• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 1990.10a
• /
• pp.137-142
• /
• 1990

본 연구에서는 유한요소법을 사용하여 이방성으로 적층된 평판의 고유모드 를 예측하고, 이론적인 예측의 정확성을 연구하기 위해 사변 단순지지의 다 양한 각도로 적층된 정사각형 CFRP평판의 8번째 진동모드까지 실험적인 결 과와 비교하였다. 이 연구에서 사용된 모든 평판은 중앙면에 대칭이며, 이것 은 Bundling-stretching coupling을 제거하기 위해서이다. 그러나 만일 비대 칭적으로 적층된 평판이라면 이 효과를 포함한 해석이 되어야 할 것이다.

• Journal of the Korea institute for structural maintenance and inspection
• /
• v.15 no.6
• /
• pp.219-225
• /
• 2011

Advanced composite structures are too difficult for such design engineers for construction and some simple but accurate enough methods are necessary. The simply supported laminated plates are analyzed by the specially orthotropic laminates theory. This method, however, may be too difficult for some practising engineers. In this paper, the result of analysis for such plate by means of the beam theory with unit width is reported. The plate aspect ratio considered is from 1 : 1 to 1 : 5. Most of the bridge and building slabs on girders have large aspect ratios. For such cases further simplification is possible by neglecting the effect of the longitudinal moment terms($M_x$) on the relevant partial differential equations of equilibrium. In this paper. the influence of the aspect ratio on the natural frequency of the specially orthotropic laminated plates is studied and it is concluded that the method used is sufficiently accurate for engineering purposes. The result of this paper can be used for simply supported laminated plates analysis.

• Journal of Korean Association for Spatial Structures
• /
• v.6 no.4 s.22
• /
• pp.45-52
• /
• 2006

FRP laminated plates have strong material-nonlinearity. Through vibration Analysis of FRP laminated plates, the result of nonlinearity analysis is compared with the result of linearity analysis according to stacking angle and squency. This study is a fundamental study about displacement in nonlinearity dynamic behavior of FRP laminated plates.

• Proceedings of the Korean Vacuum Society Conference
• /
• 2010.08a
• /
• pp.120-120
• /
• 2010

유기 발광 소자는 차세대 디스플레이 소자와 조명 광원으로서 많은 응용성 때문에 활발한 연구가 진행되고 있다. 백색광을 구현하는 대표적인 방법으로는 밴드갭이 큰 고분자 물질에 염료를 넣는 방법, 적 녹 청을 순차적으로 증착하는 방법을 사용하지만 인가 전압의 증가 및 효율 저하, 유기물질의 수명감소, 색 안정성 감소, 제조공정의 복잡화의 문제가 발생된다. 이 문제를 해결하기 위하여 발광효율 및 안정성이 향상된 유기발광 재료 개발, 다층 이종구조 및 형광/인광성 물질의 도핑에 대한 연구가 진행되고 있다. 이와 더불어 기존의 수직 적층 구조에서 벗어난 평행하게 적 녹 청을 배열한 백색 유기 발광 소자 및 색변환 물질을 사용한 백색 유기발광소자가 제시되고 있다. 본 연구에서는 고분자 물질의 용해도가 다른 선택적 식각 방법을 이용하여 제조 공정이 간단하며 동일평면에서 적색 및 청색을 발광하여 백색을 발생하는 백색 유기발광소자를 제작하였다. 두 가지 유기물을 일정 성분비로 용매에 용해하여 적색 발광 고분자 발광층을 제작하였다. 이렇게 형성한 박막층을 한 가지 유기물만을 선택적으로 용해시켜 다공성 고분자 박막층을 형성 한 후 열 진공 증착법에 의해 청색 빛을 내는 저분자 유기물을 증착하여 적색과 청색이 동시에 발광하는 백색 유기 발광 소자를 제작하였다. 다공성고분자/저분자 층이, 수직 적층된 구조와 비교하였을 때 수직 적층된 구조는 높은 highest occupied molecular orbital 준위를 가진 저분자층으로 인해 적색에서 청색 발광층으로 정공의 주입이 일어나지 않는다. 그러나 적색과 청색이 평행한 적층 구조를 가진 발광소자인 경우 정공이 적색층과 청색층에 동시에 주입되기 때문에 문턱전압의 감소하고 백색의 빛을 발광하였다.

• Journal of the Korea institute for structural maintenance and inspection
• /
• v.11 no.3
• /
• pp.123-131
• /
• 2007

The buckling behavior of a fiber reinforced plastic pipe was researched. When a cylindrical structure is made of isotropic material, it shows two dimensional buckled shape which has same deformed section along the longitudinal direction. But an anisotropic cylindrical structure shows three dimensional buckled shape which has different deformed section along the longitudinal direction. Because the modulus of elasticity is varied in a certain direction when ply angles are changed, the strength of a pipe are changed as ply angles are changed. In this study, the limitation of two dimensional and three dimensional buckling mode was investigated and the buckling strength of a laminated composite pipe was evaluated.

• Journal of the Korea institute for structural maintenance and inspection
• /
• v.8 no.2
• /
• pp.169-175
• /
• 2004

In this paper, the stability of cantilever composite laminated structures with open channel section is studied. This paper deals with the buckling behavior under the variation of the geometrical shape (length ratio, crank angle in the open channel section), the fiber reinforced angle, and so on in order to offer a effective and reliable design data. Also, sensitive analyses are carried out on the stability by the interaction of design factors. Based on this fact, the proper channel section and lamination scheme of composite material cantilever structures are considered in the engineering aspect.

• Journal of Korean Society of Steel Construction
• /
• v.12 no.3 s.46
• /
• pp.291-302
• /
• 2000

In recent years the development of high modulus, high strength and low density boron and graphite fibers bonded together has brought renewed interestes in structural elements. When a plate with arbitrarily oriented layers and clamped boundary conditions is subjected to uniform loading, it is difficult to analyze and apply, compared with isotropic and orthotropic cases. Therefore the numerical methods, such as finite difference method or finite element method, should be emloyed to analyse such problems. In this study the finite difference technique is used to formulate the bending analysis of symmetric composite laminated skew plates. When this technique is used to solve the problem, it is desirable to reduce the order of the derivatives in order to minimize the number of the pivotal points involved in each equation. The 4th order partial differential equations of laminated skew plates are converted to an equivalent three of 2nd order partial differential equations with three dependant variables.

• Journal of Korean Association for Spatial Structures
• /
• v.10 no.4
• /
• pp.75-83
• /
• 2010

Laminated composite plates have shown their superiority over metals in applications requiring high specific strength, high specific modulus, and so on. Therefore, they have used in various industry. However, they have poor resistance to impact compared to typical metal materials. So, many researchers have investigated about impact behavior of laminated composite plate. To investigate impact behavior of laminated composite plate, we have to calculate contact force between impactor and laminated composite plate at the first. Impactor's equation of motion, plate's equation of motion and correlations for indentation were solved to know the contact force at the same time. In this study, low velocity impact behavior of composite plate was investigated using the finite element program which is involved the classical Hertzian law, Sun's law and Sun & Yang's experimental law and Sun & Tan's experimental law considering the stacking method.

• Transactions of the Korean Society of Mechanical Engineers A
• /
• v.40 no.12
• /
• pp.1013-1019
• /
• 2016

CFRP is the composite material manufactured by the hybrid resin on the basis of carbon fiber. As this material has the high specific strength and the light weight, it has been widely used at various fields. Particularly, the unidirectional carbon fiber can be applied with the layer angle. CFRP made with layer angle has the strength higher than with no layer angle. In this paper, the property of crack growth due to each layer angle was investigated on the crack propagation and fracture behavior of the CFRP compact tension specimen due to the change of layer angle. The value of maximum stress is shown to be decreased and the crack propagation is slowed down as the layer angle is increased. But the limit according to the layer angle is shown as the stress is increased again from the base point of the layer angle of $60^{\circ}$. This study result is thought to be utilized with the data which verify the probability of fatigue fracture when the defect inside the structure at using CFRP of mechanical structure happens.

• Composites Research
• /
• v.26 no.2
• /
• pp.79-84
• /
• 2013

The prediction and analysis procedure of fatigue damage crack growth life for a stiffener bonded composite laminate panel including center hole and edge notch damage, was studied. It was performed on the basis of fatigue damage growth test results on a laminated skin panel specimens and the analysis results of stress intensity factor for the stiffener bonded composite panel. According to the comparison between experimental test and prediction results of fatigue damage growth life, it was concluded that the residual strength and damage tolerance assessment can be carried out along to the edge notch crack growth.