• 제목/요약/키워드: 표면해석

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Basic Analysis of Bubble Behavior in the Viscous Flow Domain with the Free Interface (자유표면을 가지는 점성 유동장내의 기포거동에 관한 기초해석)

  • I.R. Park;H.H. Chun
    • Journal of the Society of Naval Architects of Korea
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    • v.39 no.1
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    • pp.16-27
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    • 2002
  • A level-set method is used for analyzing the behaviors of gas bubbles in two fluids incompressible viscous flow domain. The governing equations are solved by using a finite volume method. The numerical results are verified by comparing with the experimental and other computational results. Computations for the deformations and motions of one or multi-bubbles in the flow domain with the initial undisturbed free interface are conducted. It can be seen that numerical results for different surface tension and density ratio arise very different behaviors of bubbles. When bubbles rise near the free interface, the free interface gives some great influence on the behaviors of bubbles. The present results computed by a level-set method give useful information about the properties of bubble motions and deformations.

Inversion of spectral analysis of surface waves with analytic Jacobian (해석적 자코비안을 이용한 표면파 기법의 역산)

  • Ha, Hee-Sang
    • Journal of the Korean Geophysical Society
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    • v.5 no.3
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    • pp.233-245
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    • 2002
  • The spectral-analysis-of-surface-waves (SASW) method is a nondestructive testing method based upon generation and detection of elastic stress waves. SASW is widely used as one of the techniques to determine stiffness profile in engineering geophysics. The essential steps involved are construction of an experimental dispersion curve from data collected in situ, and inversion of the dispersion curve to determine the stiffness profile. The main object of this study is to derive an analytical Jacobian for the inversion. If we set the subsurface to N homogeneous layer, it could save 2N times Jacobian calculation compared to numerical jacobian calculation during inversion. To reconstruct a stiffness profile, constrained damped least square method was applied for the inversion. The algorithm was tested for the numerical data and for the real asphalt and tunnel data, which were able to verify the stiffness profile. The stiffness profile reconstructed by the algorithm showed the possibility to appraise the soundness of tunnel with applications SASW.

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Behavior Analysis of PPWS Sockets for Suspension Bridges Considering Frictional Contact (마찰 접촉을 고려한 현수교 PPWS용 소켓의 거동 해석)

  • Yoo, Hoon;Lee, Sung-Hyung;Seo, Ju-Won
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.33 no.4
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    • pp.1281-1293
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    • 2013
  • A sophisticated finite element model is illustrated to analyze the behavior of Prefabricated Parallel Wire Strand(PPWS) sockets for main cables of suspension bridges. An orthotropic model is proposed for the casting material by considering both effects of individual wires and a casting alloy, and the contact between surfaces of a socket and a casting alloy is idealized by using the Coulomb friction and the surface-based contact model. The proposed FE model is verified by comparing the strain distributions obtained from the tensile test and FE analysis. The mechanical behavior of a socket is investigated with respect to the variation of the frictional coefficient. The result shows that the friction between surfaces significantly diminishes the stress concentration of a socket and a casting alloy, and the normal stress from the design equation represents the averaged value of the upper and lower quartiles in the distribution of contact stresses between a socket and a casting alloy.

Development of Software for Electrochemical Plating Simulation Including Diffusion Layer Effects (확산층을 고려한 정밀 도금 Simulator 개발)

  • Seo, Seok;Lee, Ju-Dong;Gwon, Si-Hyeon;Ryu, Dong-Hwan
    • Proceedings of the Korean Institute of Surface Engineering Conference
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    • 2012.11a
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    • pp.76-77
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    • 2012
  • 전기 도금 시스템에서 전산모사 해석을 이용하여 도금층 두께를 정확히 예측하기 위해서 음극 표면의 확산층이 고려된 도금 Simulator를 개발하였다. 특정 형상의 경우 도금액 교반이 원활하지 않아 불균일한 도금이 이루어지는 경우가 있기 때문에 이를 예측하기 위해서는 교반 영향을 나타내는 확산층을 고려해야 한다. 유동해석을 통해 도금액 교반 조건 및 형상에 따른 음극 표면의 유속을 결정하고 유속별 도금액 DB를 구성하여 음극의 위치별 분극곡선을 차별화하여 유동 조건에 따른 확산층 변화를 고려하는 형태로 구현하였다. 유속별 도금액 DB는 실험 데이터 및 해석 데이터를 종합하여 구축하였다. 교반의 영향을 많이 받는 시스템을 대상으로 개발된 Simulator 결과의 타당성을 검증하였고 확산층 적용에 따른 도금 결과의 차이를 확인하였다.

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A New Concept to Transport a Droplet on Horizontal Hydrophilic/Hydrophobic Surfaces (친수성/소수성 수평 표면상에서의 액적이송에 관한 새로운 개념)

  • Myong, Hyon Kook
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.38 no.3
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    • pp.263-270
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    • 2014
  • A fluid transport technique is a key issue for the development of microfluidic systems. In this paper, a new concept for transporting a droplet without external power sources is proposed and verified numerically. The proposed device is a heterogeneous surface which has both hydrophilic and hydrophobic horizontal surfaces. The numerical simulation to demonstrate the new concept is conducted by an in-house solution code (PowerCFD) which employs an unstructured cell-centered method based on a conservative pressure-based finite-volume method with interface capturing method (CICSAM) in a volume of fluid (VOF) scheme for phase interface capturing. It is found that the proposed concept for droplet transport shows superior performance for droplet transport in microfluidic systems.

Implementation of Roughness-Induced Turbulent Transition Model on Inflight Icing Code (표면 조도를 고려한 난류 천이 모델의 항공기 결빙 해석자에 대한 적용 연구)

  • Min, Seungin;Yee, Kwanjung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.1
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    • pp.23-33
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    • 2020
  • In this study, the effect of surface roughness distribution and its influence on the inflight icing code was investigated. Previous numerical studies focused on the magnitude of surface roughness, and the effects were only addressed in terms of changes in thermal boundary layers with fully turbulent assumption. In addition, the empirical formula was used to take account the turbulent transition due to surface roughness, which was regarded as reducing the accuracy of ice shape prediction. Therefore, in this study, the turbulent transition model based on the two-equation turbulence model was applied to consider the effects of surface roughness. In order to consider the effect of surface roughness, the transport equation for roughness amplification parameter was applied, and the surface roughness distribution model was implemented to consider the physical properties. For validation, the surface roughness, convective heat transfer coefficient, and ice shape were compared with experimental results and other numerical methodology. As a result, it was confirmed that the excessive prediction of the heat transfer coefficient at the leading edge and the ice horn shape at the bottom of the airfoil were improved accordingly.

Comparison of Moment Method/Monte-Carlo Simulation and PO for Bistatic Coherent Reflectivity of Sea Surfaces (바다 표면의 Bistatic Coherent Reflectivity 계산을 위한 Monte-Carlo/모멘트 법과 PO 모델 비교)

  • Kim Sang-Keun;Oh Yi-Sok
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.17 no.1 s.104
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    • pp.39-44
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    • 2006
  • This paper proposes a method of moments(MoM)/Monte-Carlo simulation and Physical Optics(PO) model to determine Bistatic Coherent Reflectivity of sea surfaces at various wind speeds. For the MoM simulation, a Gaussian random rough sea surface was generated based on the data of Tae-An ocean at various wind speeds and sea surface heights. The numerical results of the MoM/Monte Carlo simulations were used to verify the validity region of the PO model. It was found that the numerical result for a flat surface agrees quite well with the Fresnel reflection coefficient. The validity of the PO model on the rough sea surface is shown by using ray tracing method.

A Study on the Structure Strength of Wing In Ground effect Ship (표면 효과익선(WIG)의 구조 강도에 관한 연구)

  • 고재용;박석주;정성호;박성현
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2002.11a
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    • pp.95-100
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    • 2002
  • The wing in ground effect (WIG) ship is an energy saying vessel that uses the lift from its air-wing along with the lift increase from the ground effect by flying low above the sea surface. The WIG Ship should consist of thin plate in order to float on the sea and to fly in the air. Therefore, the structure of WIG, Ship has very thin and light shell plate and stiffener like stringer and frame has comparatively large cross section area. This structure makes shell plate nearly pure shear field when shell plate is pressed by in-plane load. This complex thin plate structure of WIG Ship can he considered as a closed section beam which makes it possible to analyze structure response of WIG Ship affected by shear load and bending load. In this respect, the present study will show basic theory for analysing shear stress and focus on the analysis of structure strength of model WIC Ship's wing.

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Numerical Simulation of Radar Backscattering from Oil Spills on Sea Surface for L-band SAR (기름이 유출된 바다 표면의 L-밴드 전파 산란에 대한 수치해석적 연구)

  • Park, Seong-Min;Yang, Chan-Su;Oh, Yi-Sok
    • Korean Journal of Remote Sensing
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    • v.26 no.1
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    • pp.21-27
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    • 2010
  • This paper presents a numerical simulation of the radar backscattering from oil spills on ocean surface. At first, a one-dimensionally rough sea surface is numerically generated for a given wind speed at HEBEI SPIRIT accident. Then, an oil-spilled sea surface is represented with a two-layered medium, which is generated by adding a thin low-dielectric oil layer on the randomly-rough highdielectric sea surface. The backscattering coefficients of various oil-spilled sea surfaces are obtained using the Method of Moments and Monte Carlo technique for various surface roughness, oil-layer thicknesses, frequencies, polarizations and incidence angles. The numerical method is verified with theoretical models for simple structures. The reduction of the backscattering coefficients due to the lowdielectric oil-layers on sea surfaces has been analyzed. These numerical results will help to detect any oil spills on sea surfaces, and consequently, to classify SAR images.

Prediction of Radiated Sound Field by Using Boundary Element Method Based on the Pressure Measurements (음장측정치를 사용한 경계요소법에 의한 진동체 방사음장 예측)

  • 김봉기;김진연;이정권
    • The Journal of the Acoustical Society of Korea
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    • v.12 no.2
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    • pp.28-36
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    • 1993
  • 임의의 형상을 갖는 진동체에 의한 방사 음장해석은 경계요소법에 의하여 이미 많은 해석이 시도되었다. 그러나, 진동체의 형상이 매우 복잡한 경우에는 겉표면의 요소수가 크게 증가할 뿐만 아니라 각 요소에서의 경계조건을 모두 알아내어야 하므로, 저주파에 국한된 해석일지라도 엄청난 시간과 노력이 필요하게 된다. 이러한 어려움을 극복하기 위하여 경계요소법을 사용하되, 복잡한 형상의 진동체를 둘러싸는 가상적인 표면을 매우 간단하게 설정한 후 그 표면상의 경계조건인 음압을 측정한다. 임의의 형상에 대한 파수 영역에서의 감쇠파의여파작업을 위하여 특이값 분리를 사용하였다. 특이값 분리에 의하여 음압분포를 측정위치에서 설정된 일반 좌표계에서의 고유모드로 분해한다. 각 고유모드의 원거리 음장의 기여도에 해당하는 각 특이벡터에 대한 특이값의 크기를 비교하여, 유한개의 고유모드만을 포함시킴으로써 원거리 음장을 예측한다. 몇 개의 예제를 통하여 해석적 방법의 기존의 경계요소법에 의한 결과를 본 연구 방법의 결과와 비교하여 잘 일치함을 확인하였다.

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