• 한국세라믹학회지
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• 제44권7호
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• pp.368-374
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• 2007

CVD-SiC coating has been introduced as a protective layer in TRISO nuclear fuel particle of high temperature gas cooled reactor (HTGR) due to its excellent mechanical stability at high temperature. In order to prevent the failure of the TRISO particles, it is important to evaluate the fracture strength of the SiC coating layer. It is needed to develop a new simple characterization technique to evaluate the mechanical properties of the coating layer as a pre-irradiation step. In present work, direct strength measurement method with the specimen of hem i-spherical shell configuration was suggested. The indentation experiment on a hemisphere shell with a plate indenter was conducted. The fracture strength of the coating layer is related with the critical load for radial cracking of the shell. The finite element analysis was used to drive the semi-empirical equation for the strength measurement. The SiC hemispherical shells were successfully recovered from the section-grinding of TRISO coated particle and successive heat treatment in air. The strength of CVD-SiC coating layer was evaluated from the experimentally measured critical load during the indentation on SiC hemisphere shell. Weibull diagram of fracture strength was also constructed. This study suggested a new strength equation and experimental method to measure the fracture strength of CVD-SiC coating of TRISO coated fuel particles.

• 한국해양공학회지
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• 제35권5호
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• pp.327-335
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• 2021

Microcracks can rapidly grow and develop in high-strength steels used in offshore structures. It is important to render these microcracks harmless to ensure the safety and reliability of offshore structures. Here, the dependence of the aspect ratio (As) of the maximum depth of harmless crack (a_hlm) was evaluated under three different conditions considering the threshold stress intensity factor (Δk_th) and residual stress of offshore structural steel F690. The threshold stress intensity factor and fatigue limit of fatigue crack propagation, dependent on crack dimensions, were evaluated using Ando's equation, which considers the plastic behavior of fatigue and the stress ratio. a_hlm by peening was analyzed using the relationship between Δk_th obtained by Ando's equation and Δk_th obtained by the sum of applied stress and residual stress. The plate specimen had a width 2W = 12 mm and thickness t = 20 mm, and four value of As were considered: 1.0, 0.6, 0.3, and 0.1. The a_hlm was larger as the compressive residual stress distribution increased. Additionally, an increase in the values of As and Δk_th(l) led to a larger a_hlm. With a safety factor (N) of 2.0, the long-term safety and reliability of structures constructed using F690 can be secured with needle peening. It is necessary to apply a more sensitive non-destructive inspection technique as a non-destructive inspection method for crack detection could not be used to observe fatigue cracks that reduced the fatigue limit of smooth specimens by 50% in the three types of residual stresses considered. The usefulness of non-destructive inspection and non-damaging techniques was reviewed based on the relationship between a_hlm, a_NDI (minimum crack depth detectable in non-destructive inspection), a_{cr N} (crack depth that reduces the fatigue limit to 1/N), and As.

• 대한토목학회논문집
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• 제33권6호
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• pp.2411-2425
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• 2013

퇴적층과 암반층이 층상구조로 되어있는 지반의 층상암반층 위에 말뚝기초를 설계할 경우, 연직하중에 대한 지지암반의 파괴모드(휨파괴, 펀칭전단파괴 혹은 선단지지파괴)를 검토하고 지지력을 계산하기 위해서는 층상지지암반층의 구조해석이 필요하다. 그러나 ACI committee 436과 우리나라 구조물기초설계기준에서 제안하고 있는 기존의 이용 가능한 탄성평판해석법(Elastic Plate Analysis Method)은 매우 복잡하여 기술자가 이용하는데 어려움이 많다. 따라서 본 연구에서는 복잡한 탄성평판해석법 대신 비교적 간단한 원형기초해석법(Circular Foundation Analysis Method)을 이용할 수 있도록 등가유효폭(반경)의 개념과 식을 제시하였고, 이를 통하여 탄성평판해석에 의한 모멘트와 전단력이 원형평판해석의 결과와 같도록 관계식을 제안하였다. 그 결과 등가유효폭을 이용한 원형기초해석의 방법은 매우 단순하고 편리하였고, 제안된 방법에 의한 결과를 탄성평판해석과 유한요소해석 결과와 비교한 결과 매우 잘 일치하였다.

• 한국전산구조공학회논문집
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• 제13권1호
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• pp.25-35
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• 2000

일반적으로 보에 의해서 탄성 지지된 등방성 판은 슬래브교(Slab Bridge)나 거더교(Slab on Girder Bridge)와 같은 교량의 상부구조를 형성하게 된다. 그러나 이러한 탄성 지지된 등방성 판에 대한 해석은 주로 고정 지지된 경계 조건만을 이용하여 이루어 졌으며, 근래에 제시된 해석방법에서도 판 경계의 처짐 형상을 가정하거나 하중 위치를 고정한 상태에서 정해를 유도하므로 탄성지점인 보와 판의 상호관계를 정확하게 묘사하지 못하고 있다. 또한 유한 요소법을 이용한 해석은 정확한 결과를 얻을 수 있는 반면, 많은 해석시간을 요하는 문제점을 안고 있다. 따라서,. 본 연구에서는 조화해석법을 적용하여 보와 등방성 판의 매크로 요소(Macro Element)의 변위 함수를 구성하고, 이를 판의 탄성 지점에서의 평형방정식을 이용해 계산함으로써 단시간 내에 전체 시스템의 응답을 결정할 수 있는 해석법을 개발하고 이를 프로그램화하였다. 또한, 본 해석법의 타당성을 검증하기 위해서 다양한 하중 조건과 판의 형상비, 탄성 지점 조건 등을 가진 교량 바닥판에 대한 해석을 수행하였으며, 해석법의 단순성 과 해석시간의 단축으로 교량 바닥판과 거더에 대한 매개변수 분석 등에 사용될 수 있을 것이다.

• 태양에너지
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• 제13권1호
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• pp.11-21
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• 1993

이차원(二次元) 충돌공기분류계(衝突空氣噴流系)에서 흐름방향과 수직(垂直)이 되게 설치한 평판전열면(平板傳熱面) 전방(前方)에 난류촉진체(亂流促進體)인 정4각(正4角) 로드군(群)(로드폭=4mm, 로드피치=50mm)을 설치하고 로드와 전열면(傳熱面)사이의 간극(間隙)(C=1, 2, 4, 6mm), 노즐출구와 전열면간(傳熱面間) 거리(H/B=2, 6, 10, 14) 및 Re수($Re=6.410{\times}10^3{\sim}5.769{\times}10^4$)를 변화시켜 실험한 결과, 평판(平板)에서 열전달계수(熱傳達系數)의 감소율이 큰 영역에서도 로드를 설치하므로써 높은 열전달계수(熱傳達係數)를 얻을 수 있었으며, 실험범위내의 Re수와 H/B에 대하여 열전달계수(熱傳達係數)가 최대(最大)가 되는 최적간극(最適間隙)은 C=1mm이고, 최대(最大) 열전달증진율은 H/B=2, C=1mm에서 로드를 설치하지 않은 평판(平板)보다 약 43% 증진한다.

• 한국항공우주학회지
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• 제38권5호
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• pp.403-413
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• 2010

PSE와 $e^N$-method를 이용하여 익형 위 경계층의 천이지점을 예측하였다. PSE 해석으로 부터 교란의 증폭률을 얻고 증폭률의 적분을 통해 N-factor 곡선들을 계산하였다. 평판 및 익형 위 경계층에 대한 계산결과를 기존 문헌 결과와 비교하여 코드의 검증을 수행하였다. NACA0012, NLF(1)-0414F 그리고 NLF(1)-0416 익형 위 경계층에 대한 천이지점을 예측을 수행하였다. 예측된 천이지점들이 실험결과들과 잘 일치함을 확인하였다.

• 한국전산유체공학회지
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• 제15권2호
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• pp.21-27
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• 2010

Immersed boundary lattice Boltzmann method (IBLBM) has been applied to simulate a turbulent flow over circular cylinder in a flow field effectively. Although IBLBM is very effective method to simulate the flow over a complex shape of obstacle in the flow field regardless of the constructed grids in the calculation domain, the results, however, become numerically unstable in high reynolds number flow. The most effective suggestion to archive the numerical stability in high Reynolds number flow is applying the multiple relaxation time (MRT) model instead of single relaxation time(SRT) model in the collision term of lattice Boltzmann equation. In the research MRT model for IBLBM was introduced and comparing the numerical results obtained by applying SRT and MRT. The hydraulic characteristic of cylinder in a flow field between two parallel plate at the range of $Re{\leqq}2000$represented and it is also compared the drag and lifting coefficients of the cylinder calculated by IBLBM with SRT and MRT model.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2009년 춘계학술대회논문집
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• pp.368-376
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• 2009

Studies on the effect of the wall-ion, wall-water, water-ion and ion-ion interaction on properties of water and ions in nano-channels have been performed through the use of different kinds of ions or different models of potential energy between wall-ion or wall-water. On this paper, we address the effect of water-wall interaction potential on the properties of confined aqueous solution by using the molecular dynamics (MD) simulations. As the interaction potential energies between water and wall we employed the models of the Weeks-Chandler-Andersen (WCA) and Lennard-Jones (LJ). On the MD simulations, 680 water molecules and 20 ions are included between uniformly charged plates that are separated by 2.6 nm. The water molecules are modeled by using the rigid SPC/E model (simple point charge/Extended) and the ions by the charged Lennard-Jones particle model. We compared the results obtained by using WCA potential with those by LJ potential. We also compared the results (e.g. ion density and electro-static potential distributions) in each of the above cases with those provided by solving the Poisson-Boltzmann equation.

• Advanced Composite Materials
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• 제18권4호
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• pp.327-338
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• 2009

In this paper, through an evaluation process conducted on several designs of mini-LIPCA (Lightweight Piezo-Composite curved Actuator), an optimal design of a mini-LIPCA has been proposed. Comparing with the LIPCA-C2, the design of the mini-LIPCA comes with reduced overall size and a thinner active layer. Since a variation in the number and lay-up of fiber composite layers may strongly affect the performance of the device, one is able to configure several designs of mini-LIPCA. The evaluation process is then followed in order to determine a configuration which characterizes the possibly optimal performance. That is, a design of a mini-LIPCA is said to be optimal if it is capable of producing a maximum out-of-plane displacement. The size of the LIPCA to be investigated was selected to be $10\;mm\;{\times}\;20\;mm$ in which the thickness of PZT plate is about 0.1 mm. The thickness of glass/epoxy and carbon/epoxy are about 0.09 mm and 0.1 mm, respectively. The evaluation process has been conducted thoroughly, i.e., analytical estimation, numerical approximation and the experimental measurement are all involved. Firstly, the design equation was used to calculate essential parameters of proposed lay-up configurations. Secondly, ANSYS, a commercial FEA package, was utilized to estimate displacement outputs of the actuators upon being excited. Finally, experimental measurements were able to verify the predicted results.

• 한국전산유체공학회지
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• 제20권3호
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• pp.54-61
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• 2015

In the present study, a flow solver using a kinetic BGK scheme was developed for the compressible Navier-Stokes equation. The kinetic BGK scheme was used to simulate flow field from the continuum up to the transitional regime, because the kinetic BGK scheme can take into account the statistical properties of the gas particles in a non-equilibrium state. Various numerical simulations were conducted by the present flow solver. The laminar flow around flat plate and the hypersonic flow around hollow cylinder of flare shape in the continuum regime were numerically simulated. The numerical results showed that the flow solver using the kinetic BGK scheme can obtain accurate and robust numerical solutions. Also, the present flow solver was applied to the hypersonic flow problems around circular cylinder in the transitional regime and the results were validated against available numerical results of other researchers. It was found that the kinetic BGK scheme can similarly predict a tendency of the flow variables in the transitional regime.