• 항공우주시스템공학회지
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• 제15권1호
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• pp.86-94
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• 2021

PCB 기반 전개형 태양전지판은 경량화 및 전기적 연결의 용이성으로 주로 큐브위성에 사용되나, 태양전지판의 면적이 증가할수록 발사환경에서 유발되는 굽힘거동이 증가하기 때문에 태양전지셀의 구조건전성 보장에 한계가 있다. 종래에는 태양전지판의 강성증가를 통해 굽힘거동을 최소화하고자 알루미늄 및 복합재 기반의 보강재를 또는 태양전지판을 적용하였지만, 태양전지판의 부피 및 무게 증가로 제한적인 설계요구조건을 가진 태양전지판의 단점으로 작용한다. 본 연구에서는 점탄성 테이프로 다층 박판을 적층하여 고댐핑 특성 구현이 가능한 6U 규격의 고댐핑 적층형 태양전지판을 제안하였다. 제안된 태양전지판의 기본특성파악을 위해 자유감쇠시험을 수행하였으며, 인증수준의 발사진동시험을 통해 설계유효성을 입증하였다. 또한, 시험결과를 토대로 일반 PCB 태양전지판과 고댐핑 적층형 태양전지판의 진동특성을 예측하고 비교분석을 수행하였다.

• 전기전자학회논문지
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• 제27권4호
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• pp.644-649
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• 2023

DRAM(Dynamic Random Access Memory) 스케일링 과정에서 발생하는 셀간 거리의 감소에 따라 STI(Shallow Trench Isolation)두께 감소는 문턱이하 누설이 증가되는 패싱워드라인 효과를 유발한다. 인접한 패싱워드라인에 인가된 전압으로 인한 문턱이하누설 전류의 증가는 데이터 보존시간에 영향을 주며, 리프레시의 동작 횟수가 증가되어 DRAM의 소비 전력을 증가시키는 요인이 된다. 본 논문에서는 TCAD Simulation을 통해 패싱워드라인 효과에 대한 원인을 확인한다. 결과적으로, 패싱워드라인 효과가 발생하는 DRAM 동작상황을 확인하고, 이때 패싱워드라인 효과로 인해 전체 누설전류의 원인에 따른 비중이 달라지는 것을 확인하였다. 이를 통해, GIDL(Gate Induced Drain Leakage)에 의한 누설전류뿐만 아니라 문턱이하 누설전류를 고려의 필요성을 확인하며 이에 따른 DRAM 구조의 개선 방향의 지침이 될 수 있다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제2권1호
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• pp.24-33
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• 2010

Design of a Pump Jet Propulsor (PJP) was undertaken for an underwater body with axisymmetric configuration using axial/low compressor design techniques supported by Computational Fluid Dynamics (CFD) analysis for performance prediction. Experimental evaluation of the PJP was earned out through experiments in a Wind Tunnel Facility (WTF) using momentum defect principle for propulsive performance prior to proceeding with extensive experimental evaluation in towing tank and cavitation tunnel. Experiments were particularly conducted with respect to Self Propulsion Point (SPP), residual torque and thrust characteristics over a range of vehicle advance ratio in order to ascertain whether sufficient thrust is developed at the design condition with least possible imbalance torque left out due to residual swirl in the slip stream. Pumpjet and body models were developed for the propulsion tests using Aluminum alloy forged material. Tests were conducted from 0 m/s to 30 m/s at four rotational speeds of the PJP. SPP was determined confirming the thrust development capability of PJP. Estimation of residual torque was carried out at SPP corresponding to speeds of 15, 20 and 25 m/s to examine the effectiveness of the stator. Estimation of thrust and residual torque was also carried out at wind speeds 0 and 6 m/s for PJP RPMs corresponding to self propulsion tests to study the propulsion characteristics during the launch of the vehicle m water where advance ratios are close to Zero. These results are essential to assess the thrust performance at very low advance ratios to accelerate the body and to control the body during initial stages. This technique has turned out to be very useful and economical method for quick assessment of overall performance of the propulsor and generation of exhaustive fluid dynamic data to validate CFD techniques employed.

• 대한기계학회논문집 C: 기술과 교육
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• 제3권2호
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• pp.141-148
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• 2015

본 연구에서는 진공 차단기(Vacuum circuit breaker)의 동적 특성을 모사하기 위해 리커다인을 이용한 다물체 동역학 해석 모델이 개발 되었다. 진공 차단기는 VI(Vacuum interrupter)를 포함한 3 개의 주회로 부와, 구동 메커니즘을 포함한 기구부로 구성된다. 이 해석적 모델의 검증을 위해, 해석 결과와 실측을 통한 실험적 결과를 비교 하였다. 일반적으로, 원활한 사고 전류 차단을 위해서는 0.9~1.1m/s 의 차단속도(Opening velocity)가 필요하다. 차단 속도의 향상을 위해, 다구찌 기법을 이용하여 진공 차단기의 설계 변수 최적화를 수행하였다. 또한 향상된 차단기의 동적 특성을 검증하기 위해, 해석 결과와 개선된 샘플의 실험적 결과를 비교 분석 하였다.

• International Journal of Aeronautical and Space Sciences
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• 제15권4호
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• pp.345-355
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• 2014

This paper focuses on aerodynamic and inertial modeling of the propeller for its applications in flight dynamics analyses of a propeller-driven airplane. Unsteady aerodynamic and inertial loads generated by the propeller are formulated using the blade element method, where the local velocity and acceleration vectors for each blade element are obtained from exact kinematic relations for general maneuvering conditions. Vortex theory is applied to obtain the flow velocities induced by the propeller wake, which are used in the computation of the aerodynamic forces and moments generated by the propeller and other aerodynamic surfaces. The vortex lattice method is adopted to obtain the induced velocity over the wing and empennage components and the related influence coefficients are computed, taking into account the propeller induced velocities by tracing the wake trajectory trailing from each of the propeller blades. Aerodynamic forces and moments of the fuselage and other aerodynamic surfaces are computed by using the wind tunnel database and applying strip theory to incorporate viscous flow effects. The propeller models proposed in this paper are applied to predict isolated propeller performances under steady flight conditions. Trimmed level forward and turn flights are analyzed to investigate the effects of the propeller on the flight characteristics of a propeller-driven light-sports airplane. Flight test results for a series of maneuvering flights using a scaled model are employed to run the flight dynamic analysis program for the proposed propeller models. The simulations are compared with the flight test results to validate the usefulness of the approach. The resultant good correlations between the two data sets shows the propeller models proposed in this paper can predict flight characteristics with good accuracy.

• Smart Structures and Systems
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• 제19권2호
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• pp.115-126
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• 2017

In this paper, size dependent bending and free flexural vibration behaviors of functionally graded (FG) nanobeams are investigated using a nonlocal quasi-3D theory in which both shear deformation and thickness stretching effects are introduced. The nonlocal elastic behavior is described by the differential constitutive model of Eringen, which enables the present model to become effective in the analysis and design of nanostructures. The present theory incorporates the length scale parameter (nonlocal parameter) which can capture the small scale effect, and furthermore accounts for both shear deformation and thickness stretching effects by virtue of a hyperbolic variation of all displacements through the thickness without using shear correction factor. The material properties of FG nanobeams are assumed to vary through the thickness according to a power law. The neutral surface position for such FG nanobeams is determined and the present theory based on exact neutral surface position is employed here. The governing equations are derived using the principal of minimum total potential energy. The effects of nonlocal parameter, aspect ratio and various material compositions on the static and dynamic responses of the FG nanobeam are discussed in detail. A detailed numerical study is carried out to examine the effect of material gradient index, the nonlocal parameter, the beam aspect ratio on the global response of the FG nanobeam. These findings are important in mechanical design considerations of devices that use carbon nanotubes.

• 한국운동역학회지
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• 제12권1호
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• pp.205-219
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• 2002

This research seeks to identify the plantar pressure distribution graph and change in force in connection with effective golf drive strokes and thus to help ordinary golfers have appropriate understanding on the moving of the center of weight and learn desirable drive swing movements. To this end, we conducted surveys on five excellent golfers to analyze the plantar pressure applied when performing golf drive strokes, and suggested dynamic variables quantitatively. 1) Our research presents the desire movements as follows. For the time change in connection with the whole movement, as a golfer raises the club head horizontally low above ground from the address to the top swing, he makes a semicircle using the left elbow joint and shaft and slowly turns his body, thus lengthening the time. And, as the golfer twists the right waist from the middle swing to the impact with the head taking address movement, and does a quick movement, thus shortening the time. 2) For the change in pressure distribution by phase, to strike a strong shot with his weight imposed from the middle swing to the impact, a golfer uses centrifugal force, fixes his left foot, and makes impact. This showed greater pressure distribution on the left sole than on the right sole. 3) For the force distribution graph by phase, the force in the sole from the address to halfway swing movements is distributed to the left foot with 46% and to the right foot with 54%. And, with the starting of down swing, as the weight shifts to the left foot, the force is distributed to the left sole with 58%. Thus, during the impact and follow through movements, it is desirable for a golfer to allow his left foot to take the weight with the right foot balancing the body. 4) The maximum pressure distribution and average of the maximum force in connection with the whole movement changed as the left (foot) and right (foot) supported opposing force, and the maximum pressure distribution also showed much greater on the left sole.

• 동력기계공학회지
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• 제15권1호
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• pp.24-31
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• 2011

Rectangular box type structures are used in many fields of civil, mechanical and marine engineering. Especially, Most ship structures are often in contact with inner or outer fluid, like ballast, fuel and stem tanks. Fatigue damages are sometimes observed in these tanks which seem to be caused by resonance with exciting force of engine and propeller. Vibration characteristics of these thin walled tanks in contact with fluid near engine and propeller are strongly affected by added mass of containing fluid. Therefore it is essentially important to estimate the added mass effect to predict vibration of the tanks. Many authors have studied vibration of rectangular tanks containing fluid. Few research on dynamic interaction among tank walls filled with fluid are reported in the vibration of rectangular tanks recently. In case of rectangular tanks, structural coupling between adjacent panels and effect of vibration modes of multiple panels on added mass of water have to be considered. In the previous report, a numerical analysis is performed for the coupling effect between panels of a tank on added mass of containing fluid, the effect of structural constraint between panels on each vibration mode for fluid region, and mode characteristics in accordance with changing breadth of the plates by using finite element method for plates and boundary element method for fluid region. In this paper, the coupling effect between panels of a tank on added mass of containing fluid, the effect of structural constraint between panels on each vibration mode for fluid region, and mode characteristics in accordance with changing length, thickness, and boundary condition of the plates are investigated numerically and discussed.

• 한국도로학회논문집
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• 제13권2호
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• pp.1-8
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• 2011

본 연구의 목적은 중온화 첨가제(LEADCAP$^{(R)}$)를 사용한 중온 아스팔트 바인더의 노화 방법에 따른 물성 변화 특성을 평가하고자 하였다. 아스팔트 바인더의 노화 거동을 모사하기 위해 단기노화인 RFTO를 실시하였으며, 햇빛에 의한 자연 노화 거동을 알아보기 위해 자외선 경화기를 이용하여 자외선에 의한 열화거동을 모사하였다. 이러한 열화 중온 아스팔트 바인더의 역학적인 물성과 유변동학적인 특성을 시험하기 위해서 만능시험기(UTM)과 동적전단유동기를 이용하여 직접인장력과 유변동학적인 거동을 평가하였다. 또한, 열분석 장비를 이용하여 온도에 따른 중온 아스팔트 바인더의 특성을 평가하여, 자외선 노출에 따른 열화가 발생하여도 온도에 따른 물성 변화가 많이 발생하지 않음을 발견하였다. $70^{\circ}C$에서 중온화 첨가제가 첨가한 단기노화 중온 아스팔트 바인더의 경우, PG 등급에서의 고온 등급의 기준값을 만족함을 알 수 있었다. 또한 저온에서 중온 아스팔트 바인더의 인장 특성을 평가한 결과, 인장강도 향상과 함께 인장력이 증가됨을 알 수 있었다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2005년도 춘계학술대회 논문집
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• pp.965-968
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• 2005

Roll drafting operation causes variations in the linear density of bundles because the bundle flow cannot be controlled completely by roll pairs. Defects occurring in this operation bring about many problems successively in the next processes. In this paper, we attempt to analyze the draft dynamics and the linear density irregularity based on the governing equation of a bundle motion that has been suggested in our previous studies. For analyzing the dynamic characteristics of the roll drafting operation, it is indispensable to investigate a transient state in time domain before the bundle flux reaches a steady state. However, since governing equations of bundle flow consisting of continuity and motion equations turn out to be nonlinear, and coupled between variables, the solutions for a transient state cannot be obtained by an analytical method. Therefore, we use the Finite Difference Method(FDM), particularly, the FTBS(Forward-Time Backward-Space) difference method. Then, the total equations system yields to an algebraic equations system and is solved under given initial and boundary conditions in an iterative fashion. From the simulation results, we confirm that state variables show different behavior in the transient state; e.g., the velocity distribution in the flow field changes more quickly the linear density distribution. During a transient flow in a drafting zone, the output irregularity is influenced differently by the disturbances, e.g., the variation in input bundle thickness, the drafting speed, and the draft ratio.