• Proceedings of the Materials Research Society of Korea Conference
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• 2003.03a
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• pp.194-194
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• 2003

지르콘은 내침식성, 내마모성, 열 충격 저항성 및 기계적 물성이 우수하여 내화재료, 연마재료 등으로 다양하게 활용된다. 이러한 지르콘의 물성은 출발원료의 입도와 순도, 첨가제, 열처리 온도 등에 크게 의존한다. 본 연구에서는 출발 물질의 평균 입도를 각각 5$\mu\textrm{m}$와 3$\mu\textrm{m}$, l$\mu\textrm{m}$ 이하로 제어하였고, 시료의 열처리 온도를 135$0^{\circ}C$, 140$0^{\circ}C$, 145$0^{\circ}C$, 150$0^{\circ}C$, 155$0^{\circ}C$로 소결하였다. 각각의 지르콘 소결체는 미세 경도 측정, 결정상 분석, 밀도 측정, 미세구조 관찰을 통하여 특성 평가하였다. 미세경도 값은 140$0^{\circ}C$에서 소결된 지르콘의 가장 높았으며, 밀도는 150$0^{\circ}C$에서 소결된 지르콘이 가장 높으며, 155$0^{\circ}C$에서 소결된 지르콘은 과소결되어 전체적으로 물성이 저하되는 것을 관찰하였다.

• Polymer(Korea)
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• v.25 no.3
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• pp.406-413
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• 2001

Blending has become an interesting way for preparing new materials with tailored properties. Unfortunately, many materials are incompatible due to the difference in their viscoelastic properties, surface energy and interaction. Therefore, the properties of polymer blends are not obtained as expected levels. Silicone rubber has an excellent heat-resistance and electrical characteristics, and ethylene propylene diene monomer (EPDM) rubber also has good mechanical properties. The purpose of this study is to develop a new engineering material which has excellent electrical and mechanical properties through blending of silicone with EPDM rubber.

• Proceedings of the Membrane Society of Korea Conference
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• 1998.06a
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• pp.49-80
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• 1998

다른 프로세스와의 경쟁력확보를 위해서는 막소재의 혁신적인 성능향상이 수반되어야 한다. 그러므로 막소재의 물성에 대한 고찰이 필요한데, 이는 고분자재료의 고유한 성질에 \ulcorner랴 분리막의 성능이 좌우되기 때문이다. 막재료로서의 고분자의 성질은 매우 여러 가지가 있지만 본 고에서는 막분리성능에 크게 관련되는 고분자의 물성 및 종류에 대해 논하겠다.

• Composites Research
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• v.27 no.6
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• pp.219-224
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• 2014

Nancomposites manufacture has been developed rapidly, because of reinforcing effects of CNT in terms of mechanical, electrical and thermal properties. In this study, 10 wt% CNT paste was fabricated with good dispersion state and easy processability. Damage sensing and reinforcing effect of CNT paste were investigated in nanocomposites. 10 wt% CNT paste exhibited better tensile and flexural properties than those of general 1 wt% CNT nanocomposites. To observe the healing effect of CNT paste, a crack was made artificially with 30wt% CF30wt%/PP composites, and the CNT paste was filled inside the crack. The damage sensing of CNT paste in CF30wt%/PP composites was investigated by electrical resistance measurement and mechanical tests. CNT paste exhibited good reinforcing effect in mechanical properties of CF30wt%/PP composites, and this reinforcing effect was getting better with larger cracks. The reason was because CNT paste had good interfacial adhesion with CF30wt%/PP composites to resist crack propagation. In electrical resistance measurement, there was a jump in electrical resistance signal at the adhesion interface. The jumping signal could be used to predict fracture of CF/PP composites. CNT nanocomposites for damage sensing had crack reducing effect and damage detection using electrical resistance method.

• Composites Research
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• v.16 no.1
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• pp.42-49
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• 2003

Brittle matrix composites often have interfacial debonding between the fiber and matrix which may lead to strength and stiffness degradation. The effect of interfacial debonding and fiber volume fraction on the mechanical properties of composite material were studied by using finite element method. Firstly, the modelling of fiber and matrix constituting the composite material was simplified under some assumptions. Traction and displacement continuity conditions were imposed along the boundary of adjacent representative volume elements. In order to obtain the effective material properties of composite material, stiffness constants were inverted. Numerical values of longitudinal moduli in case of perfect bonding were compared with theoretical values obtained by rule of mixtures and yielded consistency. Material properties of composite with large debonding an81e were found to decrease even though the fiber volume fraction increased.

• Proceedings of the Materials Research Society of Korea Conference
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• 2009.05a
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• pp.41.2-41.2
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• 2009

최근 자동차 시장에서는 레이저 열처리에 대한 관심이 집중되고 있다. 이는 현재까지 사용되어 왔던 점용접에 비해 이음부 형상에 제한이 적고 자유도가 높으며 짧은 시간내에 용접을 마쳐 열변형의 문제가 적기 때문이다. 이러한 이점 때문에 자동차 시장의 기술개발 동향이 차체 부품의 경량화와 원가절감을 위한 신기술 개발로 레이저 가공 기술을 접목시키고 있으며 이러한 신공정 개발은 지속적으로 확대되어 가고 있는 추세이다. 본 실험에서는 차체 접합을 위하여 신기술로 대두 되고 있는 레이저 용접법으로 박판을 접합하였다. 실험 조건은 동일한 재료 두 판을 합쳐 전력량을 변화시켰으며, 전력량의 한 조건을 잡아 용접 속도에 변화를 주었다. 용접 샘플의 물성을 평가하기 위하여 제품 내부의 구조를 비파괴 시험법을 통하여 분석하여 내부적 결함 및 내부 구조를 관찰하고, 열영향부 및 용접부 내부의 조직을 관찰하여 신기술에 대해 재료적 물성을 평가하고자 한다. 평가방법은 산업용 단층 촬영기(CT X-RAY)를 이용하여 재료를 파괴하지 않고 용접상태에 따른 내부구조를 분석하였으며, 용접부, 열영향부 그리고 모재 부분에 대해 경도를 측정하여 용접조건에 따른 경도양상을 관찰하였다. 또한 부위별로 조직을 관찰하여 재료 내부의 상을 관찰하였다.

• Composites Research
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• v.16 no.5
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• pp.7-14
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• 2003

Modeling of thick composite structures for finite element analysis is relatively complicated. 2-D plane elements may cause inaccurate result since the plane stress condition cannot be applicable in these structures. Therefore a 3-D modeling should be used. However, the difficulty to model all the layers with different material properties and ply orientation arise in this case. In this paper, an equivalent modeling is proposed and numerically tested for analysis of thick composite structures. By grouping layers with same material and ply orientation, number of elements through the thickness is remarkably reduced and still the result is close enough to the one from a detail finite element model. MSC/NASTRAN and PATRAN are used for the analysis. The proposed modeling technique has been applied for analysis of composite rotor hub system designed by Korea Aerospace Research Institute(KARI). Using the proposed equivalent modeling technique, we could conduct stress analysis for the hub system and check the safety factor of each part.

• Composites Research
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• v.36 no.4
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• pp.275-280
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• 2023

Because polymer-based composites are lightweight and have excellent properties, their demand is growing rapidly as a way to fulfill properties that are difficult to achieve with a single material. As a result, there has been a lot of research on polymer nanocomposites, which are made by dispersing particles with a size of 1-100 nm in a polymer matrix. In addition, many nanocomposites using thermoplastic resins as matrix materials are being studied. In this study, poly(ethylene terephthalate) (PET)-based nanocomposites containing organic nanoclays modified with cetyltrimethylammonium bromide (CTAB) as interlayer materials were prepared. Among various nanoclays, vermiculite (VMT) has been studied to increase the mechanical and thermal properties of polymeric materials due to its low cost, abundant reserves and unique properties. However, the strong interlayer bonding of VMT has limited its utilization due to its poor exfoliation and dispersion performance within polymer matrices. In this study, the mechanical properties of the VMT content were confirmed by tensile tests, the dispersion of VMT particles in the PET matrix was evaluated by TEM cross-sectional images, and the nitrogen gas barrier properties were evaluated.

• Composites Research
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• v.22 no.4
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• pp.20-26
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• 2009

In the current study, thermoforming and compression analysis were carried out for the woven composite egg-box panel with the non-orthogonal constitutive material model, which is proposed by Xue et al. The material model is implemented in commercial engineering software, LS-DYNA, with a user subroutine. Directional properties in non-orthogonal coordinates are determinedusing the deformation gradient tensor and the material modulus matrix in local coordinate is updated at eaeh corresponding time step. After the implemented non-orthogonal constitutive model is verified by the bias extension test, the egg-box panel simulations are performed. The egg-box panel simulations are divided into two categories: thermoforming (draping) and crushing. The finite element model for crushing analysiscan be obtained using the displacement result of thermoforming process.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.29 no.1
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• pp.61-65
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• 2016

Composites are materials that are widely used in industries such as automobile and aircraft. The composite material is required as a material for using in a high temperature environment as well as acting as a high pressure environment like the nozzle part of the ship. It is important to know the properties of composites. Result values obtained substituting the properties of matrix and fiber numerically have an large error compared with experimental value. In this study we utilize CASADsolver EDISON program for using Finite Element Method. Properties by substituting the fiber and Matrix properties of the composite material properties were compared with those measured in the experiment and calculated by the empirical properties.