• Proceedings of the Korea Water Resources Association Conference
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• 2015.05a
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• pp.40-40
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• 2015

최근 기후변화로 인해 홍수의 발생빈도와 홍수량이 증가하고 있으며, 여름철 집중호우 및 태풍에 의해 하천의 둔치가 침수됨으로써 다양한 침수피해를 야기한다. 대하천 사업 이후 하천의 둔치를 활용한 체육시설, 자전거도로 및 생태공원과 같은 친수시설들이 조성되었으며 태풍으로 인한 하천의 홍수위 상승은 이러한 친수시설에 대한 직접적인 피해를 가져올 수 있다. 따라서 이와 같은 침수피해를 예측하기 위해서는 둔치를 포함한 복단면에서의 흐름해석을 통한 수리학적 영향을 분석해야하며, 둔치에서의 흐름양상은 주수로에 비해 수심이 얕고 흐름에 대한 저항이 크기 때문에 2차원 수리해석이 바람직한 것으로 제안되고 있다. 2차원 수리해석에 있어 하천의 홍수위 상승과 하강으로 인해 발생하는 둔치구간에서의 마름과 젖음 현상은 수치해의 발산을 야기하며, 이러한 문제를 해결하기 위해 다양한 마름/젖음 해석 기법에 대한 연구들이 진행되어 왔으며 일반적으로 마름/젖음에 대한 문제를 해결하는 방법은 마름/젖음에 상관없이 모든 부분에서 방정식을 푸는 박막기법과 해석영역으로부터 마름 부분을 제거하는 이동경계법으로 나눌 수 있다. 본 연구에서는 단기간에 수위가 급변하는 태풍사상에 대한 둔치에서의 홍수위험도를 평가하기 위해 마름/젖음 해석이 가능한 2차원 유한차분모형인 Nays2D 모형을 이용하여 마름/젖음에 대한 과거 선행연구들의 결과와 적용된 모형의 결과를 비교하여 모형의 적용성을 검증하였고, 검증된 모형을 강정-고령보에서부터 달성보 사이 구간에 적용하여 수리학적 영향을 분석하였다. 또한, 모형의 결과를 이용하여 홍수위험지수를 산정하였으며, 이를 통해 둔치구간에서의 홍수위험도 평가를 실시하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.10
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• pp.1-6
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• 2006

This paper predicts the stall characteristics of three-dimensional wings. An iterative decambering approach is introduced into the nonplanar lifting surface method to take into consideration the stall characteristics of wings. An iterative decambering approach uses known airfoil lift curve and moment curve to predict the stall characteristics of wings. The multi-dimensional Newton iteration is used to take into consideration the coupling between the different sections of wings. Present results are compared with experiments and other numerical results. Computed results are in good agreement with other data. This scheme can be used for any wing with the twist or control surface and for wing-wing configurations such as wing-tail configuration or canard-wing configuration.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.11 no.2
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• pp.15-26
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• 1991

The lateral forces such as the earthquake and wind my cause the torsion to be coupled with the lateral bending in the gider, the cross-section of wich has only one axis of symmetry. This induces additional stresses especially in cables arranged in double-planes. Since this effect cannot be considered by using the conventional frame elements, the stiffness and the mass matrices of the geometrically nonlinear thin-walled frame element are developed in this study to model the girder. The equivalent modulus of elasticity proposed by Ernst is used for the cable elements. Verification of the present theory is made through a numerical example. Then, the free vibration of a three dimensional cable-stayed bridge is analyzed to study the coupled flexural-torsional behavior.

• Geophysics and Geophysical Exploration
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• v.20 no.1
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• pp.33-42
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• 2017

Recently, the grounded electrical-source airborne transient electromagnetic (GREATEM) system with high power source was introduced to achieve deeper investigation depth and to overcome high noise level. Although the GREATEM is a transient electromagnetic system using a long grounded wire as the transmitter, GREATEM data have been interpreted with 1D earth models because 2D or 3D modeling and inversion of vast airborne data are complicated and expensive to calculate. Generally, 1D inversion is subsequently applied to every survey point and combining 1D images together forms the stitched conductivity-depth image. However, the stitched models often result in abrupt variations in neighboring models. To overcome this problem, laterally constrained inversion (LCI) has been developed in inversion of ATEM data, which can yield layered sections with lateral smooth transitions. In this study, we analysed the GREATEM data through 1D numerical modeling for a curved grounded wire source. Furthermore, we developed a laterally constrained inversion scheme for continuous GREATEM data based on a layered earth model. All 1D data sets and models are inverted as one system, producing layered sections with lateral smooth transitions. Applying the developed LCI technique to the GREATEM data, it was confirmed that the laterally constrained inversion can provide laterally smooth model sections that reflect the layering of the survey area effectively.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.20 no.8
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• pp.797-805
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• 2009

In this paper, we developed MoM(Moment of Method) forward solver to implement the inverse scattering by using BIM(Born Iterative Method) for the detection of cancer in human body Especially, we adopted two-dimensional breast structure to analyze electromagnetic scattered phenomena. For the two-dimensional scattering structure, the integral equations is solved with MoM employing two-dimensional Green's function. Also, calculated results are compared with the measured results obtained from breast cancer detecting equipment.

• Journal of Energy Engineering
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• v.6 no.2
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• pp.137-144
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• 1997

Turbulent swirling cold-flow in a cyclonic gasifier has been analyzed by numerical analysis. Comparison of two dimensional and three dimensional analyses has shown that concept of equivalent slit is appropriate for the two dimensionalization of three dimensional phenomena. Flow characteristics have been scrutinized by varying swirl number which is a crucial parameter in determining the flow pattern of the cyclonic gasifier. Reactive flow field has been estimated by using theoretical swirl number and equivalent slit width for reactive flow. Results show that proper flow field for the reactive coal gasification can be formed by controlling the exit area and azimuthal location of coal burners.

• Journal of the Society of Naval Architects of Korea
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• v.39 no.3
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• pp.28-40
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• 2002

Turbulent flows around two-dimensional wing sections in ground effect are analysed by incompressible RANS equations and a finite difference method. The Baldwin-Lomax algebraic turbulence model is used to simulate high Reynolds number flows. The main purpose of this study is to clarify the two-dimensional ground effect and its flow characteristics due to different ground boundary conditions, i.e., moving and fixed bottom boundary. As a first step, to validate the present numerical code, the computational result of Clark-Y(t/C 11.7%) is compared with published numerical results and experimental data. Then, NACA4412 section in ground effect is calculated for various ground clearances with two bottom boundary conditions. According to the computational results, the difference in the lift and moment simulated with the two bottom boundary conditions is negligible, but the drag force simulated by the fixed bottom is to some extent smaller than that by the moving bottom. Therefore, it can be concluded that the drag force measured in a wind tunnel with the fixed bottom could be smaller than that with the moving bottom.

• Transactions of the Korean Society of Mechanical Engineers
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• v.15 no.6
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• pp.1831-1838
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• 1991

The deformation of coil spring with noncircular section, which is used in the engine valve of automobiles under the applied load is usually accompanied by sectional warping and additional displacements of geometric center. In this study the isoparametric beam element formulations are modified and expanded to consider these two effects. To verify these formulations, simple torsion tests are made and compared with the analysis results. For the case of the zero-pitch spring, the stress distributions of oval and circular section are coincided with those of the analysis using the solid elements. Cylindrical coil springs with oval section are analyzed. These results are agreed with those of Nagaya.

• Proceeding of EDISON Challenge
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• 2014.03a
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• pp.610-613
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• 2014

본 연구에서는 Dyson사의 Air multiplier의 Coanda surface각도에 따른 Air foil 주변의 2차원 유동을 분석하고 Surface각도가 유동에 미치는 영향에 대해 해석하였다. Air multiplier 단면의 작은 Slit을 통해 분류된 공기는 Venturi effect에 의해 가속되며 Coanda effect에 의해 단면을 따라 흐르며 압력차를 발생시켜 주변의 공기를 추가적으로 유입시킨다. EDISON CFD를 이용하여 Surface 각도에 따른 Air foil 주변의 유동을 구현하고 각도가 유동에 미치는 영향을 해석하였다. 또한 다른 논문에서 발췌한 실험값과 CFD 분석을 통해 얻은 값을 비교하여 CFD분석이 유효한지 확인하였다.

• Proceeding of EDISON Challenge
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• 2016.03a
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• pp.560-565
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• 2016

최근 대형 컨테이너선의 개발이 지속적으로 이루어짐에 따라 슬래밍에 의한 선수 및 선미의 구조안정성 문제가 대두되고 있지만 설계 단계에서 슬래밍에 대해 고려하기에는 현상의 복잡성으로 인해 어려움이 많았다. 이를 위해 KRISO에서 시행된 WILS JIP의 선수 단면 형상 및 선미 단면인 쐐기 형상으로 격자를 생성하여 EDISON CFD 다상유동 해석자를 통해 수치해석을 시도하였다. 기존 방식과 달리 계산 시간 절감을 위하여 격자 변형 기법을 적용하지 않고 모형 시험결과를 기반으로 한 유입류 조건을 설정하여 입수 충격 문제를 해석해보았다. 그 결과, 선미 형상의 경우 선행연구와 유사하게 실험 결과에 근접한 유체 충격력을 정량적으로 얻어낼 수 있었다. 선수 형상의 경우에서는 구상 선수로 인해 파생되는 센서 위치별 충격력의 변화를 확인할 수 있었으며, 실제 유동에 가까운 유동 형상과 슬래밍에 의한 충격력을 개략적으로 구할 수 있었다.