• Journal of the Korean Society of Fisheries and Ocean Technology
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• v.40 no.4
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• pp.360-366
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• 2004

This paper presents a method analyzing the motion of cylindrical buoy moored at 2 points and tensions action on each mooring line under the action of periodic waves. It was found that submersible buoy was more effective than floating one in the severe conditions considering its dynamic motions, wave forces, and mooring line tensions. The wave induced its dynamic responses and mooring line tensions peak when the ratio d/${\lambda}$ of the buoy length d to the waves length ${\lambda}$ was 0.66 due to its natural frequency. The results of this study were in agreement with the existing measurement ones, however, further verifications are needed considering resonance of cylindrical buoy and its displacements to wave height by a series of model tests.

• Proceedings of the Korea Water Resources Association Conference
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• 2007.05a
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• pp.1353-1357
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• 2007

국내에서 홍수 범람과 농지침수 분석에 이용되는 FLUMEN 모형은 원형섬 주변 처오름 현상과 급변류 해석만이 검증되어 소개되었다. 따라서 FLUMEN 모형의 만곡부나 합류부 등 개수로에서 적용가능성을 파악하기 위해서 하상경사 급변화, 원형 교각 주변 흐름변화, $180^{\circ}$ 만곡부 및 $90^{\circ}$ 합류부 실험 결과와 비교 검토를 수행하였다. FLUMEN 모형은 유한 체적법을 이용한 수치 계산으로 천이구간에서 발생하는 불연속점에서도 수치 모의가 잘 이루어지며, 만곡 수로와 합류 수로에서 전체적인 수심 분포가 최대 6%미만의 오차를 보이고 있어 매우 양호한 수치 모의를 할 수 있다. 또한 임의의 기하학적 형상을 원하는 위치에 반영한 지형 격자망 생성이 가능하다. 따라서 FLUMEN은 교각 주변, 만곡부 및 합류부 흐름 특성을 비교적 정확한 모의가 가능하며, 실제 하천에 적용하기에 충분한 수치 모의 능력을 지닌 모형이라 판단된다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2003.05a
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• pp.45-48
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• 2003

The plume interference is a complex phenomenon, consisting of plume-induced boundary layer separation, separated shear layer, multiple shock waves, and their interactions. The base knowledge of plume interference effect on powered missiles and flight vehicles is not yet adequate to get an overall insight of the flow physics in plume-freestream flow field. Computational studies are performed to better understand the flow physics of the plume-induced shock and separation for Simple, Rounded, Porous-extension test model configurations. The present study simulates highly underexpanded exhaust plume effect on missile body at the transoni $c^ersonic speeds. In order to investigate the plume-induced separation phenomenon, Simple, Rounded and Porous-extension plate are attacked to the missile afterbody. The computational result shows that the rounded afterbody and the porous-extension wall attached at the missile base can alleviate the plume-induced shock wave and separation phenomenon and improve the control of the missile body.dy.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.9
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• pp.879-888
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• 2009

Unsteady three-dimensional reacting flowfield generated by transverse hydrogen injection into a supersonic mainstream is numerically investigated using DES and finite-rate chemistry model. Comparisons are made with experimental results to investigate the turbulent reacting flow physics. The numerical OH distribution describes well the experimental OH-PLIF result, while the numerical ignition delay time shows some disparity due to the restricted available experimental data. The intermittency phenomena are identified by the comparative analysis between RANS and DES. Those effects are also quantified by the temperature distributions along streamlines and superimposed OH mass fraction along with time.

• Proceedings of the Korean Geotechical Society Conference
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• 2004.03b
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• pp.348-355
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• 2004

본 연구에서는 geosynthetics로 보강된 다짐토의 보강 메카니즘을 파악하기 위한 목적으로 실내시험 및 수치계산 수행하였다. 본 연구에서 고려하는 보강 메카니즘은 전단에 의한 다짐토의 체적 팽창(부의 다일렌탄시)을 geosynthetics에 의해 구속 억제하는 과정에서 생성되는 효과로 생각한다. 먼저, 실내실험을 위한 구제직인 방법으로서, geosynthetics의 보강효과를 정량직으로 파악하기 위하여 사질토를 다짐하여 공시체를 만들어 그 주위에 geosynthetics를 설치하여 전체적으로 압축전단 시험을 실시하였다. 또한, 다짐토의 다짐도를 달리 하고 한 가지 종류만의 geosynthetics를 이용하여, 다짐토와 geosynthetics의 상호작용에 따른 압축력 변화, geosynthetics의 인장력 변화 및 공시체의 파괴 진행상황 등을 살펴보았다. 수치계산에서는 다짐토의 다일렌탄시 특성에 대하여 표현 가능한 탄소성 구성모델을 이용하였다. 또한, 탄소성 구성 모델에서의 항복 이전의 탄성영역의 거동을 묘사하기 위하여 Hashiguchi(1989)가 제안한 subloading surface의 개념을 도입하였고, 유한요소(FEM)해석을 통해 얻어진 결과들을 실내시험의 결과와 비교 분석하였으며, 그 결과 양자 양호한 결과를 얻었다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.04a
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• pp.329-334
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• 2007

An axisymmetric supersonic jet screech in the Mach number range from 1.07 to 1.2 is numerically simulated. The axisymmetric mode is the dominant screech mode for an axisymmetric jet. The Reynolds-averaged Navier-Stokes equations in the conjunction with modified Spalart-Allmaras turbulence model are employed. A high resolution finite volume essentially non-oscillatory(ENO) schemes are used along with nonreflecting characteristic boundary conditions that are crucial to screech tone computations to accurately capture the sound waves, shock-cell structures, unsteady shock motions and large-scale instability waves.

• Journal of the Korean Society of Propulsion Engineers
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• v.5 no.3
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• pp.33-40
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• 2001

In order to investigate the operating characteristics of a supersonic steam ejector, the axisymmetric, compressible, Reynolds-averaged, Wavier-Stokes computations are performed using a finite volume method. The secondary and back pressures of the ejector system with a second throat are changed to investigate their effects on the suction mass flow. Three operation modes of the steam ejector system, the critical mode, subcritical mode and back flow mode, are discussed to predict the critical suction mass flow. The present computations are validated with some experimental results. The secondary and back pressures of the supersonic steam ejector significantly affect the critical suction mass flow. The present computations predict the experimented critical mass flow with fairly good accuracy A good correlation is obtained for the critical suction mass flow. The present results show that provided the primary nozzle configuration and secondary pressure are blown, we can predict the critical mass flow with good accuracy.

• Journal of Korean Society of Coastal and Ocean Engineers
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• v.6 no.1
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• pp.40-50
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• 1994

For an accurate prediction of the temperature field induced by heated water discharged into a shallow crossflow, a two-dimensional near-field numerical model is developed. It is based on a 4-equation turbulence model in which the transport equations for mean of the temperature fluctuation squared and its dissipation rate are added to those of a 2-equation turbulence model which cannot give the information of the thermal time scale ratio. Vertical diffusion is also considered by including buoyancy production and turbulence heat flux terms. The developed model is applied to a steady flow in an open channel with simple geometry and the results are compared with existing experimental data and those of the already established 2-equation turbulence model. Numerical results of the model agree with the experimental data better than those of the 2-equation model. The present model also simulates quite adequately the physical characteristics of thermal discharge in the jet entrainment and stable regions.

• Journal of the korean Society of Automotive Engineers
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• v.9 no.1
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• pp.23-32
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• 1987

기계,구조물의 신뢰성을 향상시키는 입장에서, 최근에 특히 진동문제가 크로즈업되고 있다. 이것 은 기계, 구조물이 고속화, 대형화, 대용량화함에 따라 종래의 기술만으로는 통용이 되지않기 때 문이라고 생각한다. 이러한 이유로 기계, 구조물의 동력학적 검토를 위해 수치해석기술과 실험해 석기술이 근년에 대단히 비약적으로 발전하고 있다. 이러한 해석기술의 진보를 뒷받침하는 것은 근년의 계산기 및 그 이용기술이다. 즉, 수치해석분야에서 Cray RAN을 시초로 하는 각종전자계 측기기, 고성능미니컴퓨터와 시계열통계해석기술 및 모우도 해석기술이다. 특히 모우드해석에 관 해서는 근년의 진보가 현저하고, 종래의 간단한 가진실험 데이터로부터의 모우도, 파라미터(고유 치, 고유감쇠비, 고유모우드)의 추출에 그치지 않고, 진동응답예측(simulation)과 유한요소법과의 결합이라고 하는 광범위한 기술내용의 포함하는 중요한 기술이 되고 있다. 여기에서는, 이 모우 드해석 특히 실험적 모우드해석기술을 기계구조물에 어떻게 응용할것인가에 대해서 설명한다.

• Journal of the Society of Naval Architects of Korea
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• v.34 no.2
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• pp.39-47
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• 1997

In the present paper, viscous flow fields around a wigley hull with appendages are analysed to study interactions between the hull and appendages. Navier-Stokes and continuity equations are solved by a finite volume method in a body-fitted coordinate system which conforms three dimensional ship geometries with appendages. A Sub-Grid Scale(SGS) turbulent model is used for a calculation of high Reynolds number flow. Numerical computations has been done for a Wigley hull form at $Rn=1.0{\times}10^6$. The results show that the present approach can predict, at least in qualitative sense, the influence of the appendages upon the flow field around a ship.