• Water for future
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• v.52 no.2
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• pp.43-51
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• 2019

• Journal of Korea Water Resources Association
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• v.37 no.10
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• pp.789-798
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• 2004

Conjunctive use of surface and ground water is emerging as an alternative to resolve water shortage problems caused by drought or overpopulation. The region whose water supply depends on a single source has high risk of emergency situations, and may need to consider conjunctive use to overcome its weakness. Conjunctive use also can be a realistic and effective solution when additional or new water resources are to be developed. This paper presents a new methodology for managing surface and ground water resources with the aim of supplying water in a sustainable way. The developed method encompasses procedures to assess site suitability for conjunctive use, to devise water supply scenarios based on drought analysis, and to quantify the amount of water attained. It is believed that the systematic and objective features of the developed method enable it to be a useful supportive tool for water management planning and decision-making.

• Proceedings of the Korea Water Resources Association Conference
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• 2010.05a
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• pp.689-693
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• 2010

본 연구는 최근 기상이변에 따른 집중호우에 의해 도시지역에서 빈번히 발생하고 있는 침수피해를 XP-SWMM모형을 이용하여 침수해석을 수행한 것으로서, 이를 위해 대상유역의 강우분석을 선수행하고 하천 외수위 상승에 따른 배수구역의 10년, 20년, 30년, 50년 설계빈도별 침수해석을 실시하였다. 이에 본 연구에서는 과거 하천 외수위 변화에 따른 내수배제 불량으로 인한 침수피해가 일어난 지역을 산정하고, 도시유역의 강우-유출해석과 하수관거 해석을 실시한다. 이를위해 XP-SWMM 모형을 이용하여 하수관망 시스템과 하천 외수를 연계 해석하여 장래 하천의 빈도별 홍수량에 대한 침수가능 여부를 분석하였다. 본 연구의 대상유역 면적은 62.35ha, 총 관로연장 12,741m, 소유역 60개, 하수관로 175개로 모형을 구성 하였고, 유출해석결과 설계빈도 50년의 임계지속시간은 90분, 총 침수량은 $15,362m^3$, 침수면적은 $65,384m^2$였으며, 최대 침수심은 0.81m인것으로 산정되었다. 침수피해 경감효과로는 245세대, 585명의 피해경감 효과가 있을 것으로 분석 되었다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.42 no.11
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• pp.958-967
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• 2014

A hybrid method based on high-frequency asymptotic optics was developed in order to predict the RCS of flying vehicles for RCS reduction studies. In cavity return, the rays are assumed to bounce from the inlet cavity based on the laws of geometrical optics and to exit the cavity via the aperture. In other parts of a flying vehicle, the physical optics method is applied to compute the back-scattered field from the solid surface. The hybrid method was validated by considering simple models of sphere and sphere with cavity. In addition, RCS analysis of a flying vehicle was conducted using the new hybrid electromagnetic scattering method based on physical optics and geometrical optics theories.

• Journal of Korean Tunnelling and Underground Space Association
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• v.8 no.4
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• pp.355-363
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• 2006

In this study, it was analyzed how the pore pressure behind a subsea tunnel influences on the stability of the tunnel. The tunnel is located in the soft rock layer, and a soft sandy layer and weathered soil layer are located on the top of it. Coupled numerical analyses are performed for both drained and undrained condition with varying coefficients of lateral earth pressure. In the case of undrained conditions, the stability of the tunnel was analyzed with different thicknesses of shotcrete. On the other hand, a sensitivity analysis was performed with different hydraulic conductivities and porosities of the shotcrete for the drained conditions. The stability of a subsea tunnel was evaluated in terms of safety factor suggested by You et al.(2000, 2001, 2005) based on the shear strength reduction technique. In this paper, the safety factor of a tunnel was calculated under steady state flow condition during hydro-mechanical coupled analysis. As a result, it was found that the stability of a subsea tunnel could be rather increased by allowing a proper amount of groundwater inflow into a subsea tunnel.

• Proceedings of the KIPE Conference
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• 2007.11a
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• pp.18-20
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• 2007

3상 계통 연계 형 인버터 시스템은 낮은 THD를 가지는 계통 전류를 공급해주기 위해 LCL 필터를 사용한다. LCL 필터를 사용하는 가장 큰 장점은 낮은 스위칭 주파수에서도 만족할 만한 수준의 THD를 가지는 계통 전류를 생성시킬 수 있다는 점이다. 반면에, 단점은 LCL필터를 포함하는 계통 연계 형 인버터 시스템의 전달함수에 하나의 공진 극점이 존재한다는 점이다. 이것은 계통 전류 제어 loop에서, 안정성 문제에 영향을 미친다. 정확한 제어를 위해서 시스템의 전달함수는 필수적이다. 여기서 중요한 점은 많은 저자들이 시뮬레이션과 실험을 할 때, 중성점이 없는 회로에서 행하지만 회로 해석을 할 때에는 중성점이 있는 회로에서 해석을 한다는 점이다. 그래서 우리는 등가 델타회로에서 LCL 필터를 포함한 전체 시스템의 수학적인 모델을 제안한다. 이 모델은 모든 인덕터와 커패시터의 기생 저항을 고려한다. 또한 이 논문은 계통 전류를 제어하기 위한 제어기의 해석적인 설계 절차를 포함한다. 제안한 수학적인 모델을 입증하기 위해, PSIM을 통한 시뮬레이션과 Simulink를 통한 시뮬레이션 결과를 비교하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.11
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• pp.7-14
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• 2005

A subdomain-interface finite element method is suggested to solve a class of fully- coupled thermomechanical problems with contact boundaries. The penalty method is used for connecting subdomains that satisfy interface compatibility conditions. As a result, effective stiffness matrices are always positive definite, and computational efficiency can be improved to a considerable degree. Moreover, any complex-shaped domain can be divided into independently modeled subdomains without considering the conformity of meshes on interfaces. Using a computer code based on the present method, these advantageous features are shown through a set of numerical studies.

• 한국전산유체공학회:학술대회논문집
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• 2011.05a
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• pp.343-349
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• 2011

A loosely coupling method is adopted to combine a computational fluid dynamics (CFD) solver and the comprehensive structural dynamics (CSD) code, CAMRAD II, in a systematic manner to correlate the airloads, vortex trajectories, blade motions, and structural loads of the HART I rotor in descending flight condition. A three-dimensional compressible Navier-Stokes solver, KFLOW, using chimera overlapped grids has been used to simulate unsteady flow phenomena over helicopter rotor blades. The number of grids used in the CFD computation is about 24 million for the isolated rotor and about 37.6 million for the rotor-fuselage configuration while keeping the background grid spacing identical as 10% blade chord length. The prediction of blade airloads is compared with the experimental data. The current method predicts reasonably well the BVI phenomena of blade airloads. The vortices generated from the fuselage have an influence on airloads in the 1st and 4th quadrants of rotor disk. It appeared that presence of the pylon cylinder resulted in complex turbulent flow field behind the hub center.

• The Journal of Engineering Geology
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• v.21 no.2
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• pp.179-186
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• 2011

Problems that arise from the use of groundwater can be minimized by connecting surface water with groundwater. We investigated the groundwater level at Osibcheon, Yeongdeok-gun, Gyeongsangbuk Province, and performed borehole investigation. We then used the SWAI-MODFLOW model to analyze variations in groundwater level and discharge amount. We also discuss how to assess the potential of groundwater dams in Korean by analyzing the hydrogeological properties of the candidate site.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.3
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• pp.31-36
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• 2006

In this study, nonlinear static aeroelastic analysis system for a high-aspect-ratio wing are developed using the transonic small disturbance (TSD) and large deflection beam theory and validated. For the coupling between fluid and structure, the transformation of displacement from the structural mesh to aerodynamic one is performed by the shape function of the beam finite element and the inverse transformation of force by work equivalent load concept. Also, for the static aeroelastic analysis of the wing the use of TSD aerodynamics are justified. The validation of the system includes one of the efficient transformation methods of force and displacement.