Earticle

Considering the management problem for Internet of Things, existing IP-based network management protocols such as Simple Network Management Protocol (SNMP) and the Network Configuration (NETCONF) protocol may possibly be utilized to manage smart objects (the main components in Internet of Things). Based on the thinking of extension indicated by some network management standardizations, this paper tries to introduce Extenics into the study on management of smart objects. This paper proposes a simplified formalization for management of smart objects based on the extension model, and formalizes information, knowledge and policy related to Manager, Agent and Management Information Base (MIB) for management of smart objects by making use of basic-elements, composite-elements, extension transformations, dependent functions and extension sets. The case study of this paper shows that, the proposed formalized framework of Manager, Agent and MIB in the form of information-knowledge-policy for management of smart objects based on the extension model is feasible.

This paper presents the simplified welding distortion analysis method to predict the welding deformation of both plate and stiffener in fillet welds. Currently, the methods based on equivalent thermal strain like Strain as Direct Boundary (SDB) has been widely used due to effective prediction of welding deformation. Regarding the fillet welding, however, those methods cannot represent deformation of both members at once since the temperature degree of freedom is shared at the intersection nodes in both members. In this paper, we propose new approach to simulate deformation of both members. The method can simulate fillet weld deformations by employing composite shell element and using different thermal expansion coefficients according to thickness direction with fixed temperature at intersection nodes. For verification purpose, we compare of result from experiments, 3D thermo elastic plastic analysis, SDB method and proposed method. Compared of experiments results, the proposed method can effectively predict welding deformation for fillet welds.

This paper presents a closed-form higher-order analysis of interfacial shear stresses in RC continuous beams strengthened with bonded prestressed laminates. For retrofitting reinforced concrete continuous beams is to bond fiber reinforced prestressed composite plates to their tensile faces. An important failure mode of such plated beams is the debonding of the composite plates from the concrete due to high level of stress concentration in the adhesive at the ends of the composite plate. The model is based on equilibrium and deformations compatibility requirements in and all parts of the strengthened beam, where both the shear and normal stresses are assumed to be invariant across the adhesive layer thickness. In the present theoretical analysis, the adherend shear deformations are taken into account by assuming a parabolic shear stress through the thickness of both the RC continuous beams strengthened with bonded prestressed laminates. The theoretical predictions are compared with other existing solutions. A parametric study has been conducted to investigate the sensitivity of interface behavior to parameters such as laminate stiffness and the thickness of the laminate where all were found to have a marked effect on the magnitude of maximum shear and normal stress in the composite member.

본 연구는 일반적인 적층 복합재료의 구조요소에서 탄성영역에 대한 해석적 해에 대한 방법을 나타낸 것이다. 혼합된 경계조건 하에서 2차원 평면응력탄성문제는 변위포텐셜함수라 불리는 단일미지함수로 표현된 1/4 부분미분방정식의 해로 축소시켰으며, 응력과 변위의 모든 성분은 어떠한 경계조건에도 적합한 방법을 만드는 동일한 변위포텐셜항으로 표현하였다. 이 방법은 각도를 가진 적층판과 90도 적층판으로 각각 구성된 구조요소의 두 가지 특별문제에 대해서 해석적인 해를 얻는데 적용된다. 본 연구에서 나타낸 몇 가지 수치적인 결과는 두 가지로 적층된 유리섬유복합재료에 관한 것이다. 연구결과는 지지된 하중의 임계영역에서 모든 경계조건이 정확히 만족되어 크게 신뢰할 만한 결과를 나타내었다. 이는 혼합된 어떠한 경계조건하에서도 복합재료의 구조요소에서 탄성영역에 대한 정확한 해석적 해를 얻는 데 적용시킬 수 있을 뿐 아니라 단순한 문제를 해결하는 데도 신뢰할 만한 결과를 얻을 수 있음을 입증한 것이다.

The present study describes a method for analytical solution to elastic field in structural elements of general symmetric laminated composite materials. The two dimensional plane stress elasticity problems under mixed boundary conditions are reduced to the solution of a single fourth order partial differential equation, expressed in terms of a single unknown function, called displacement potential function. In addition, all the components of stress and displacement are expressed in terms of the same displacement potential function, which makes the method suitable for any boundary conditions. The method is applied to obtain analytical solutions to two particular problems of structural elements consisting of an angle-ply laminate and a cross-ply laminate, respectively. Some numerical results are presented for both the problems with reference to the glass/epoxy composite. The results are highly accurate and reliable as all the boundary conditions including those in the critical regions of supports and loads are satisfied exactly. This verifies the method as a simple and reliable one as well as capable to obtain exact analytical solution to elastic field in structural elements of composite materials under mixed and any other boundary conditions.

This paper deals with a fully coupled piezoelectric-mechanical assumed strain solid element that can be used for geometric and material nonlinear modeling of thin piezoelectric actuators. Since the assumed strain solid element can alleviate locking, the element is suitable for performance analysis of very thin actuators without locking. A finite element code is developed based on the finite element formulation and validated by solving typical numerical examples such as bimorph and unimorph beams. Using thecode, we have conducted performance analysis for LIPCA actuator. The estimated actuation displacement of LIPCA agrees well with experimental data under low prescribed voltage.

최근 자동차 인터랙션 시스템은 자동차 산업과 정 보화 기술이 끊임없이 융합하여 발전하는 산물이다. 계속 발전하고 있는 자동차 인터랙션 기술을 보면 자 동차 인터페이스는 이론 연구 측면에서든 실제적인 응용 측면에서든 유례가 없는 발전 활력이 있는 것을 알 수 있다. 하지만 이 영역의 발전에 대한 연구는 실 증적인 연구가 아직 없는 상황이다. 또한 디자인에서 자동차 인터페이스의 디자인 연구를 깊게 연구하고 자동차 인터페이스 연구의 공백을 매운다. 본 연구의 목적은 운전자와 승차인으로 하여금 초 강력한 선호도, 초고도의 인지도, 이어서 초강력한 사 용의도를 느끼게 하기 위하여 자동차 VR 인터페이스 디자인 요소를 고려하고 이러한 활용된 디자인 요소 가 운전자와 승차인의 선호도와 인지도, 그리고 사용 의도에 어떠한 영향을 미치는지에 대해 융합적 연구 활동을 하고자 한다. 따라서 본 논문은 VR 인터랙션 기술을 활용한 자동- 338 차 인터페이스를 사용해본 적이 있는 소비자들을 대상 으로 연구를 시도하였다. 총 450부의 설문지를 배포하였 다. 최종적으로 총 389부의 유효 설문지를 대상으로 통 계분석을 실시하였다. 실증분석을 위해 SPSS V. 22.0과 AMOS V. 22.0 통계패키지를 이용하여 빈도분석, 신뢰 도분석, 탐색적 요인분석, 확인적 요인분석, 구조방정식 모형 등 분석기법을 이용하였고 분석을 실시하였다. 연구결과 및 내용은 다음과 같다. 첫째 자동차 VR 인터페이스 디자인 요소가 소비자선호도에 긍정적인 영향을 미칠 것이라는 가설은 부분적으로 채택되었다. 둘째, 자동차 VR 인터페이스 디자인 요소가 소비자 인지도에 긍정적인 영향을 미칠 것이라는 가설은 부 분적으로 채택되었다. 셋째 소비자의 선호도와 인지도 가 소비자의 사용의도에 긍정적인 영향을 미친다는 결과를 나타났다. 이러한 연구결과를 바탕으로 연구의 시사점, 한계점 및 향후 연구방향을 제시하였다.

The automobile interaction system is the result of the continuous integration and development of the automotive industry and the information technology. In the face of the continuous innovation of automotive interaction technology, the interface of automotive interaction system has shown unprecedented vitality in the theoretical research and the practical application. However, the status of the development and research in this field is still short of a systematic exposition. In the perspective of design, this paper profoundly explores the development, design, application and research of the interface of automotive interaction system, which fills the research gap. The purpose of this study is to consider the VR interaction interface visual design factor in order to make the rider feel an intense sense of preference, ultrahigh awareness, and then intense use intention. This study explores how visual design factors affect the preference, recognition, and intention of the driver and rider. Therefore, this study selected consumers who have used automotive interface using VR interaction technology and distributed a total of 450 questionnaires. Finally, a total of 389 valid questionnaires were analyzed statistically. For empirical analysis, SPSS V. 22.0 and AMOS V. 22.0 was used. Finally, frequency analysis, exploratory factor analysis, reliability analysis, correlation analysis, and regression analysis were performed. The results of the empirical analysis of this study are as follows. First, the hypothesis that the VR interaction interface visual design factor will positively influence consumer preference was partially adopted. Then, the hypothesis that the visual design elements of the automobile VR interaction interface will have a positive effect on consumer awareness was partially adopted. Finally, consumers 'preference and awareness have a positive effect on consumers' intention to use. Based on these results, we expected implications, limitations, and future direction of the research process.

강화재의 복잡한 배열로 인하여 복합재 구조에 대한 유한요소 모델링은 상당히 까다로운 문제가 될 수 있다. 본 논문에서는 복합재 구조에 대하여 효율적으로 주기 격자망을 생성시킬 수 있는 기법을 제안한다. 먼저 육면체 유한요소로 구성된 규칙적인 격자망을 준비하고, 이를 복합재 내의 강화재에 대한 표면 정보에 맞추어 깎아낸다. 강화재와 기지재 사이에서 깎여진 육면체 유한요소는 임의의 절점과 면을 가질 수 있는 다면체 유한요소에 해당한다. 일관된 알고리즘을 이용하여 육면체 유한요소를 깎아내기 때문에 강화재와 기지재 사이의 요소는 자동적으로 적합한 형태로 구성된다. 또한 대표체적영역 내에서 강화재의 주기성을 추가적으로 고려하면, 대표체적영역에 대한 각각의 주기 경계 쌍에서 절점과 요소의 형태가 모두 일치하는 주기 격자망을 효율적으로 생성시킬 수 있다. 그러므로 별도의 처리 없이 대표체적영역에 주기 경계조건을 부여할 수 있다. 수치예제에서는 본 논문에서 제안한 기법의 효용성을 검증한다.

Finite element modeling of composite structures may be cumbersome due to complex distributions of reinforcements. In this paper, an efficient scheme is proposed that can generate periodic meshes for the composite structures. Regular meshes with hexahedral finite elements are first prepared, and the elements are then trimmed to fit external surfaces of reinforcements in the composite structures. The trimmed hexahedral finite elements located at interfaces between the matrix and the reinforcements correspond to polyhedral finite elements, which allow an arbitrary number of nodes and faces in the elements. Because the trimming process is consistently conducted by means of consistent algorithms, the elements of the reinforcements are automatically compatible with those of the matrices. With the additional consideration of periodicity of reinforcements in a representative volume element(RVE), the proposed scheme provides periodic meshes in an efficient manner, which are compatible for each pair of periodic boundaries of the RVE. Therefore, periodic boundary conditions for the RVE are enforced straightforwardly. Numerical examples demonstrate the effectiveness of the proposed scheme for finite element modeling of complex composite structures.

This study prepared fabric-heating elements of carbon nanofiber composite to characterize morphologies and electrical properties. Carbon nanofiber composite was prepared with 15wt% PVDF-HFP/acetone solution, and 0, 1, 2, 4, 8, and 16wt% carbon nanofiber. Dispersion of solution was conducted with stirring for a week, sonification for 24 hours, and storage for a month, until coating. Carbon nanofiber composite coated fabrics were prepared by knife-edge coating on nylon fabrics with a thickness of 0.1mm. The morphologies of carbon nanofiber composite coated fabrics were measured by FE-SEM. Surface resistance was determined by KS K0555 and worksurface tester. A heating-pad clamping device connected to a variable AC/DC power supply was used for the electric heating characteristics of the samples and multi-layer fabrics. An infrared camera applied voltages to samples while maintaining a certain distance from fabric surfaces. The results of morphologies indicated that the CNF content increased specifically to the visibility and presence of carbon nanofiber. The surface resistance test results revealed that an increased CNF content improved the performance of coated fabrics. The results of electric heating properties, surface temperatures and current of 16wt% carbon nanofiber composite coated fabrics were $80^{\circ}C$ and 0.35A in the application of a 20V current. Carbon nanofiber composite coated fabrics have excellent electrical characteristics as fabric-heating elements.

The stiffness of 6-node isotropic element is stiffer than that of 8-node isotropic element of same configuration. This phenomenon was called 'Relative Stiffness Stiffening Phenomenon'. In this paper, an equation of sampling point modification which correct this phenomenon was derived for the composite plate, as well as an equation for an isotropic plate. The relative stiffness stiffening phenomena of an isotropic plate element could be corrected by modifying Gauss sampling points in the numerical integration of stiffness matrix. This technique could also be successfully applied to the static analyses of composite plate modeled by the 3-dimensional 16-node elements. We predicted theoretical errors of stiffness versus the number of layers that result from the reduction of numerical integration order. These errors coincide very well with the actual errors of stiffness. Therefore, we can choose full integration of reduced integration based upon the permissible error criterion and the number of layers by using the thoretically predicted error.

Composite materials are consist of two or more different materials to produce desirable properties for structural strength. Because of their superiority in strength, corrosion resistance, and weight reduction, they are used extensively as structural members. The objective of this study is to present the effectivness of the laminated composite elements by analyzing in-plane displacement and stress of the anisotropic laminated annular elements. Anisotropic laminated structures are very difficult to analyze and apply, compared with isotropic and orthotropic cases for arbitrary boundaries and fiber angle -ply. Boundary conditions for the examples used in this study consist of two opposite edges clamped and the other two edges free, and finite difference method is used in this study for numerical analysis. From the numerical result, it is found that the program used in this study can be used to obtain the displacement of the straight beams considering it's transverse shear deformation as well as anisotropic laminated elements. Several numerical examples show the advantages of the stiffness increase when the angle-ply composite materials are used. Therefore it gives a guide in deciding how to make use of fiber's angle for the subtended angle, load cases, and boundary conditions.

본 논문에서는 고인성 시멘트 복합체(ECC)가 적용된 날개벽 요소의 면 접합방식에 따른 평가를 실시하였다. 또한 비내진상세를 갖는 RC 골조에 ECC날개벽 요소 보강하여 보강 유무에 따른 내진성능평가를 실시하였다. 면 접합 방법에 따른 거동 특성을 비교하기 위하여 2면 접합은 상 하부 보에 3면 접합은 상 하부 보 및 기둥에 접합하여 실험을 실시 하였다. 또한 비내진상세를 갖는 기존 구조체와의 일체로 거동하는 합성거동을 위해 3면 접합 방식으로 ECC날개벽 요소 보강을 실시하였다. ECC날개벽 요소 실험과 골조 실험은 점증되는 층간변위에 따라 2회씩 반복가력하여 실험을 진행하였다. 실험 결과 ECC 날개벽 요소 실험체의 경우 3면 접합이 2면 접합보다 우수한 내진성능 나타내었다. 각각의 실험체는 우수한 재료 특성으로 인하여 미세한 다수의 균열이 ECC날개벽 요소 전면에 폭넓게 분포하였다. 또한 보통 콘크리트와 달리 최대강도 이후 연성적인 거동을 나타내었으며, 이에 우수한 에너지소산능력을 나타내었다. ECC날개벽 요소를 보강한 실험체와 기존 골조에서는 ECC날개벽 요소 보강에 따른 최대강도 이후 연성적인 거동을 나타내었다. 이에 따라 에너지소산능력이 증가하였으며, 강성저하 또한 완만한 곡선을 나타내며 기존 골조보다 우수한 내진특성을 나타내었다. 이에 ECC 날개벽 요소의 보강이 비내진상세를 갖는 구조체에 우수한 내진 특성을 부여하는 판단된다.

This study was conducted to experimentally investigate the seismic retrofitting performance of non-ductile reinforced concrete (RC) frames by introducing engineered cementitious composite (ECC) wing panel elements. Non-ductile RC frame tested in this study were designed and detailed for gravity loads with insufficient or no consideration to lateral loads. Therefore, Non-ductile RC frame were not satisfied on present seismic code requirements. The precast ECC wing panels were used to improve the seismic structural performance of existing non-ductile RC frame. A series of experiments were carried out to evaluate the structural performance of ECC wing panel elements alone a non-ductile RC frame strengthened by adding ECC panel elements. Failure pattern, strength, stiffness and energy dissipation characteristics of specimens were evaluated based on the test results. The test results show that both lateral strength and stiffness were significantly improved in specimen strengthened than non-ductile RC frame. It is noted that ECC wing wall elements application on non-ductile RC frame can be effective alternative on seismic retrofit of non-ductile building.

본 논문에서는 섬유강화복합재의 멀티스케일 해석을 위해 필요한 대규모/소규모 통계적 체적요소 모델을 개발하였다. 미시영역모델의 크기효과를 최소화하기 위해서 섬유를 최대한 포함한 거대모델을 구성하였다. 이를 위해 국부 영역의 요소 절단법을 이용하여 전체 유한요소 크기에 상관없이 신속한 격자 섬유/기지의 모델링이 가능한 요소생성기를 구성하였다. 이를 통해 대규모 통계 체적 모델을 도출하여 체적모델의 크기에 따른 국부하중 공유의 차이를 고찰하고, 섬유방향의 연속체손상역학모델을 BSVEs 모델 해석으로부터 도출 하였다. BSVEs 모델을 보편적인 RVE모델과 비교 검증하였다.

In this paper, statistical volume element modeling method was developed for multi-scale progressive failure analysis of fiber reinforced composite materials. Big-size statistical volume elements (BSVEs) was considered to minimize the size effect in the micro-scale, by including as many fibers as possible. For that purpose, a mesh cutting method is suggested and adapted into the fiber model generator that creates finite element domain rapidly. The fiber defect model was also developed based on the experimental distribution of the fiber strength. The size effects from the local load sharing (LLS) are evaluated by increasing the fiber inclusion in the micro-scale model. Finally, continuum damage mechanics (CDM) model to the fiber direction was extracted from numerical analysis on BSVEs. And it was compared with strength prediction from typical representative volume element (RVE) model.

A modified 16-node element for composite plate has been proposed and compared with the 20-node element to check the validity of it. The fields of numerical inspection include mode analysis and specific damping analysis. By symetrizing the conventional unsymmetric damping matrix in the analysis of specific damping capacity, we could compute the specific damping capacity and make a program, effectively. In addition, we could predict the errors caused by reduction of integration order in thickness direction depending upon the number of layers.