• 한국전산유체공학회지
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• 제14권1호
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• pp.35-44
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• 2009

To adequately analyze flows in pipe or duct network system, traditional node-based junction coupling methods require the junction loss which is specified by empirical or analytic correlations. In this paper, a new finite volume junction coupling method using a ghost junction cell is developed by considering the interchange of linear momentum as well as the important wall-effect at junction without requiring any correlation on the junction loss. Also, boundary treatment is modified to preserve the stagnation enthalpy across boundaries, such as pipe-end and the interface between junction and branch. Also, the computational accuracy and efficiency of the Godunov-type finite volume schemes are investigated by tracing the total mechanical energy of rapid transients due to sudden closure of valve at downstream end.

• 한국전자파학회논문지
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• 제18권5호
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• pp.486-495
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• 2007

일반적인 여파기는 대역폭과 원하지 않는 신호들의 억압이 더 중요한 반면, 국부 발진기 여파기의 경우, 차단 주파수에서의 억압이 중요한 척도가 되며, 이 때 대역폭은 통과 대역 주파수에서 삽입 손실을 최소화하도록 설계한다. 본 논문에서는 이러한 특수성을 고려한 대역 여파기의 설계 절차를 보였다. 또한, 대역 여파기 제작 시 알 수 없는 기생 성분으로 인해 원하지 않는 결과를 야기시켜 제작 후의 조정이 이루어지게 된다. 따라서 이러한 문제점을 고려하여 Momentum에 근거한 제작 이전의 설계적인 조정 절차를 제시하였다.

• 한국전자통신학회논문지
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• 제15권4호
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• pp.659-664
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• 2020

본 논문에서는 실리콘 기반의 광 집적회로에서 외부 전압 조절을 통해 |l|=1 궤도 각운동량 모드의 궤도 각양자수를 변조할 수 있는 전기 광학 변조기를 설계하였다. 설계된 전기 광학 변조기는 위치별로 서로 다른 도핑농도를 가지는 실리콘 코어와 실리콘 산화막으로 구성되어 있으며, 도핑농도의 분포를 통해 궤도 각운동량 모드를 구성하는 두 고유 모드의 전파 손실과 유효굴절률 변화량을 조절할 수 있도록 설계되었다. 변조기는 역전압을 기준으로 -0.33V에서는 궤도 각운동량 모드의 부호가 유지되는 광도파로로, 10V에서는 궤도 각양자수 부호 변환기로서 동작한다. 고유 모드 확장법으로 계산한 신호변조 후의 전기장 분포를 통해 얻은 궤도 각양자수는 두 동작모드에서 모두 |l|>0.92 으로 매우 높은 궤도 각운동량 모드 순도를 보였다.

• 디지털융복합연구
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• 제20권4호
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• pp.389-396
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• 2022

딥러닝(Deep Learning)은 퍼셉트론을 기반으로 하고 있으며 현재에는 이미지 인식, 음성 인식, 객체 검출 및 약물 개발 등과 같은 다양한 영역에서 사용되고 있다. 이에 따라 학습 알고리즘이 다양하게 제안되었고 신경망을 구성하는 뉴런수도 연구자마다 많은 차이를 보이고 있다. 본 연구는 현재 대표적으로 사용되고 있는 확률적 경사하강법(SGD), 모멘텀법(Momentum), AdaGrad, RMSProp 및 Adam법의 뉴런수에 따른 학습 특성을 분석하였다. 이를 위하여 1개의 입력층, 3개의 은닉층, 1개의 출력층으로 신경망을 구성하였고 활성화함수는 ReLU, 손실 함수는 교차 엔트로피 오차(CEE)를 적용하였고 실험 데이터셋은 MNIST를 사용하였다. 그 결과 뉴런수는 100~300개, 알고리즘은 Adam, 학습횟수(iteraction)는 200회가 딥러닝 학습에서 가장 효율적일 것으로 결론을 내렸다. 이러한 연구는 향후 새로운 학습 데이터가 주어졌을 경우 개발될 알고리즘과 뉴런수의 기준치에 함의를 제공할 것이다.

• 한국유체기계학회 논문집
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• 제11권5호
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• pp.15-21
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• 2008

In modem wind power system of large capacity above 1MW, horizontal axis wind turbine(HAWT) is a common type. And, the optimum design of wind turbine to guarantee excellent power performance and its reliability in structure and longevity is a key technology in wind Industry. In this study, mathematical expressions based upon the conventional BEMT(blade element momentum theory) applying to basic 1MW wind turbine blade configuration design. Power coefficient and related flow parameters, such as Prandtl's tip loss coefficient, tangential and axial flow induction factors of the wind turbine analyzed systematically. X-FOIL was used to acquire lift and drag coefficients of the 2-D airfoils and we use Viterna-Corrigan formula to interpolate the aerodynamic characteristics in post-stall region. In order to predict the performance characteristics of the blade, a performance analysis carried out by BEMT method. As a results, axial and tangential flow factors, angle of attack, power coefficient investigated in this study.

• 한국연소학회지
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• 제4권1호
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• pp.1-15
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• 1999

In order to analyze the sensitivity on the pulverized coal flames of the several variables, a numerical study was conducted at the gasification process. Eulerian approach is used for the gas phase, whereas lagrangian approach is used for the solid phase. Turbulence is modeled using the standard $k-{\varepsilon}$ model. The turbulent combustion incorporates eddy dissipation model. The radiation was solved using a Monte-Carlo method. One-step two-reaction model was employed for the devolatilization of Kideco coal. In pulverized flame of long liftoff height, the initial turbulent intensity seriously affects the position of flame front. The radiation heat transfer and wall heat loss ratio distort the temperature distributions along the reactor wall, but do not influence the reactor performance such as coal conversion, residence time and flame front position. The primary/secondary momentum ratio affects the position of flame front, but the coal burnout is only slightly influenced. The momentum ratio is a variable only associated with the flame stabilization such as flame front position. The addition of steam in the reactor has a detrimental effect on all the aspects, particularly reactor temperature and coal burnout.

• 천문학회보
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• 제37권1호
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• pp.39.1-39.1
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• 2012

Nuclear rings in barred galaxies are sites of active star formation (SF). We investigate SF and its feedback effects occurring in barred galaxies, for the first time, using high-resolution grid-based hydrodynamic simulations. The gaseous medium is assumed to be infinitesimally thin, isothermal, and unmagnetized. The SF recipes include a density threshold corresponding to the Jeans condition, a SF efficiency of 1%, and momentum feedback via Type II supernova events together with stellar-wind mass loss. To investigate various environments, we vary the gas sound speed as well as the efficiency of momentum injection in the in-plane direction. We find that when the sound speed is small, the surface density of a ring becomes largely independent of the azimuthal angle, resulting in star-forming regions distributed over the whole length of the ring. When the sound speed is large, on the other hand, the ring achieves the largest density at the contact points between the dust lanes and the ring where SF occurs preferentially, leading to a clear age gradient of star clusters in the azimuthal direction. Since rings shrink with time, a radial age gradient of star clusters naturally develop regardless of sound speed, consistent with observations. SF persists over 200 Myr, with an average rate of ${\sim}1.3M_{\odot}/yr$ similar to observed values. Rings gradually become hostile to SF as they lose gas into stars and turbulent motions dominate.

• 한국전산유체공학회지
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• 제22권1호
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• pp.67-80
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• 2017

The high-speed bypass effect on the heat exchanger performance has been investigated numerically. The plate-fin type heat exchanger was modeled using two-dimensional porous approximation for the fin region. Governing equations of mass, momentum, and energy equations for compressible turbulent flow were solved using ideal-gas assumption for the air flow. Various bypass-channel height were considered for Mach numbers ranging 0.25-0.65. Due to the existence of the fin in the bypass channel, the main flow tends to turn into the core region of the channel, which results in the distorted velocity profile downstream of the fin region. The boundary layer thickness, displacement thickness, and the momentum thickness showed the variation of mass flow through the fin region. The mass flow variation along the fin region was also shown for various bypass heights and Mach numbers. The volumetric entropy generation was used to assess the loss mechanism inside the bypass duct and the fin region. Finally, the correlations of the friction factor and the Colburn j-factor are summarized.

• 한국추진공학회지
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• 제7권2호
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• pp.15-22
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• 2003

본 연구에서는 2차원 압축성 Navier-Stokes 방정식을 사용하여 $30^{\cire}$ 경사진 터빈익의 냉각구를 통한 유출계수를 예측하였다. 내/외부 유동이 유출계수에 미치는 영향을 알아보기 위하여 외부유동만 존재하는 경우, 내부유동만 존재하는 경우 그리고 내/외부 유동이 없는 3가지 경우에 대하여 수치해석을 수행하였으며. 실험결과와 비교하였다. 본 연구의 수치해석결과는 유출계수를 잘 예측하였으며, 외부유동은 유출계수를 감소시키고, 내부유동은 냉각구내에서의 전압손실과 경계층의 영향을 감소시켜 특정 구간에서 유출계수를 증가시킨다는 것을 알았다.

• Advances in Energy Research
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• 제6권1호
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• pp.35-54
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• 2019

A successful blade design must satisfy some criterions which might be in conflict with maximizing annual energy yield for a specified wind speed distribution. These criterions include maximizing power output, more resistance to fatigue loads, reduction of tip deflection, avoid resonance and minimize weight and cost. These criterions can be satisfied by modifying the geometrical parameters of the blade. This study is dedicated to the aerodynamic assessment of a 20 kW horizontal axis wind turbine operating with two possible airfoils; that is $G{\ddot{o}}ttingen$ 413 and NACA 2415 airfoils (the Gottingen airfoil never been used in wind turbines). For this study parameters such as chord (constant, tapered and elliptic), twist angle (constant and linear) are varied and applied to the two airfoils independently in order to determine the most adequate blade configuration that produce the highest annual energy output. A home built numerical code based on the Blade Element Momentum (BEM) method with both Prandtl tip loss correction and Glauert correction, X-Foil and Weibull distribution is developed in Matlab and validated against available numerical and experimental data. The results of the assessment showed that the NACA 2415 airfoil section with elliptic chord and constant twist angle distributions produced the highest annual energy production.