• Proceedings of the Materials Research Society of Korea Conference
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• 2003.03a
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• pp.127-127
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• 2003

전자종이에 대한 관심이 높아지면서 전자잉크의 pigment 소재에 대한 연구가 최근 활발하게 이루어지고 있다. 많은 재료 중 TiO$_2$는 비표면적이 크고 열적안정성 및 명암도가 뛰어나 전자잉크 재료로 많은 장점을 지닌다. TiO$_2$ 나노 입자를 전자종이에 적용할 경우 우수한 디스플레이 구현을 위해 높은 전기영동 특성 및 분산 안정성이 요구되어진다 이를 위해 표면 개질된 나노 크기의 루틸상 TiO$_2$ 입자의 제조 및 분산에 대한 최적의 공정조건에 대해 연구하였다. 10$0^{\circ}C$ 이하의 저온에서 가열하여 균일하게 침전시키는 저온균일침전법(HPPLT)으로 루틸 결정상의 TiO$_2$ 나노입자를 제조하였다. 제조된 TiO$_2$ 나노 입자와 용매의 비중을 맞추기 위해 비중이 낮은 투명성 polymer로 코팅을 한 후 비중병을 이용해 비중을 확인하였다. 그 후 copolymer block을 가지는 분산제를 TiO$_2$ 입자 기준 0.5-5wt% 범위에서 저유전율을 가지는 다양한 유기용매에 첨가하여 최적의 분산 및 전기영동 조건을 찾았다. 실험을 통한 분산안정성 및 전기영동 특성 평가를 위해 ζ-potential analyzer와 입도 분석기를 이용하였고 코팅된 입자의 표면상태는 FT-IR을 통해 측정하였다.

• Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.21 no.8
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• pp.1-9
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• 2007

Characteristics of electrodeless lamp as a load of the ballast are different compared to normal fluorescent lamp because the lame includes an inductance due to coupling magnetics for inductive discharging process. This increased parameter makes the development of self-oscillation type ballast more complex and time consuming. Practical simulation method for an easy design of self-oscillation type ballast especially for Endura lamp, is presented by using a model and various analysis of simulation. Results of experiment are given for a verification of proposed method.

• Journal of the Society of Naval Architects of Korea
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• v.36 no.3
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• pp.60-70
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• 1999

The longitudinal stability characteristics of a Wing-In-Ground Effect Craft are quite different from that of the conventional airplane due to the existence of force and moment derivatives with regard to height. This stability characteristics plays a great role in designing a safe and efficient WIG due to its potential danger in sea surface proximity. The static and dynamic stability criteria are derived from the motion equations of WIG in the framework of small disturbance theory and discussed in the paper. The static and dynamic stability analyses of a 20-passenger WIG are conducted based on the wind tunnel test data and the dynamic motion behaviors are investigated for the change of the design parameters. Finally, the flying quality of the 20-passenger WIG is analysed at the cruising condition according to the military regulations.

• Korean Chemical Engineering Research
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• v.52 no.2
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• pp.199-204
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• 2014

In binary solidification compositional convection in a porous mushy layer influences the quality of the final products. We consider the mushy layer solidifying from below with a constant solidification velocity. The disturbance equations for the mushy layer are derived using linear stability theory. The basic-state temperature fields and the distribution of the porosity in the mushy layer are investigated numerically. When the superheat is large, the thickness of the mushy layer is relatively small compared to the thickness of the thermal boundary layer. With decreasing the superheat the critical Rayleigh number based on the thickness of the mushy layer increases and the mushy layer becomes stable to the compositional convection. The critical Rayleigh number obtained from the continuity conditions of temperature and heat flux at the mush-liquid interface is smaller than that from the isothermal condition at the upper boundary of the mushy layer.

• Journal of Korean Society of Steel Construction
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• v.12 no.2 s.45
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• pp.221-230
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• 2000

Checking the stability of anisotropic plates with free edges, it is impossible that buckling loads and modes are found via existing classical methods about various loads and boundary conditions. For solving this problems. finite difference method(FDM) is used to analyze the buckling behaviors for arbitrary boundary conditions. Using FDM, it is difficult to treat the fictitious points on free edges. So, this paper analyzes buckling behaviors of analytic models with one edge free and the other edges clamped and with opposite two edges free and other two edges clamped. The various buckling loads and mode characteristics through numerical results are given for buckling behaviors of anisotropic plates on free edges.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.2
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• pp.67-74
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• 2005

This paper concerns attitude controller design for a 3-staged launch vehicle which has movable nozzle TVC systems for all stages as its control systems. The PD-type control gains are determined by shaping the corresponding closed-loop natural frequencies for the purpose of guaranteeing the required stability margin. Bending filters are also designed to stabilize the bending modes by using parametric optimization method. The designed controllers are verified using six degree of freedom flight simulations in MATLAB.

• Korean Journal of Optics and Photonics
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• v.4 no.4
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• pp.363-372
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• 1993

An optimization technique with variable orthogonalization and SVD(singular value decomposition) is examined in a double-Gauss type photographic lens design and its convergence and stability are compared with ordinary least squares and DLS(damped least squares) method. It is known that there are close relationship between the stability of optimization and condition number of nomal equation, the ratio between maximum and minimum of eigenvalues. In this study, the stability is greatly improved by limiting the condition number, the SVD, as expeded. The case of DLS with small damping, orthogonalization and SVD shows the most rapid convergence and stability. It means that the unstability of DLS method with small damping is overcome by using the variable orthogonalization and SVD.

• Journal of the Institute of Electronics Engineers of Korea SC
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• v.44 no.4 s.316
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• pp.61-66
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• 2007

PID control is windely used to control stable processes, however, its application to integrating processes is less common. In this paper we proposed a simple PID controller tuning method for integrating processes with time delay to meet a stable specification. With the proposed PID tuning method, we can obtain stable integrating processes using PD controller in inner feedback loop and a loop transfer function with desired stable specification. This guarantees bout robustness and performance. Simulation examples are given to show the good performance of the proposed tuning method to other methods.

• Geotechnical Engineering
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• v.6 no.2
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• pp.47-54
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• 1990

The accuracy of a limit equilibrium analysis of slope stability depends on the accuracy with which the strength properties and geometric conditions can be defined, and on the inherent accuracy of the method of analysis. Most of the slope stability analysis method have been computer coded, and this is a comparative study on the accuracy of these programs. Comparative analyses have shown that for the slopes with relatively simple conditions Host of the programs which are widely used in this country result in the same value of safety factor with an accuracy no worse than $\pm$5%. Similar results can be obtained from the examination of the several slope failure for which accurate information is available on the strength and geometric conditions of the earth slope. The critical failure surface, however, can be different from the actual slip surface, although nearly the same factors of safety are obtained from the analyses of each surface.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2004.07a
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• pp.82-85
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• 2004

Colloidal Silica(CS) HSA/2327과 methyltrimethoxysilane(MTMS), 1034A와 tetramethoxysilane(TMOS)/MTMS 간의 졸겔 반응조건이 코팅도막의 특성에 미치는 영향을 조사하기 위하여 CS종류, CS 대비 TMOS/MTMS의 함량비, 반응시간 등을 달리하여 졸을 합성하고, 합성된 졸을 slide glass에 코팅한 후 $300^{\circ}C$에서 경화시킨 도막의 특성들을 조사하였다. HSA/2327/MTMS에 의한 졸로부터 제조된 코팅도막은 졸 반응시간 의존성이 거의 없으며 반응초기부터 접촉각이 상당히 안정되어 있고 특히 낮은 MTMS 함량을 가진 졸들이 더욱 안정된 표면물성을 보였다. 1034A/TMOS/MTMS에 의해서 제조된 코팅도막은 적절한 소수성의 형성과 표면조도의 향상과 더불어 안정된 접촉각 양상을 나타내었다. 표면거칠기는 HSA/2327 혼합 CS계에 의해서는 반응시간이 길고 MTMS 함량이 높아질 때 비교적 표면조도가 나빠지는데 반응시간과 더불어 약간씩 증가하는 경향을 보였다. 1034A CS계에서는 반응시간과 MTMS 함량의 조건에 영향을 받지 않고 표면조도와 균질성이 우수하였다.