• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2006년도 Proceedings of ISRS 2006 PORSEC Volume I
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• pp.21-24
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• 2006

Processes controlling the interannual variation of mixed layer temperature (MLT) averaged over the NINO3 domain ($150-90^{\circ}W$, $5^{\circ}N-5^{\circ}S$) are studied using an ocean data assimilation product that covers the period of 1993 to 2003. Advective tendencies are estimated here as the temperature fluxes through the domain's boundaries, with the boundary temperature referenced to the domain-averaged temperature to remove the dependence on temperature scale. The overall balance is such that surface heat flux opposes the MLT change but horizontal advection and subsurface processes assist the change. The zonal advective tendency is caused primarily by large-scale advection of warm-pool water through the western boundary of the domain. The meridional advective tendency is contributed mostly by Ekman current advecting large-scale temperature anomalies though the southern boundary of the domain. Unlike many previous studies, we explicitly evaluate the subsurface processes that consist of vertical mixing and entrainment. In particular, a rigorous method to estimate entrainment allows an exact budget closure. The vertical mixing across the mixed layer (ML) base has a contribution in phase with the MLT change. The entrainment tendency due to temporal change in ML depth is negligible comparing to other subsurface processes. The entrainment tendency by vertical advection across the ML base is dominated by large-scale changes in wind-driven upwelling and temperature of upwelling water. Tropical instability waves (TIWs) result in smaller-scale vertical advection that warms the domain during La Ni? cooling events. When the advective tendencies are evaluated by spatially averaging the conventional local advective tendencies of temperature, the apparent effects of currents with spatial scales smaller than the domain (such as TIWs) become very important as they redistribute heat within the NINO3 domain. However, such internal redistribution of heat does not represent external processes that control the domain-averaged MLT.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2010년 춘계학술대회논문집
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• pp.530-533
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• 2010

This paper presents numerical analysis and design optimization of various turbine blade cooling techniques with three-dimensional Reynolds-averaged Navier-Stokes(RANS) analysis. The fluid flow and heat transfer have been performed using ANSYS-CFX 11.0. A fan-shaped hole for film-cooling has been carried out to improve film-cooling effectiveness with the radial basis neural network method. The injection angle of hole, lateral expansion angle of hole and ratio of length-to-diameter of the hole are chosen as design variables and spatially averaged film-cooling effectiveness is considered as an objective function which is to be maximized. The impingement jet cooling has been performed to investigate heat transfer characteristic with geometry variables. Distance between jet nozzle exit and impingement plate, inclination of nozzle and aspect ratio of nozzle hole are considered as geometry variables. The area averaged Nusselt number is evaluated each geometry variables. A rotating rectangular channel with staggered array pin-fins has been investigated to increase heat transfer performance ad to decrease friction loss using KRG modeling. Two non-dimensional variables, the ratio of the eight diameter of the pin-fins and ratio of the spacing between the pin-fins to diameter of the pin-fins selected as design variables. A rotating rectangular channel with staggered dimples on opposite walls are formulated numerically to enhance heat transfer performance. The ratio of the dimple depth and dimple diameter are selected as geometry variables.

• 전력전자학회논문지
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• 제16권3호
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• pp.250-257
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• 2011

본 논문은 병렬 삼상 부스트 컨버터에서 Interleaved PWM에 의해 발생하는 고 주파수 순환전류를 효과적으로 저감시키기 위해서, AC 입력단에 연결되는 삼상 결합 인덕터의 특성을 분석하였다. 제시된 삼상 결합 인덕터 분석은 삼상 결합 인덕터의 구조와 전압 방정식의 해석을 통하여 이루어졌다. 그리고 이것을 바탕으로 기존의 저 주파수 평균화 모델에 삼상 결합 인덕터를 추가하여, 고 주파수 순환전류와 저 주파수 순환전류를 동시에 저감시킬 수 있는 새로운 형태의 평균화 모델을 제안하였다. 새로운 평균화 모델의 영상성분을 이용하면, 삼상 결합 인덕터와 라인 인덕터의 순환전류에 대한 총 인덕턴스를 각각 구해 비교 할 수 있다. 시뮬레이션과 실험결과를 토대로 병렬 삼상 부스트 컨버터에서 사용되는 삼상 결합 인덕터의 유용성을 검증하였다.

• 융합신호처리학회논문지
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• 제15권1호
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• pp.9-14
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• 2014

이동 통신망의 기지국과 이동국 사이의 거리 차로 인하여 발생하는 경로 손실 데이터를 분석하였다. 본 논문에서는, 측정된 수신 신호세기(RSSI)로부터 송수신기 거리 차이에 따른 경로 손실을 계산하여 이를 그래프로 표시하고, 평균한 데이터를 이용하여 기존의 경로 손실 모델들(자유공간 모델, 지면반사파 모델, 하타 모델, ${\ldots}$)과 그래프를 동시에 그려서 비교하였다. 2 Km, 1 Km, 0.5 Km 간격으로 평균한 경로 손실 데이터에 대한 표준 편차를 구해 보니, 각각 2.29 dB, 3.39 dB, 4.75 dB가 되었다. 본 논문에서는 거리별로 계산된 경로 손실 평균값들의 미분 값을 구하여, 앞에서 구한 경로 손실 표준 편차의 1 또는 2배수를 초과하여 변동하는 위치를 찾아내는 방법을 제안 하였다. 이렇게 제안한 방법을 적용하여 분석한 결과, 송수신기 사이에서 손실이 급격하게 발생하는 지점이, 2 Km 간격으로 경로 손실을 평균한 경우에는 5 지점, 1 Km 간격으로 평균한 경우에는 7 지점, 0.5 Km 간격으로 평균한 경우에는 19 지점이 됨을 알 수 있었고, 구체적인 위치를 파악하는 성과를 얻었다.

• 한국가시화정보학회:학술대회논문집
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• 한국가시화정보학회 2002년도 추계학술대회 논문집
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• pp.23-26
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• 2002

The phase-averaged velocity fields of 3 dimensional turbulent wake behind a marine propeller measured by 2D PIV and stereoscopic PIV(SPIV) were compared directly. In-plane velocity fields obtained from the consecutive particle images captured by one camera in 2D PIV have perspective errors due to out-of-plane motion. However, the perspective errors can be removed by measuring three component velocity fields using SPIV method with two cameras. It is also necessary to measure three components velocity fields for the investigation of complicated near-wake behind the propeller for the suitable propeller design. 400 instantaneous velocity fields were measured for each of four different blade phases of $0^{\circ},\;18^{\circ},\;36^{\circ}C\;and\;54^{\circ}$. They were ensemble averaged to investigate the spatial evolution of the propeller wake in the downstream region. The phase-averaged velocity fields show the viscous wake developed along the blade surfaces and tip vortices were formed periodically. The perspective errors caused by the out-of-plane motion was estimated by the comparison of 2D PIV and SPIV results. The difference in the axial mean velocity fields measured by both techniques are nearly proportional to the mean out-of-plane velocity component which has large values in the regions of the tip and trailing vortices. The axial turbulence intensity measured by 2D PIV was overestimated since the out-of-plane velocity fluctuations influence the in-plane velocity vectors and increase the in-plane turbulence intensities.

• 한국항행학회논문지
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• 제25권1호
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• pp.84-89
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• 2021

표준 단일 모드 광섬유가 가지는 색 분산과 비선형 현상에 의한 광 신호 왜곡을 보상할 수 있는 분산 제어와 광 위상 공액이 결합된 링크의 한계인 대칭적 구조를 해결할 수 있는 방법을 제안하였다. 대칭적 구조는 전반 전송 구간과 후반 전송 구간의 중계 구간수, 분산 분포 등등이 광 위상 공액기를 중심으로 대칭되어야 한다는 것을 의미한다. 본 연구에서 제안하는 분산 제어 링크는 광 위상 공액기가 전반의 6개 중계 구간과 후반의 14개 사이에 존재하고, 각 전송 반 구간에서의 평균 중계 구간 당 잉여 분산 (RDPS; residual dispersion per span)이 서로 동일한 구조이다. 제안된 분산 제어 링크에서의 광 신호 왜곡 보상 효과의 분석은 평균 RDPS가 각 전송 반 구간에서 서로 다르게 설정된 링크에서의 결과와의 비교를 통해 이루어졌다. 시뮬레이션 결과 전송 반 구간 사이의 RDPS 평균값의 동일 여부보다 인접한 중계 구간 간 RDPS 편차가 보상에 더 큰 영향을 미치는 것은 확인하였다.

• 한국원자력학회:학술대회논문집
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• 한국원자력학회 1997년도 추계학술발표회논문집(1)
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• pp.19-24
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• 1997

In this study, we extend the application of the interface-matrix(IM) method for reflector modeling to Analytic Flux Expansion Nodal (AFEN) method. This include the modifications of the surface-averaged net current continuity and the net leakage balance conditions for IM method in accordance with AFEN fomular. AFEN-interface matrix (AFEN-IM) method has been tested against ZION-1 benchmark problem. The numerical result AFEN-IM method shows 1.24% of maximum error and 0.42% of root-mean square error in assembly power distribution, and 0.006%Δk of neutron multiplication factor. This result proves that the interface-matrix method for reflector modeling can be useful in AFEN method.

• 대한기계학회논문집B
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• 제24권10호
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• pp.1335-1342
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• 2000

Three-dimensional flow analysis and numerical optimization methods are presented for the design of an axial-flow fan. Steady, incompressible, three-dimensional Reynolds-averaged Navier-Stokes equations are used as governing equations, and standard k- ${\varepsilon}$ turbulence model is chosen as a turbulence model. Governing equations are discretized using finite volume method. Steepest descent method, conjugate gradient method and BFGS method are compared to determine the searching directions. Golden section method and quadratic fit-sectioning method are tested for one dimensional search. Objective function is defined as a ratio of generation rate of the turbulent kinetic energy to pressure head. Two variables concerning sweep angle distribution are selected as the design variables. Performance of the final fan designed by the optimization was tested experimentally.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집B
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• pp.704-708
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• 2000

A new efficient numerical method for computing unsteady, incompressible flows, DRANS (Decoupled Reynolds-Averaged Navier-Stokes), is presented. To eliminate the restriction of CFL condition, a fully-implicit time advancement in which the Crank-Nicolson method is used fer both the diffusion and convection terms. is adopted. Based on decomposition method, the velocity-turbulent quantity decoupling is achieved. The additional decoupling of the intermediate velocity components in the convection term is made for the fully-implicit time advancement scheme. Since the iterative procedures for the momentum, ${\kappa}\;and\;{\varepsilon}$ equations are not required, the components decouplings bring fourth the reduction of computational cost. The second-order accuracy in time of the present numerical algorithm is ascertained by computing decaying vortices. The present decoupling method is applied to turbulent boundary layer with local forcing.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집B
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• pp.51-56
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• 2000

The Finite Element Solutions Is reported on solid-liquid phase change in porous media with natural convection including freezing. The model is based on volume averaged transport equations, while phase change is assumed to occur over a small temperature range. The FEM (Finite Element Method) algorithm used in this study is 3-step time-splitting method which requires much less execution time and computer storage the velocity-pressure integrated method and the penalty method. And the explicit Lax-Wendroff scheme is applied to nonlinear convective term in the energy equation. For natural convection including melting and solidification the numerical results show reasonable agreement with FDM (Finite Difference Method) results.