• Journal of the Computational Structural Engineering Institute of Korea
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• v.21 no.2
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• pp.199-208
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• 2008

In this paper, to analyze the initial valued non-homogeneous elastic half space by the scaled boundary analysis, the infinite element approach was introduced. The free surface of the initial valued non-homogeneous elastic half space was modeled as a circumferential direction of boundary scaled boundary coordinate. The infinite element was used to represent the infinite length of the free surface. The initial value of material property(elastic modulus) was considered by the combination of the position of the scaling center and the power function of the radial direction. By use of the mapping type infinite element, the consistent elements formulation could be available. The performance and the feasibility of proposed approach are examined by two numerical examples.

• Journal of the Korea institute for structural maintenance and inspection
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• v.13 no.1 s.53
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• pp.125-134
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• 2009

This paper deals with the free vibrations of circular strip foundations which have uniform solid rectangular cross-section. The ground which supports circular strips was modeled as the two parameter elastic foundation. Differential equations governing the flexural-torsional free vibrations of circular strips supported by such foundation were derived, and solved numerically for obtaining the natural frequencies and mode shapes. Boundary condition of free-free ends was considered for numerical examples. Four lowest natural frequencies according to the variations of five system parameters i.e. subtended angle, depth ratio, contact ratio, elasticity ratio and soil parameter are reported in the non-dimensional forms. Also, typical mode shapes of both deformations and stress resultants are presented in the figures. Experiment was conducted for validating the theory developed in this study.

• Tunnel and Underground Space
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• v.16 no.1 s.60
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• pp.58-72
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• 2006

In recent years, not only the occurrences but the magnitude of earthquakes in Korea are on an increasing trend and other sources of dynamic events including large-scale construction, operation of hi띤-speed railway and explosives blasting have been increasing. Besides, the probability of exposure fir rock joints to free faces gets higher as the scale of rock mass structures becomes larger. For that reason, the frictional behavior of rock joints under dynamic conditions needs to be investigated. In this study, a shaking table test system was set up and a series of dynamic test was carried out to examine the dynamic frictional behavior of rock joints. In addition, a computer program was developed, which calculated the acceleration and deformation of the sliding block theoretically based on Newmark sliding block procedure. The static friction angle was back-calculated by measuring yield acceleration at the onset of slide. The dynamic friction angle was estimated by closely approximating the experimental results to the program-simulated responses. As a result of dynamic testing, the static friction angle at the onset of slide as well as the dynamic friction angle during sliding were estimated to be significantly lower than tilt angle. The difference between the tilt angle and the static friction angle was $4.5\~8.2^{\circ}$ and the difference between the tilt angle and the dynamic friction angle was $2.0\~7.5^{\circ}$. The decreasing trend was influenced by the magnitude of the base acceleration and inclination angle. A DEM program was used to simulate the shaking table test and the result well simulated the experimental behavior. Friction angles obtained by shaking table test were significantly lower than basic friction angle by direct shear test.

• Journal of the Korean Society for Marine Environment & Energy
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• v.3 no.1
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• pp.25-34
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• 2000

A panoramic-PIV technique is employed to characterize the travelling tip vortices and the profile of oil-water Interface in the tandem fence arrangement. Instantaneous as well as time-averaged velocity profiles of the water layer close to the interface were obtained to evaluate the possibility of measuring the shear stress distribution on oil-water interface. It was proven that the present technique could provide some qualify data precise enough to resolve detailed flow structures inside a shear layer formed on oil-water interface provided it is nearly stationary.

• Journal of the Society of Naval Architects of Korea
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• v.29 no.3
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• pp.21-32
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• 1992

Numerical solutions are presented for solving the free surface flow created by a three-dimensional body moving beneath the free surface with constant velocity at an angle of attack. The solution is obtained using a panel method based on the perturbation potential, which employs Havelock sources and normal dipoles distributed on the body surface and Havelock normal dipoles in the wake downstream of the trailing edge. A pressure Kutta condition with an iterative solution procedure is implemented to satisfy equal pressure condition on the upper and lower surfaces at the trailing edge. Numerical calculation examples in the present paper include an ellipsoid at zero angle of attack, a rectangular planform wing at a small angle of attack in the limit of zero Froude number and then free surface flows and hydrodynamic forces acting on the submerged spheroid and parabolic strut are calculated. Discussions are made about the validity of the present method.

• The Journal of the Korea Contents Association
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• v.10 no.10
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• pp.451-455
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• 2010

Hydraulics usually deals with flows with free surface. When the surface curvature is small, the assumption of hydrostatic pressure distribution is enough. However, in the case, when the curvature is big, the non-hydrostatic pressure distribution should be taken into account and the Navier-Stokes equations should be employed instead of the depth-averaged shallow water equations. For the simulation of two immiscible fluids with different characteristics (e.g. water and air, water and oil), the level set method is selected for this purpose. The developed model is applied to classical dam break problem and the computational results are compared with the experimental data. The effectiveness of the developed model is confirmed.

• Journal of the Korean Ceramic Society
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• v.11 no.2
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• pp.38-49
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• 1974

운모기판에 증착한 비정형 셀레니움 박막의 결정성장의 형태와 그 변태속도에 대하여 연구하였다 열처리된 박막에서 비정질성분은 CS2에 용해되나 결정질은 아무 변화없이 남아 있으므로 쉽게 현미경을 이용하여 그 모양을 조사할 수 있다. 결정은 (30$^{\circ}$~10$0^{\circ}C$ 온도 범위에서) 박막과 운모기관의 경계면을 따라서 원형상(구상 결정의 이차원 적 모양) 중심으로 부터 일정 속도로 자란다. 또한 필라멘트 형태의 결정이 원형상 결정의 비 규칙적인 부분에서 박막을 뚫고 위로 자란다. 이들 필라멘트형 결정은 자유표면에 도달하여 새로이 자유표면을 따라서 원형상으로 자라게 된다. 경계에 있는 원형상 결정의 두께는 약 500$\AA$정도이고 이것이 비정질 세레니움 박막에서 보이는 "어두어 지는" 현상의 원인이 되고 있음이 밝혀졌다. 원형상 결정은 아주 조그마한 결정 "도메인"으로 구성되어 있으며 이들 "도메인"의 축 방향은 경계면과 나란하고 반경방향에 수직으로 되어 있다. 고온처리에서 얻어지는 규칙적인 결정은 이들 "도메인"이 모여서 "라멜라"를 형성하여 중심부에서부터 뻗어나가고 이들 "라멜라"간의 공간은 불규칙적으로 나열된 "도메인"으로 연결되어 있으며, 고분자 결정에 비하여 훨씬 두껍다. 반경 방향으로의 결정성장 속도는 아주 순도가 높은 박막에서는 시간에 따라 일정하고 주어진 온도에서 재현성이 아주 좋다. 이 실험에서 측정된 성장속도는 지금까지 발표된 어느 실험에서 관측된 것보다 빠르고 또 자유표면에서 자라는 속도에 비해서 약 백 여배나 빠르다. 결장 성장의 온도 의존은 u=6$\times$1015 exp[-32.7(kcal/mol)/RT] cm/sec로 표시할 수 있다.

• Proceedings of the KIEE Conference
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• 2011.07a
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• pp.844-845
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• 2011

스피리컬 전동기의 적용대상인 기존의 다자유도 시스템은 다수의 전동기를 동시에 제어해야 하므로 제어성과 전력공급면에서 단점을 갖는다. 하나의 전동기로 다 자유도 시스템을 구현할 수 있는 스피리컬 전동기는 출력 밀도 측면에서 영구자석을 이용한 형태의 연구가 주로 진행되고 있는데, 세계적으로 기초연구 단계에 있다. 스피리컬 영구자석형 전동기를 구현하기 위해서는 회전자를 지지하면서 3자유도 구현이 가능한 구조적인 설계, 3자유도의 전동력의 발생 메커니즘 설계, 3차원 전자장 해석 및 제어알고리즘 구현이 필요하다. 회전축이 기울여진 상황에서 회전자계를 발생시키는 식이 보고되고 있으나 회전형 전동기와 달리 공증된 회전자계 식이 없는 상황이다. 본 연구에서는 전류벡터를 이용한 회전자계 식에 대한 연구를 진행하였다.

• Journal of the korean Society of Automotive Engineers
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• v.16 no.3
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• pp.19-29
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• 1994

본 연구에서는 상태방정식과 출력방정식에 외란항을 포함하게 된다. 최적조건을 이용하여 외란항을 포함한 리카티 방정식을 유도하고 그로부터 제어로직을 얻을 수 있다. 본 연구에서의 차량 모델링은 스프링 위 질량 3자유도와 스프링 아래 질량 4자유도 운전석의 연직방향 1자유도를 포함한 총 자유도의 선형모델로 하였다. 또 본 연구에서는 예견제어를 이용하였는데 차량앞에 미리 도로면의 정보를 인식할 수 있는 가상적인 측정장치가 있다고 가정하였다. 결과에서는 기존의 수동형 현가장치와 최적제어를 이용한 능동형 현가장치를 구분하고, 예견시간에 따른 차량의 성능을 비교 분석하였다.

• Computational Structural Engineering
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• v.9 no.4
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• pp.181-187
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• 1996

This paper concerns the singular thermal stresses at the interface corner between the elastic fiber and the viscoelastic matrix of a two-dimensional unidirectional laminate model induced during cooling from cure temperature down to room temperature. Time-domain boundary element method is employed to investigate the nature of residual thermal stresses at the interface. Numerical results show that very large stress gradients are present at the interface corner and such stress singularity might lead to local yielding or fiber-matrix debonding.