• Structural Engineering and Mechanics
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• 제75권5호
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• pp.621-631
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• 2020

A laboratory experiment is conducted is to investigate the behaviour of a low-mass-ratio and high aspect ratio flexible cylinder under vortex-induced vibration (VIV). A flexible cylinder with aspect ratio of 100 and mass ratio of 1.17 is towed horizontally to generate uniform flow profile. The range of Reynolds number is from 1380 to 13800. Vibration amplitude, in-line and cross-flow frequency response, amplitude trajectory, mean tension variation and hydrodynamic force coefficients are analyzed based on the measurement from strain gauges, load cell and CCD camera. Experimental results indicate that broad-banded lock-in region is found for the cylinder with a small Strouhal number. The frequency switches in the present study indicates the change of the VIV phenomenon. The hydrodynamic force responses provide more understanding on the VIV of a low mass ratio cylinder.

• Carbon letters
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• 제16권2호
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• pp.107-115
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• 2015

Impact damages induced by a low-velocity impact load on carbon fiber reinforced polymer (CFRP) composite plates fabricated with various stacking sequences were studied experimentally. The impact responses of the CFRP composite plates were significantly affected by the laminate stacking sequences. Three types of specimens, specifically quasi-isotropic, unidirectional, and cross-ply, were tested by a constant impact carrying the same impact energy level. An impact load of 3.44 kg, corresponding to 23.62 J, was applied to the center of each plate supported at the boundaries. The unidirectional composite plate showed the worst impact resistance and broke completely into two parts; this was followed by the quasi-isotropic lay-up plate that was perforated by the impact. The cross-ply composite plate exhibited the best resistance to the low-velocity impact load; in this case, the impactor bounced back. Impact parameters such as the peak impact force and absorbed energy were evaluated and compared for the impact resistant characterization of the composites made by different stacking sequences.

• 대한전기학회논문지:전기기기및에너지변환시스템부문B
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• 제54권12호
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• pp.592-600
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• 2005

In this paper, a low loss magnetic levitation(Maglev) system is suggested and tested. The suggested Maglev system includes four hybrid magnets which consist of permanent magnet and coil. In the steady state, the levitated module system can be supported by attraction force generated by permanent magnet. The coil current controls only dynamic loads due to external disturbances. The module systems are designed by using finite element method(FEM) software tools such as MAXWELL and ANSYS. Also, digital control systems are designed to keep the magnet airgap at a constant value. The control systems include a VME(versa module europa)-based CPU(central processing unit) board, AD(analog to digital) board, PWM(pulse width modulation) board, 4-quadrant chopper, and sensors. In order to estimate the vertical velocity of the magnet, we use second order state observer with acceleration and gap signals as input and output signals, respectively. The characteristics of the suggested low loss Maglev system are demonstrated by experimental results showing coil current of 0A in the steady state of 3m airgap and performance specifications are satisfied for reference gap and force disturbance.

• Journal of Ship and Ocean Technology
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• 제12권2호
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• pp.41-52
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• 2008

The development of a high-lift rudder is needed because low speed full ships such as the VLCC(Very Large Crude oil Carrier) have difficulty for obtaining enough lifting force from a common rudder. The rudder of a ship is generally positioned behind the hull and propeller. Therefore, rudder design should consider the interactions between hull, propeller, and rudder. In the present study, the FLUENT code and body fitted mesh systems generated by the GRIDGEN program are adopted for the numerical simulations of flow characteristics around a rudder that is interacting with hull and propeller. Sliding mesh model(SMM) is adopted to analyze the interaction between propeller rotation and wake flow behind hull. Several numerical simulations are performed to compare the interactions such as hull-rudder, propeller-rudder, and hull-propeller-rudder. Also, we consider relationships between the interactions. The results of present numerical simulations show the variation of flow characteristics by the interaction between hull, propeller, and rudder, and these results are compared with an existing experimental result. The present study demonstrates that numerical simulations can be used effectively in the design of high-lift rudder behind low speed full ship.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2002년도 추계학술대회 논문집
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• pp.1055-1058
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• 2002

The movement of bone fluid from the region of the bone vasculature through the canaliculi and the lacunae of the surrounding mineralized tissue accomplishes three important tasks. First it transports nutrients to the osteocytes in the lacunae buried in the mineralized matrix. Second, it carries away the cell waste. Third, the bone fluid exerts a force on the cell process, a force that is large enough for the cell to sense. This is probably the basic mechanotrasduction mechanism in bone, the way in which bone senses the mechanical load to which it is subjected. The mechanism of bone fluid flow are described below with particular emphasis on mechanotransduction. Also described is the cell to cell communication by which higher frequency signals might be transferred, a potential mechanism in bone by which the small whole tissue strain is amplified so the bone cells can respond to it. One of the conclusions is that higher frequency low amplitude strains can maintain bone as effectively as low frequency low amplitude strains can maintain bone as effectively as low frequency high amplitude strains. This mechanism has many similarities with the mechanotransduction of acoustical signals in the ear. These conclusion leads to a paradigm shift in how to treat osteoporosis and how to cope with microgravity.

• 접착 및 계면
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• 제16권4호
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• pp.137-145
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• 2015

본 연구에서는 현재 문화재 보존 처리에 사용되고 있는 합성수지를 대체하여 금속, 목재, 도자기, 토기, 석재 유물 등 재질별 문화재 복원 작업에 활용할 수 있는 다목적용 접합, 복원재료인 에폭시 퍼티(epoxy putty)를 개발하고자 하였다. 기존에 사용되고 있는 합성수지는 높은 강도로 인한 절삭력의 문제, 긴 경화 시간으로 인한 처짐 현상, 도구나 장갑에 묻어 유물의 표면을 오염시키는 현상, 재료의 황변 현상으로 인한 재처리 등의 문제점을 보이고 있다. 이를 해결하기 위해, 1차적으로 문화재 보존 처리 현장에서 가장 많이 사용되고 있는 페이스트(paste)형태의 복원 재료를 선정하여 물성을 파악한 후 이를 비교 대상으로 선택하고, 주제 및 경화제와 충전제의 종류에 따른 에폭시 퍼티를 개발하였다. 개발된 에폭시 퍼티는 기존 재료의 문제점 해결 및 유사한 물성을 지니기 위해 성상(性狀)이 다른 주제와 경화제를 각각 선정하여 물성 실험을 실시하였다. 연구 결과 2종 모두 페이스트 형태로 경화 시간은 5~10 min 내외로 기존 재료에 비해 약 3~10배 정도 짧아 작업의 편리성과 처짐 현상을 개선하였으며, 절삭력을 높이기 위한 마모율은 약 3배 정도 향상시켜 쉽게 성형할 수 있도록 하였다. 또한 작업 중 발생하는 표면 오염 등의 단점을 보완하기 위해 충전제로 탈크(talc)와 백색의 micro-balloon을 첨가하여 사용 중 손에 묻어 나와 끈적거리는 현상을 줄여주었을 뿐만 아니라 컬러링(coloring), 경량성, 절삭력 등이 높은 저수축, 저황변, 절삭력이 우수한 다목적 복원 재료를 개발하였다.

• 대한전자공학회논문지TC
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• 제45권10호
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• pp.49-58
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• 2008

본고 및 연구를 통하여 JEM(Jet Engine Modulation)의 특성 및 기본원리를 파악하며, 실제 항공기 중 저속항공기의 RCS 및 JEM을 측정하는 것이 목적이다. 측정시에는 원하지 않는 여러 오차들이 발생하게 되는데 여러 오차를 제거하기 위해 교정(Calibration)방법을 사용하게 되는데 본고에서는 IACT(Isolated Antenna Calibration Technique)방법을 사용하였다. 측정은 옥외(Outdoor)에서 이루어졌으며 항공기는 공군에서 운용하고 있는 T-103을 표적으로 측정하였다. T-103에 대한 JEM스펙트럼을 추출하며 고정된 표적에 대한 주파수 특성과 도플러에 의한 변화를 판단하는 것이다. 주파수는 일반적인 공대공 항공기에서 운용되는 X밴드를 사용하여 측정하였으며 공대공 항공기에서 저속항공기를 식별하는데 있어 측정을 통하여 분석하였다.

• 대한기계학회논문집
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• 제17권5호
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• pp.1193-1201
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• 1993

본 연구에서는 통계학적 이론 및 희귀분석에 근거한 보정함수를 모델 수정에 도입하여 조업조건별로 예측오차 요인들을 제거함으로써 예측 모델의 정도를 향상시키 고자 하였다. 이를 위해 일반강에 비해 압연하중 모델의 예측정도가 상대적으로 낮은 극저탄소강을 대상으로 하여 압연조업에 따른 압연하중 예측모델의 오차요인을 조업인 자별로 분석하였고 적용시켜 모델의 적중도를 향상시켰다.

• Tribology and Lubricants
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• 제22권5호
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• pp.243-251
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• 2006

Molecular dynamics simulations of nanoimprint lithography NIL) are performed in order to investigate effects of process parameters, such as stamp shape, imprinting temperature and adhesive energy, on nanoimprint lithography process and pattern transfer. The simulation model consists of an amorphous $SiO_{2}$ stamp with line pattern, an amorphous poly-(methylmethacrylate) (PMMA) film and an Si substrate under periodic boundary condition in horizontal direction to represent a real NIL process imprinting long line patterns. The pattern transfer behavior and its related phenomena are investigated by analyzing polymer deformation characteristics, stress distribution and imprinting force. In addition, their dependency on the process parameters are also discussed by varying stamp pattern shapes, adhesive energy between stamp and polymer film, and imprinting temperature. Simulation results indicate that triangular pattern has advantages of low imprinting force, small elastic recovery after separation, and low pattern failure. Adhesive energy between surface is found to be critical to successful pattern transfer without pattern failure. Finally, high imprinting temperature above glass transition temperature reduces the imprinting force.

• Tribology and Lubricants
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• 제20권2호
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• pp.68-76
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• 2004

Applying a general Galerkin FE lubrication analysis method to spiral groove dry gas seals, this study intends to analyze in detail the effects of groove design parameters, such as a spiral angle, groove width ratio, groove radius ratio, groove depth ratio, and groove taper ratio, on the lubrication performances of an opening force, leakage, axial stiffness and damping, and angular stiffness and damping at low and high rotating speeds: 3,600 and 15,000 nm. Results show that, for the primary design consideration performances such as the opening force and axial and angular stiffnesses, a spiral angle of $25^{\circ}$, a groove width ratio of 0.46, a groove radius ratio of 1.1, a groove depth ratio of 1.0, and a groove taper ratio of 0.0 are preferred. Where the recommended relatively low values of groove depth and taper ratios are to keep the axial and angular dampings positive or higher than 0 particularly at the high rotating speed.