• Structural Engineering and Mechanics
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• 제15권4호
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• pp.463-476
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• 2003

This paper deals with nonlinear asymmetric dynamic buckling of clamped laminated angle-ply composite spherical shells under suddenly applied pressure loads. The formulation is based on first-order shear deformation theory and Lagrange's equation of motion. The nonlinearity due to finite deformation of the shell considering von Karman's assumptions is included in the formulation. The buckling loads are obtained through dynamic response history using Newmark's numerical integration scheme coupled with a Newton-Raphson iteration technique. An axisymmetric curved shell element is used to investigate the dynamic characteristics of the spherical caps. The pressure value beyond which the maximum average displacement response shows significant growth rate in the time history of the shell structure is considered as critical dynamic load. Detailed numerical results are presented to highlight the influence of ply-angle, shell geometric parameter and asymmetric mode on the critical load of spherical caps.

• 대한조선학회지
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• 제21권2호
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• pp.19-27
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• 1984

An extension of the finite element method to the stability analysis of shells of revolution under static axisymmetric loading is presented in this paper. A systematic procedure for the formulation of the problem is based upon the principle of virtual work. This procedure results in an eigenvalue problem. For solution, the shell of revolution is discretized into a series of conical frusta. The buckling mode in the circumferential direction is assumed, this assumption makes the problem economical for the computing time. The present method is applied to a number of shells of revolution, under axial compression or lateral pressure, and comparision are made with other theoretical results. The results show good agreement each other. The effects of aspect ratio, boundary conditions and buckling modes on the buckling strength of shells of revolution are studied. Also the optimum shape of cylindrical shell under uniform axial compression is obtained from the view point of structural stability.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집A
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• pp.602-607
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• 2000

Fuel-storage tank is a representative example of liquid-structure interaction systems. In order to prevent the undesired structural failure by a variety of external loads, the reliable analysis of the dynamic response of such structural system is of a great importance. In this paper, we address the analytical study on free vibration of axisymmetric cylindrical fuel-storage tanks together with the parametric investigation of eigen-characteristics with respect to the relative fuel fill-height and the relative tank height. Numerical results illustrating theoretical results are also included.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2001년도 추계학술대회논문집 II
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• pp.876-876
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• 2001

Axisymmetric finite element model is developed to determine sound propagation characteristics in a circular duct lined with a poroelastic foam. The foam and air models are derived based on the Biot's theory and the Helmholtz equation respectively and finally result in a quadratic eigenvalue problem in the wave number. Some cross sectional mode shapes are shown and sound attenuations and phase speeds of some acoustic modes are given. Those of fundamental modes are compared with those by forced response solutions and those from measurement results. The influence of lining thickness is also described on sound propagation characteristics.

• 한국광학회지
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• 제14권3호
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• pp.219-223
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• 2003

광섬유의 잔류응력(residual stress)을 측정하기 위해 위상보정 편광기(polariscope)를 새롭게 구성하고, 간섭이나 회절에 대한 영향을 최소화시키면서 빠르고 정확하게 측정하는 방법을 제시하였다. 이 방법을 이용하여 일반 광섬유의 잔류 응력 분포를 측정할 수 있었다. 또한 광섬유의 잔류응력이 모재의 잔류응력분포와 달리 인출 시 발생하는 광섬유 내 온도의 냉각곡선에 밀접한 관계를 갖고 있음을 알 수 있었다.

• Advances in nano research
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• 제15권2호
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• pp.141-153
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• 2023

The main objective of this paper is to develop the finite element study on the nonlinear free vibration of functionally graded nanocomposite spherical shells reinforced with graphene platelets under the first-order shear deformation shell theory and von Kármán nonlinear kinematic relations. The governing equations are presented by introducing the full asymmetric nonlinear strain-displacement relations followed by the constitutive relations and energy functional. The extended Halpin-Tsai model is utilized to specify the overall Young's modulus of the nanocomposite. Then, the finite element formulation is derived and the quadrilateral 8-node shell element is implemented for finite element discretization. The nonlinear sets of dynamic equations are solved by the use of the harmonic balance technique and iterative method to find the nonlinear frequency response. Several numerical examples are represented to highlight the impact of involved factors on the large-amplitude vibration responses of nanocomposite spherical shells. One of the main findings is that for some geometrical and material parameters, the fundamental vibrational mode shape is asymmetric and the axisymmetric formulation cannot be appropriately employed to model the nonlinear dynamic behavior of nanocomposite spherical shells.

• 대한기계학회논문집B
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• 제29권9호
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• pp.997-1005
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• 2005

The extinction characteristics of low strain rate normal gravity (1-g) nonpremixed methane-air flames were studied numerically and experimentally. A time-dependent axisymmetric two-dimensional (2D) model considering buoyancy effects and radiative heat transfer was developed to capture the structure and extinction limits of 1-g flames. One-dimensional (1D) computations were also conducted to provide information on 0-g flames. A 3-step global reaction mechanism was used in both the 1D and 2D computations to predict the measured extinction limit and flame temperature. A specific maximum heat release rate was introduced to quantify the local flame strength and to elucidate the extinction mechanism. Overall fractional contribution by each term in the energy equation to the heat release was evaluated to investigate the multi-dimensional structure and radiative extinction of 1-g flames. Images of flames were taken for comparison with the model calculation undergoing extinction. The two-dimensional numerical model was validated by comparing flame temperature profiles and extinction limits with experiments and ID computation results. The 2D computations yielded insight into the extinction mode and flame structure of 1-g flames. Two combustion regimes depending on the extinction mode were identified. Lateral heat loss effects and multi-dimensional flame structure were also found. At low strain rates of 1-g flame ('Regime A'), the flame is extinguished from the weak outer flame edge, which is attributed to multi-dimensional flame structure and flow field. At high strain rates, ('Regime B'), the flame extinction initiates near the flame centerline due to an increased diluent concentration in reaction zone, which is the same as the extinction mode of 1D flame. These two extinction modes could be clearly explained with the specific maximum heat release rate.

• 한국구조물진단유지관리공학회 논문집
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• 제8권1호
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• pp.195-202
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• 2004

일반적으로 쉘 표면에 수직한 압력은 변형 전 쉘 표면에 수직한 방향으로 작용한다고 가정하고 쉘 표면의 변형으로 인한 표면적의 변화를 고려하지 않음으로써 이에 의한 변형에너지를 무시한다. 그러나, 변형된 쉘 표면에 수직으로 작용하는 압력은 고유진동수와 좌굴하중에 큰 영향을 미칠 수 있다. 본 연구에서는 구조물의 변형에 의한 쉘 단면적의 변화와 압력의 방향변화에 대한 변형에너지를 구하고 이를 변분하여 부가매트릭스를 산정하였다. 이를 축대칭요소에 추가하여 전산구조해석을 통해 외압의 부가효과를 고려한 고유진동수를 계산하였다. 외압의 크기가 증가함에 따라 쉘 구조물의 고유진동수는 감소하며, 고유진동수가 영이 될 때의 외압의 크기를 좌굴하중으로 볼 수 있다. 이를 이용하여 정해가 존재하는 원통 쉘에 적용한 결과 유사한 해를 얻을 수 있었으며, 부가효과를 고려하지 않았을 경우는 상당한 차를 나타내었다. 그러나, 반구형 돔에서는 원통 쉘에 비해 압력의 부가효과가 거의 나타나지 않는 것으로 나타났다.

• 비파괴검사학회지
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• 제21권4호
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• pp.406-414
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• 2001

폴리에틸렌 코팅 가스배관의 결함탐상을 위해 광범위 비파괴탐상기법인 유도초음파를 적용하였다. 가스배관의 내경은 190.7mm, 두께는 5.3mm, 그리고 바깥 표면은 $1.9{\pm}0.5mm$의 폴리에틸렌 층으로 코팅되어 있다. 폴리에틸렌 코팅 배관의 외면에 0.5MHz 탐촉자와 가변각 웨지를 사용하여, 비축대칭 유도초음파를 가진 시켰다. 주파수와 위상속도 조정을 통하여 가스배관의 결함 탐상을 위한 적절한 모드를 찾아내고, 모드의 특성을 단시간 퓨리어 변환을 이용하여 분석하였다. 결함탐상 결과를 두께 손실 및 원통형 관통결함에 대한 인위결함에 대해 나타내었다. 그리고 가스배관에 인위적으로 삽입한 두께 손실과 원통형 관통결함에 대한 검출 성능을 평가하였다.

• The Journal of Advanced Prosthodontics
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• 제4권3호
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• pp.139-145
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• 2012

PURPOSE. To evaluate the shear bond strength of resin luting agent to dentin surfaces cleansed with different agents like pumice, ultrasonic scaler with chlorhexidine gluconate, EDTA and the influence of these cleansing methods on wetting properties of the dentin by Axisymmetric drop Shape Analysis - Contact Diameter technique (ADSA-CD). MATERIALS AND METHODS. Forty coronal portions of human third molar were prepared until dentin was exposed. Specimens were divided into two groups: Group A and Group B. Provisional restorations made with autopolymerizing resin were luted to dentin surface with zinc oxide eugenol in Group A and with freegenol cement in Group B. All specimens were stored in distilled water at room temperature for 24 hrs and provisional cements were mechanically removed with explorer and rinsed with water and cleansed using various methods (Control-air-water spray, Pumice prophylaxis, Ultrasonic scaler with 0.2% Chlorhexidine gluconate, 17% EDTA). Contact angle measurements were performed to assess wettability of various cleansing agents using the ADSA-CD technique. Bond strength of a resin luting agent bonded to the cleansed surface was assessed using Instron testing machine and the mode of failure noted. SEM was done to assess the surface cleanliness. Data were statistically analyzed by one-way analysis of variance with Tukey HSD tests (${\alpha}$=.05). RESULTS. Specimens treated with EDTA showed the highest shear bond strength and the lowest contact angle for both groups. SEM showed that EDTA was the most effective solution to remove the smear layer. Also, mode of failure seen was predominantly cohesive for both EDTA and pumice prophylaxis. CONCLUSION. EDTA was the most effective dentin cleansing agent among the compared groups.