• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1999년도 가을 학술발표회 논문집
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• pp.309-316
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• 1999

Laminated composite plates are very useful in various fields of engineering where high strength-to-weight and stiffness-to-weight ratios are required. Design optimization of composite structures has gained importance in recent years as the engineering applications of fiber reinforced materials have increased and weight savings has become an essential design objective. However, due to the anisotropic material properties of laminated composite structure it is very difficult to analyze and design. In this study, numerical optimization technique together with the finite element method is used to find the optimum design of FRP. Various combination of fiber orientation for the laminate layers are investigated and several local optimum solutions are found.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2000년도 추계학술발표대회 논문집
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• pp.173-176
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• 2000

Finite element model based on the Naghdi's shell theory in the general tensor-based form is formulated in the present study. Partial mixed variational functional for assumed strain is formulated in order to avoid the severe locking troubles known as transverse shear and membrane locking. The proposed assumed strain element in general tensor Naghdi's shell model provides very accurate solutions for thin shells in benchmark problems. In additions, linear elastic constitutive equations are given in the general curvilinear coordinate system including anisotropic layered structures. Thus laminated composited shell structures are easily analyzed in the present formulation.

• 한국안전학회지
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• 제31권3호
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• pp.16-21
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• 2016

Carbon Fiber Reinforced Plastic(CFRP) composite with a higher specific strength and rigidity is more excellent than conventional metallic materials or other organic polymer of FRP. It has been widely used in vehicles, aerospaces and high technology industries which are associated with nuclear power fields. However, CFRP laminated composite has several disadvantages as like a delamination, matrix brittleness and anisotropic fibers that are the weak points of the crack initiation. In this present work, the reinforced silicon carbide(SiC) particles were added to the interlayer of CFRP laminates in order to mitigate the physical vulnerability affecting the cracking and breaking of the matrix in the CFRP laminated composite because of excellent specific strength and thermal shock resistance characteristics of SiC. The 1wt% of SiC particles were spread into the CFRP prepreg by using a spray coating method. After that, CFRP prepregs were laminated for the specimen. Also, the twill woven type CFRP prepreg was used because it has excellent workability. Thus the mechanical and fracture behaviors of the twill woven CFRP laminated composite reinforced with SiC particles were investigated with the acoustic emission(AE) method under a fracture test. The results show that the SiC particles enhance the mechanical and fracture characteristics of the twill CFRP laminate composite.

• 폴리머
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• 제26권1호
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• pp.105-112
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• 2002

연구는 electro-active polymer(EAP)의 특성을 가지는 ion-exchange polymer metal composite(IPMC)을 이용하여 지능형 대장내시경 개발에 목적을 두고 있다. IPMC는 낮은 구동전압과 빠른 반응속도로 인하여 매우 매력적인 물질이다. 본 연구에서는 IPMC구동기의 전극을 무전의 도금 방법을 이용하여 용액함침-환원방법(impregnation-reduction method)으로 제조하였으며 코팅된 백금전극의 횟수에 따라 변위와 변화를 측정하였다. 구동특성을 알아보기 위하여 길이, 주파수에 대한 변위, 힘을 측정하였으며, 주파수 대역은 저주파 대역과 공명주파수 대역을 사용하는 것이 적합하다는 결론을 얻었다. 또한 다양한 구동적 특성과 수분의 함량에 따른 영향에 대해 고전적 적층 이론 (classical laminate theory, CLT)을 이용하여 이방성 IPMC의 응력분포와 수분이동에 따른 모멘트, 변형률, 곡률(cuvature)을 모델링 하였다.

• 한국강구조학회 논문집
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• 제10권1호통권34호
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• pp.11-24
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• 1998

복합샌드위치평판은 복합재료를 갖으면서 강성이 있는 얇은 면재와 저밀도인 두꺼운 심재로 구성되어 있다. 본 연구에서는 국부전단변형을 고려한 복합면재를 갖는 샌드위치평판을 해석을 위한 지배방정식을 유도하였고, 해석적인 방법으로 해석을 하였다. 해석방법의 타당성을 확인하기 위하여 전체 전단변형을 고려한 일반 적층판 이론의 값과 비교하였다. 그리고 복합면재와 심재의 국부전단변형을 고려하였으므로 일반 적층판 해석에도 적용시킬 수 있음을 보였다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 1997년도 춘계학술대회논문집; 경주코오롱호텔; 22-23 May 1997
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• pp.687-694
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• 1997

The anisotropy and shape of distributed piezopolymer actuator have advantages over isotropic piezo ceramic materials, since these features of PVDF can be utilized as another design variable in control application. This study is interested in the reduction of sound transmission through elastic plate into interior space by using the PVDF actuator. The plate-cavity system is adopted as a test problem. The vibration of composite plate and the sound fields through plate are analyzed by using the coupled finite element and boundary element method. Some numerical simulations are performed on sound transmission through elastic plates. To investigate the effects of anisotropy and shape of distributed piezopolymer actuator, various kinds of distributed PVDF actuators are applied in sound control simulation for isotropic and anisotropic plates. The PVDF actuators applied are different from each other in their shapes and laminate angles. The results of control simulation show that the control effectiveness of distributed PYDF actuator can be enhanced by using the coupling between shape of actuator and vibration modes of structure and the anisotropy of piezoelectric properties of PVDF.

• 한국자동차공학회논문집
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• 제17권3호
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• pp.15-21
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• 2009

The anisotropic mechanical properties were measured for the three orthogonal orientations of plain weave glass fabric reinforced epoxy resin laminate. In tensile and flexural tests, axial and edge type specimens failed by pull-out of warp and fill yarns, respectively. In contrast, the thickness type specimens failed by adhesive failure process. Longitudinal cracking occurred in several of the edge type specimens during tensile test. That cracking caused pop-in in the stress-strain curve. Defects induced by improper coupon machining caused that cracking.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 추계학술대회논문집A
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• pp.516-521
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• 2000

Most of studies, using ESPI method, have handled tension, thermal and vibration analysis, and is limited to isotropic materials. However, tension and vibration simultaneously are loaded in real structure. Also, almost study using ESPI method is locally limited to the analysis on the isotropic materials and a few studies on the anisotropic materials have reported. Existing methods, such as the accelerometer method and FEA method, to analyze vibration have some disadvantages. Using the accelerometer method that is generally used to analyze vibration phenomena, it is impossible to analyze vibration on the oscillating body and one can observe no vibration mode shape during experiment. In case of the FEA method, it is difficult to define boundary conditions correctly if the shape of a body tested is complex, and one can just obtain vibration mode shapes on the peak amplitude in each modes. In this study, plane plate of stainless steel(STS304), isotropic material, that is used as structural steel is analyzed about vibration characteristics under tension. Also, in the study of stainless steel, the characteristics of composite material(AS4/PEEK) used as high strength structural material in aircraft is evaluated about vibration under tension, and studies the effect of tension on vibration.

• Structural Engineering and Mechanics
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• 제7권2호
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• pp.181-202
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• 1999

Dynamic response of axisymmetric arbitrary laminated composite cylindrical shell of finite length, using three-dimensional elasticity equations are studied. The shell is simply supported at both ends. The highly coupled partial differential equations are reduced to ordinary differential equations (ODE) with variable coefficients by means of trigonometric function expansion in axial direction. For cylindrical shell under dynamic load, the resulting differential equations are solved by Galerkin finite element method, In this solution, the continuity conditions between any two layer is satisfied. It is found that the difference between elasticity solution (ES) and higher order shear deformation theory (HSD) become higher for a symmetric laminations than their unsymmetric counterpart. That is due to the effect of bending-streching coupling. It is also found that due to the discontinuity of inplane stresses at the interface of the laminate, the slope of transverse normal and shear stresses aren't continuous across the interface. For free vibration analysis, through dividing each layer into thin laminas, the variable coefficients in ODE become constants and the resulting equations can be solved exactly. It is shown that the natural frequency of symmetric angle-ply are generally higher than their antisymmetric counterpart. Also the results are in good agreement with similar results found in literatures.

• 대한기계학회논문집A
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• 제37권2호
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• pp.265-270
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• 2013

본 논문에서는 Tsai-Wu 파손이론을 적용하여 복합재료 자전거 프레임의 경량화를 위한 강도설계에 대하여 연구하였다. 설계에 있어서 자전거 프레임의 경량화는 중요한 문제이며, 동시에 요구 강도를 만족시켜야 한다. 하중조건으로 유럽표준위원회의 EN14764 규격에 의거하여 페달, 수직, 레벨 하중조건을 적용하였다. 복합재료는 이방성을 가지므로 적절한 적층수 및 적층 순서를 결정하는 것이 중요하다. 따라서 $[0]_{8n}$, $[90]_{8n}$, $[0/90]_{2ns}$, $[{\pm}45]_{2ns}$, $[0/{\pm}45/90]_{ns}$ 의 적층에 대하여 적층수를 변화시켜가며(n=1,2,3,4) 연구를 수행하였다. 연구 결과로부터 하중 조건에 따른 자전거 프레임의 취약부와 취약적층을 확인하였고, $[0/{\pm}45/90]_{3s}$ 이 가장 적절한 적층각 모델임을 제안하였다.