라 입자의 중량비, 용매의 종류도 전기 유동유체의 역학적 특성에많은 영향을 미침을 알 수 있었다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.11a
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• pp.232-236
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• 2006

하이브리드 로켓에서 그레인 전체 부분에서 고른 연소율 향상을 이룰 수 있는 방법으로 스월 유동과 나사산 그레인을 동시에 적용하여 실험을 실시하였다. 그 결과 입구부분과 연료 후반부에 집중된 연소현상을 확인하였다. 스월 유동은 스월 유동의 종류에 상관없이 일정한 감소율을 나타낸다. 그리고 연소율 향상은 연료 벽면에서의 회전 유동 강도에 비례한다고 가정 할 수 있다. 따라서 입구부분의 집중된 연소현상을 해소하고 일정한 연소율 향상을 이룰 수 있는 스월 유동 조건에 대해 연구하였다.

• Proceedings of the Korean Nuclear Society Conference
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• 1998.05a
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• pp.514-519
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• 1998

범용 전산유체해석(computational fluid dynamics) 코드인 CFX를 이용하여 지지격자 형상에 따른 봉다발 부수로에서의 난류유동 수치해석을 수행하였다 ABB와 SIMENS가 각각 개발한 split vane이 부착된 지지격자와 원자력연구소가 개발중인 회전유동 발생장치가 부착된 지지격자를 포함하는 부수로 난류유동을 분석하였다. 각각의 지지격자 형상에 대해 부수로에서의 축방향 속도, 횡방향 속도, 난류 운동에너지, 와류크기와 압력강하 둥을 비교-분석하였다. 세가지 경우 모두 유사한 경향을 나타냈으나 SIMENS split vane의 유동 전향날개가 크기때문에 와류와 압력강하가 다소 크게 예측되었다. 난류 운동에너지와 와류크기는 지지격자 근처에서 현저히 증가한 후 급격히 감소하는 측정결과를 CFX예측결과에서도 확인할 수 있었다. CFX 예측결과는 지지격자 근처에서 실험 결과와 다소 큰 차이를 보였으나 비교적 부수로 유동특성을 잘 나타낸다.

• Journal of Korea Multimedia Society
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• v.8 no.10
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• pp.1322-1328
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• 2005

The circulation flows passing through the Ekman boundary layer on the rotating disk and transfer the angular momentum into the interior region of the container. Consequently, the circulation enhances the momentum transfer and the interior fluid is divided by a propagating shear front. This investigation focuses on computer vision and image processing technique for analysis of Non-Newtonian Fluids. To visualize marching velocity shear front for the transient flow, a particular shaped particles and light are used. To validate the proposed method, quantitative image are compared with the optical data acquired by a direct measurement of LDV (Laser Doppler Velocimetry).

• Proceedings of the KSME Conference
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• 2003.11a
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• pp.622-627
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• 2003

A numerical study is made of a flow in a cylinder with a rotating grooved endwall disk. The aim is to describe differences in the flow fields when there is concentrically-grooved obstacle characterized by amplitude(a) and wave number(N). The Reynolds number(Re) is varied from $10^{3}$ to $10^{4}$ and the aspect ratio(Ar) fixed to 1.0 for the most part of the simulation. For the various cases of amplitude(a) and wave number(N), numerical results are acquired. As the endwall groove roughness increases until certain limit, the interior azimuthal velocity component(v) increases drastically. But over the limit, the swirl motion chararcterized by velocity v decreases and finally it approaches much alike Ar=1.0-a case. The reason of activating swirl motion is based on increasing of torque transported by endwall disk. Torque coefficients($C_{T}$) are aquired for the various (a,N,Re) combinations and the limiting phenomena of swirl motion activation is explained.

• The Transactions of the Korean Institute of Electrical Engineers
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• v.39 no.10
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• pp.1066-1074
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• 1990

In this paper, we attempt to control induction motors with high power efficiency as well as high dynamic performance by utilizing the recently developed theories : singular perturbation technique and noninteracting feedback control. Our controller consists of three subcontrollers` a saturation current controller, a decoupling controller, and a well-known flux simulator. The decoupling controller decouples rotor speed (or motor torque) and rotor flux linearly. Our controller does not need the rotor resistance that varies widely with the machine temperature. To illuminate the practical significance of our results, we present simulation and experimental results as well as mathematical performance analysis.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.22 no.3
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• pp.346-359
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• 1998

The aerodynamic forces and wake structure of the non-rotating downstream circular cylinder, of which the uniform freestream flow is interfered with another spinning upstream cylinder having the same diameter that is located upstream in a line have been investigated experimentally. When the spin rate of the downstream cylinder defined as the ratio of tangential surface velocity of the spinning cylinder to the freestream velocity increases gradually from zero to 1.4, the change of surface pressure distribution, aerodynamic forces of the non-rotating downstream cylinder were measured in case of several distance ratios of 1.5, 3.0, and 4.5 defined as the ratio of distance between the centers of two cylinders to the diameter. The wake flow patterns behind the cylinder were also investigated in each case. From the present experiments, it has been found that the spin rate significantly influences the aerodynamic forces and near-wake flow phenomena of the downstream cylinder in such a way that the drag increases as the spin rate and distance ratio increase and the wake width increases as the distance ratio increases.

• Journal of the Korean Crystal Growth and Crystal Technology
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• v.3 no.1
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• pp.18-30
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• 1993

A numerical analysis has been carried out on the Czochralski flow fields when uniform and nonuniform magnetic fields are applied. Czochralski flow fields are governed by buoyancy forces, thermocapillarity, centrifugal forces, and applied magneic fields. In this analysis, pressure and three components of velocity vectors are obtained, and circumferential electrical currents are calculated. When a uniform magnetic field is applied, all the velocity components are decreased and the circumferential electric currents near the crystal surface are increased as the magnetic field intensity is increased. In the case of a nonuniform field, the flows in a meridional plane are suppressed and the circumferential velocity is increased as the non uniformity is increased. The understanding on the Czochralski flow fields under the influence of magnetic fields can lead to the study on the behavior of the concentration of the solute and impurities.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.2
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• pp.22-31
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• 2005

A design study was conducted for a new concept aircraft(Canard Rotor/Wing: CRW) that has the capability of dual mode flight, a rotorcraft and a fixed wing mode. The CRW can show a vertical take off/landing and a high speed/efficiency cruise performance simultaneously. It is not surprising to develop a new sizing code for this class of aircraft because conventional sizing codes developed solely for either the rotary wing or the fixed wing aircraft are not adequate to design a dual mode aircraft operated both by the rotary wing through tip jet effux and the fixed wing lift. Thus, a new design code was developed based on the conventional sizing code by adding some features including rotor performance, duct flow, and engine flow analysis, hence could eventually predict the performance of reaction driven rotor, the flight performance and the flight characteristics. The various design parameters were investigated to find their influences on the flight performance then, a small UAV(Unmanned Aircraft Vehicle) of 1500 lbs class was optimally designed to have minimum weight using the developed sizing code.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.20 no.7
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• pp.347-352
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• 2019

This study focused on improving the cast quality of small-sized induction motor rotors during the die casting process. A new rotor core cast model was proposed based on previous research results and parametric studies. Numerical analyses using 3-dimensional half models were performed to evaluate the filling patterns of aluminum molten metals into a mold and on-site experiment performed to verify the newly proposed cast model. The following were obtained from numerical filling analyses and experimental results. First, molten metals started to fill the lower end ring, then moved on to fill the core slot and upper end ring and finally stopped to fill at the rotor core slot. Second, significant circulation of molten metals was not observed on the lower end ring, resulting in fewer defects at the section of the lower end ring from the experimental results. Third, the new shape of a rotor core cast was effective in producing rotors with sound cast quality, and reducing the end ring cast defect area by approximately 70 %.