• 복합신소재구조학회 논문집
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• 제5권4호
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• pp.11-17
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• 2014

A progressive failure analysis procedure for composite laminates is completed in here. An anisotropic plastic constitutive model for fiber-reinforced composite material is implemented into computer program for a predictive analysis procedure of composite laminates. Also, in order to describe material behavior beyond the initial yield, the anisotropic work-hardening model and subsequent yield surface are implemented into a computer code, which is Predictive Analysis for Composite Structures (PACS). The accuracy and efficiency of the anisotropic plastic constitutive model and the computer program PACS are verified by solving a number of various fiber-reinforced composite laminates with and without geometric discontinuity. The comparisons of the numerical results to the experimental and other numerical results available in the literature indicate the validity and efficiency of the developed model.

• Smart Structures and Systems
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• 제4권1호
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• pp.19-34
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• 2008

Nowadays developments in the field of laminated composite structures with piezoelectric have attracted significant attention of researchers due to their wide range of applications in engineering such as sensors, actuators, vibration suppression, shape control, noise attenuation and precision positioning. Due to large number of parameters associated with its manufacturing and fabrication, composite structures with piezoelectric display a considerable amount of uncertainty in their material properties. The present work investigates the effect of the uncertainty on the free vibration response of piezoelectric laminated composite plate. The lamina material properties have been modeled as independent random variables for accurate prediction of the system behavior. System equations have been derived using higher order shear deformation theory. A finite element method in conjunction with Monte Carlo simulation is employed to obtain the secondorder statistics of the natural frequencies. Typical results are presented for all edges simply supported piezoelectric laminated composite plates to show the influence of scattering in material properties on the second order statistics of the natural frequencies. The results have been compared with those available in literature.

• 복합신소재구조학회지
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• 제2권2호
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• pp.48-50
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• 2011

• 항공우주시스템공학회지
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• 제17권2호
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• pp.71-77
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• 2023

액상성형공정(LCM, Liquid Composite Molding) 은 복합재료 오토클레이브(Autoclave) 성형공정의 단점을 극복할 수 있는 탈 오토클레이브(OoA, Out of Autoclave) 공정의 하나로 매우 복잡한 형상이나 대형 구조물을 일체형으로 만들 수 있어 항공산업에서 큰 경쟁력을 가진 공법으로 알려져 있다. 이러한 장점 때문에 액상성형공정을 적용한 항공 부품제작 수요가 늘고 있으며 FAA에서는 액상성형공정을 적용한 복합재료에 대한 인증(Qualification) 방법을 제시한 바 있다. 국내에서도 액상성형공정 적용 복합재료에 대한 부품제작 수요 및 재료인증 수요가 꾸준히 제기되고 있다. 따라서 본 연구에서는 기존에 구축된 프리프레그 복합재료 인증방안 이외에 LCM 공정을 적용한 복합재료에 대한 인증방안을 수립하기 위한 연구를 진행하였다.

• 한국자동차공학회논문집
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• 제5권4호
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• pp.48-69
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• 1997

The use of advanced composite materials in many engineering structures has steadily increased during the last decade. Advanced composite materials allow the design engineer to tailor the directional stiffness and the strength of materials as required for the structures. Design variables to the design engineer include multiple material systems. ply orientation, ply thickness, stacking sequence and boundary conditions, in addition to overall structural design parameters. Since the vibration and impact strength of composite cylindrical shell is an important consideration for composite structures design, the reliable prediction method and design methodology should be required. In this study, the optimum design of composite cylindrical shell for maximum natural frequency, buckling strength and impact strength are developed by analytic and numerical method. The effect of parameters such as the various composite material orthotropic properties (CFRP, GFRP, KFRP, Al-CFRP hybrid), the stacking sequences, the shell thickness, and the boundary conditions on structural characteristics are studied extensively.

• Steel and Composite Structures
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• 제19권6호
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• pp.1501-1510
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• 2015

The frequency selective surface (FSS) embedded hybrid composite materials have been developed to provide excellent mechanical and specific electromagnetic properties. Radar absorbing structures (RASs) are an example material that provides both radar absorbing properties and structural characteristics. The absorbing efficiency of an RAS can be improved using selected materials having special absorptive properties and structural characteristics and can be in the form of multi-layers or have a certain stacking sequence. However, residual stresses occur in FSS embedded composite structures after co-curing due to a mismatch between the coefficients of thermal expansion of the FSS and the composite material. In this study, to develop an RAS, the thermal residual stresses of FSS embedded composite structures were analyzed using finite element analysis, considering the effect of stacking sequence of composite laminates with square loop (SL) and double square loop (DSL) FSS patterns. The FSS radar absorbing efficiency was measured in the K-band frequency range of 21.6 GHz. Residual stress leads to a change in the deformation of the FSS pattern. Using these results, the effect of transmission characteristics with respect to the deformation on FSS pattern was analyzed using an FSS Simulator.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2004년도 춘계학술발표대회 논문집
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• pp.288-291
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• 2004

The characteristics of the buckling analysis module for stiffened composite structures were studied in this paper. Composite stiffened structures have geometrical asymmetry and material properties asymmetry. Due to these reason, postbuckling analysis was essential and the characteristics of postbuckling analysis modules for ABAQUS were researched. Static analysis module was considered. By considering the material nonlinearity, progressive failure mechanism was applied and buckling strength was estimated

• 복합신소재구조학회 논문집
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• 제1권4호
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• pp.6-12
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• 2010

This study investigates how to apply composite material to the blast loading protection devices, mainly used for military purpose. Traditionally, earth-filled blast walls have been used for protecting important parts of military facilities and personnels. However these types of blast walls show difficulty in fabrication and portability because of their nature of heavy weight. Composite materials are known to have relatively higher specific stiffness and strength than any other metallic and earth-filled materials such as sand and gravels. Totally 4 times of TNT blast experiments were performed on the carbon/epoxy blast walls. After the end of each test, the improvement of blast wall was implemented to the structure. The test results show that the use of composite material in the blast protecting area is the one of very effective and reliable alternatives.

• Steel and Composite Structures
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• 제18권5호
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• pp.1161-1176
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• 2015

The connection between a column and a beam is of particular importance to ensure the safety of civil engineering structures, such as high-rise buildings and bridges. While the connector must bear sufficient force for load transmission, increase of its ductility, toughness and damping may greatly enhance the overall safety of the structures. In this work, a composite beam-column connector is proposed and analyzed with the finite element method, including effects of elasticity, linear viscoelasticity, plasticity, as well as geometric nonlinearity. The composite connector consists of three parts: (1) soft steel; (2) polymer; and (3) conventional steel to be connected to beam and column. It is found that even in the linear range, the energy dissipation capacity of the composite connector is largely enhanced by the polymer material. Since the soft steel exhibits low yield stress and high ductility, hence under large deformation the soft steel has the plastic deformation to give rise to unique energy dissipation. With suitable geometric design, the connector may be tuned to exhibit different strengths and energy dissipation capabilities for real-world applications.

• 한국방재학회 논문집
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• 제4권2호
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• pp.35-45
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• 2004

최근 항공기, 자동차 등에 사용되어왔던 복합재료가 그 사용 영역을 넓혀 교량 상판, 상하수도용 관로 등에 적용되고 있다. 이러한 복합재료의 주요 장점은 고강도, 경량성, 그리고 뛰어난 내부식성으로 기존의 재료에 비해 많은 장점을 갖고 있으나, 이러한 재료의 정확한 특성 파악 및 이를 사용한 구족물의 거동의 정확한 분석의 어려움으로 복합재료의 적용이 활발히 이루어지지 못하고 있는 실정이며, 이러한 요인이 복합재료를 토목구조물에 적용하는데 가장 큰 제한요소로 작용해 왔다. 본 연구에서는 복합재료 구조물의 해석을 위한 사전 연구로서, 현재 국내에서 사용되고 있는 GFRP 관로에 대한 재료특성 실험을 수행하여, 각각의 구성 적층재료별 재료 특성 및 전체 적층판에 대한 재료특성을 제공한다.