• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 1999년도 봄 학술발표회 논문집(I)
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• pp.709-714
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• 1999

The objectives of this study are to estimate the strengthening effect of concrete column strengthened with CFS and to provide basic guideline for the strengthening design with laminated composite materials. Analysis stress-strain model of laminated CFS is presented based on laminate theory. This model has been implemented in the algorithm of evaluating confinement effect of CFS. From results of the algorithm, stress-strain relationship of confined concrete is obtained. Using this stress-strain relationship, section analyses of circular and rectangular concrete columns strengthened with CFS are carried our, and load-moment interaction and load-ductility curves of the columns are obtained. To evaluate the strengthening effects of CFS, parametric study is also conducted for the angle of ply, thickness of CFS, shape of section, and reinforcement ratio. Based on this investigation, design recommendations and basic guidelines for the strengthening design with CFS are proposed.

• 한국초전도ㆍ저온공학회논문지
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• 제5권3호
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• pp.43-47
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• 2003

For an electrical insulation design of HTS cable, it is important to understand the dielectric characteristics of insulation materials in $LN_2$ and the insulation type. Generally, the electrical insulation of HTS Cable is classified into two types of the composite insulation and solid insulation type. In this research, we selected the insulation paper/$LN_2$ composite insulation type for the electric insulation of a HTS cable, and studied electric insulation characteristics of synthetic Laminated Polypropylene Paper (LPP) in liquid nitrogen ($LN_2$) for the application to high temperature superconducting (HTS) cable. Furthermore, we compared the breakdown characteristics of the butt gap and bended mini-model cable. It is necessary to understand the winding parameter of insulation paper/$LN_2$ composite insulation.

• Structural Monitoring and Maintenance
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• 제4권2호
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• pp.133-151
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• 2017

The paper describes the results of an experimental and numerical investigation into the structural and damage response of sandwich composites to low-velocity impact. Sandwich panels consisting of laminated composite skins with three different layups bonded to a PVC foam core were subjected to impact at various energy levels corresponding to barely visible impact damage (BVID) in the impacted skins. Damage assessment analyses were performed on the impacted panels to characterise the extent and the nature of the major failure mechanisms occurring in the skins. The data collected during the experimental analyses were finally used to assess the predictive capabilities of an FE tool recently developed by the authors for detailed simulation of impact damage in composite sandwich panels. Good agreement was observed between experimental results and model predictions in terms of structural response to impact, global extent of damage and typical features of individual damage mechanisms.

• Composites Research
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• 제12권5호
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• pp.80-86
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• 1999

본 연구에서는 카본 스크림과 유리 스크림을 사용한 복합적층판과 원형 관의 기계적 특성을 평가하였다. 탄소섬유강화 복합재료의 층과 층 사이에 카본 스크림 또는 유리 스크림을 사용하여 제작하였다. ASTM 규격에 따라 섬유방향의 강도와 강성, 섬유수직방향의 강도와 강성 그리고 전단강도와 전단강성을 측정하였다. 본 실험 결과, 스크림재료를 사용한 경우에 섬유방향의 기계적 특성은 감소하였으나, 섬유수직방향의 기계적 특성은 상당히 개선되었다.

• Composites Research
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• 제14권2호
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• pp.50-59
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• 2001

다목적헬리콥터용으로 설계된 복합재 무힌지 로터깃에 대하여 강도저하모델을 활용하여 비행모사 하중스펙트럼에 따라 피로파손 확률분포와 잔여강도 변화거동을 해석하여 피로수명을 예측하였다. 이때 작용하는 피로하중은 실제 헬리콥터 운용상태를 모사하는 무힌지 로터깃의 표준하중스펙트럼인 FELIX 데이터로부터 비행 대 비행 하중스펙트럼을 구성하였고 피로손상이 가장 극심하게 예상되는 깃뿌리 부근의 국부응력스펙트럼은 스킨과 스파의 적층구조해석을 수행함으로써 구하였다.

• 한국자동차공학회논문집
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• 제7권8호
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• pp.272-281
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• 1999

Cylindrical panels are widely used as aircraft fuselages and rocket etc, and the cutouts for weight reduction or wiring at such structures tend to cause the stress concentration and the local radial displacement so that seriously effect the stability of structures. In this paper, for the cylindrical composite panel with coutout at the center, the buckling and postbuckling behaviour regarding the shape and size of cutout is analyzed by finite element method. Also the lamination mechanism , changing bending stiffness and fiber orientation angle variation are researched to be regarded in studying the laminated composite materials.

• Structural Engineering and Mechanics
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• 제31권5호
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• pp.481-506
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• 2009

The present study is concerned with the stochastic linear free vibration study of laminated composite plate embedded with piezoelectric layers with random material properties. The system equations are derived using higher order shear deformation theory. The lamina material properties of the laminate are modeled as basic random variables for accurate prediction of the system behavior. A $C^0$ finite element is used for spatial descretization of the laminate. First order Taylor series based mean centered perturbation technique in conjunction with finite element method is outlined for the problem. The outlined probabilistic approach is used to obtain typical numerical results, i.e., the mean and standard deviation of natural frequency. Different combinations of simply supported, clamped and free boundary conditions are considered. The effect of side to thickness ratio, aspect ratio, lamination scheme on scattering of natural frequency is studied. The results are compared with those available in literature and an independent Monte Carlo simulation.

• 한국농공학회지
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• 제43권1호
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• pp.122-128
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• 2001

The theory of non-prismatic folded plate structures was reported by D.H. Kim in 1965 and 1966. Fiber reinforced composite materials are strong in tension. The structural element for such tension force is very thin and weak against bending because of small bending stiffnesses. Naturally, the box type section is considered as the optimum structural configuration because of its high bending stiffnesses. Such structures can be effectively analyzed by the folded plate theory with relative ease. The “hollow” bending membr with uniform cross-section can be treated as prismatic folded plates which is a special case of the non-prismatic folded plates. In this paper, the result of analysis of a folded plates with one box type uniform cross-section is presented. Each plate is made of composite laminates with fiber orientation of [ABBCAAB]r, with A=-B=45${\circ}C$, and C=90${\circ}$. The influence of the span to depth ratio is also studied. When this ratio is 5, the difference between the results of folded plate theory and beam theory is 1.66%.

• Composites Research
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• 제26권4호
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• pp.265-272
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• 2013

섬유강화플라스틱(Fiber-reinforced plastic, FRP)은 복합재료 보트를 만드는 데 주 구조물로 사용되고 그것들 대부분은 몰드에서 만들어진다. 이러한 제품들은 몰드에서 분리될 때나 높은 온도의 환경에서 변형이 생긴다. 그러므로 다양한 제작 및 작동 조건에서 적층복합재료 구조물의 변형에 대한 실험적 조사 및 평가는 필수적이다. 불포화 폴리에스테르수지와 유리섬유를 이용하여 L-shape과 Curve-shape 시편을 제작하였다. 경화제 비율과 제작온도, 네 가지 작동온도가 입력인자(독립변수)로 사용되었고 출력인자는 시편에서 측정되는 변형이다. 결과로부터 경화제 비율이 높을수록 또한 제작온도가 높을수록 변형이 작게 생김을 알 수 있었다. 작동온도가 상승할 때 초기 변형 값에 따라 큰 변화를 보였다. 또한 변형 값이나 입력인자들은 회귀 방정식으로부터 예측할 수 있었다.

• 대한기계학회논문집A
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• 제33권1호
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• pp.1-26
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• 2009

Cylindrical shells of isotropic and composite laminated materials are being used many engineering applications. This paper reviews the literature focusing on various aspects of shell research. The aspects of research receiving interest here are the cylindrical theory being used, the stress, buckling analysis and the impact analysis. The vibration analyses and stiffening characteristics of the cylindrical shell are investigated. The design optimizations of the cylindrical shell are reviewed. The studies on the conical and spherical shell are also reviewed. This review aticles contain 236 referencees.