• Journal of the Computational Structural Engineering Institute of Korea
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• v.14 no.3
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• pp.299-308
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• 2001

This paper presents the three-dimensional (3-D) study of the natural vibration of cantilevered laminated composite plates. The Ritz method is used to obtain stationary values of the associated Lagrangian functional with displacements approximated by mathematically complete polynomials satisfying the boundary conditions at the clamped edge exactly. The accuracy of the 3-D model is established through a convergence study of non-dimensional frequencies followed by a comparison of the converged 3-D solutions with analytical and experimental findings in the existing literature. A wide scope of 3-D frequency results explain the influence of a number of geometrical and material parameters for cantilevered laminated plates, namely aspect ratio (a/b), width-to-thickness ratio (a/h), orthotropy of material, number of plies (NP), fiber orientation angle(θ), and stacking sequence.

• Journal of the Earthquake Engineering Society of Korea
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• v.8 no.2
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• pp.63-72
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• 2004

The purpose of this study is to evaluate seismic performance of reinforced concrete bridge piers supported by laminated rubber bearings. A computer program, named RCAHEST(Reinforced Concrete Analysis in Higher Evaluation System Technology), for the analysis of reinforced concrete structures was used. Material nonlinearity is taken into account by comprising tensile, compressive and shear models of cracked concrete and a model of reinforcing steel. The smeared crack approach is incorporated. Seismic isolator element is developed to predict behaviors of laminated rubber bearings. The proposed numerical method for seismic performance evaluation of reinforced concrete bridge piers supported by laminated rubber bearings is verified by comparison with reliable experimental results.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.25 no.4
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• pp.293-300
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• 2012

In this study, the delamination analysis has been implemented to investigate the initiation and propagation of crack in composite laminates composed of orthotropic materials. A simple modeling was achieved by moving nodal technique without re-meshing work when crack propagation occurred. This paper aims at achieving two specific objectives. The first is to suggest a very simple modeling scheme compared with those applied to conventional h-FEM based models. To verify the performance of the proposed model, analysis of double cantilever beams with composite materials was implemented and then the results were compared with reference values in literatures. The second one is to investigate the behavior of interior delamination problems using the proposed model. To complete these objectives, the full-discrete-layer model based on Lobatto shape functions was considered and energy release rates were calculated using three-dimensional VCCT(virtual crack closure technique) based on linear elastic fracture mechanics.

• Composites Research
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• v.36 no.1
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• pp.48-52
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• 2023

Fiber-reinforced composites have anisotropic material properties, so the mechanical properties of composite structures can vary depending on the stacking sequence. Therefore, it is essential to design the proper stacking sequence of composite structures according to the functional requirements. However, depending on the manufacturing condition or the shape of the structure, there are many cases where the designed stacking angle is out of range, which can affect structural performance. Accordingly, it is important to analyze the stacking angle in order to confirm that the composite structure is correctly fabricated as designed. In this study, the stacking angle was predicted from real cross-sectional images of fiber-reinforced composites using convolutional neural network (CNN)-based deep learning. Carbon fiber-reinforced composite specimens with several stacking angles were fabricated and their cross-sections were photographed on a micro-scale using an optical microscope. The training was performed for a CNN-based deep learning model using the cross-sectional image data of the composite specimens. As a result, the stacking angle can be predicted from the actual cross-sectional image of the fiber-reinforced composite with high accuracy.

• Proceedings of the Korean Vacuum Society Conference
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• 2015.08a
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• pp.212.1-212.1
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• 2015

본 연구에서는 용액 공정을 통해 제작한 IGZO 박막 트랜지스터의 Active layer를 적층 구조로 쌓아올리고, 신뢰성 평가를 위해 Gate에 지속적인 바이어스를 인가함으로써 소자의 문턱 전압 변화를 측정 실험을 진행하였다. Active layer 제작에 사용된 용액의 비율은 In:Zn:Ga = 1:1:30%로 제작되었고, 단일층부터 이중, 삼중층까지 적층을 하였다. 각 소자의 Active layer 층이 많아질수록 이동도가 1.21, 0.87, 0.69 ($cm^2/Vs$)으로 감소하는 등의 전기적 특성이 감소하는 경향을 보였다. 하지만 Gate에 10 V를 3000초간 지속적으로 인가해주었을 때 문턱 전압의 변화가 단일층일 때 10.4 V에서 삼중층일 때 1.3 V로 감소하였다. 이것은 Active layer의 층 사이의 계면이 형성되면서 current path에 영향을 주어 전기적 특성이 감소하였지만, 적층으로 인한 surface의 uniformity가 향상되는 것으로 확인하였다. 또한 1500초에서 Dit (Interface Trap Density)를 추출한 결과, 단일층에서는 $7.53{\times}10^{12}$($cm^{-2}-1$<)로 삼중층에서 $4.52{\times}10^{12}$($cm^{-2}-1$<)의 약 두 배 정도 높게 추출되었다.

• Transactions of Materials Processing
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• v.14 no.7 s.79
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• pp.587-594
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• 2005

분무성형공정은 급냉응고 및 결정입자 제어에 따른 고품위 소재 개발의 장점과 함께 고밀도 near-net-shape 제품의 제조가 가능한 합금제조기술이다 분무성형체의 미세조직은 적층표면에 도달하는 액적들의 평균 열용량, 즉 고상분율에 의하여 결정되며, 이는 액적의 비행과정에서의 분사가스-액적간의 열전달과 적층표면에서의 열유입과 열유출 속도에 영향을 받는다. 실제 다양한 공정변수들이 복합적으로 미세조직 형성과정에 영향을 미치지만, 균일한 미세조직을 얻기 위하여서는 적층표면에서의 온도와 고상분율을 항상 일정하게 제어하여야만 한다 즉, 적층표면 온도를 분무 성형공정중에 지속적으로 측정하여 이를 공정 제어 시스템에 feedback하여 원하는 적층표면온도를 유지하도록 공정변수를 제어하는 것이 필수적이다. 분무성형에 제조된 성형체는 합금원소의 편석이 없고 미세한 등방성의 결정립으로 이루어진 특징적인 미세조직을 나타낸다 이와 같은 미세조직으로 인하여 분무성형체는 우수한 성형성과 기계가공성을 나타내며, 또한 분무성형-후속가공된 최종 제품은 잉곳주조에 의하여 제조된 것과 비교하여 크게 향상된 기계적 성질을 가진다.

• Proceedings of the Korean Society of Disaster Information Conference
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• 2016.11a
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• pp.188-189
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• 2016

본 논문은 초기하중을 하중을 받는 역대칭 angle-ply 와 cross-ply 적층판의 좌굴 및 진동특성을 무재하시의 고유진동수를 이용하여 산정하는 간편법을 제시하였다. 마주보는 두변이 단순 지지된 역대칭 적층판의 운동방정식은 전단변형과 회전강성효과를 고려한 YSN 이론으로 유도하였으며 이를 선점법을 이용하여 해석하였다. 초기응력을 받는 적층판의 무차원화 고유진동수, 임계좌굴계수 및 동적 주 불안정영역 문제들을 무재하시의 무차원화 고유진동수로서 각각의 특성을 정립시켰다. 본 연구에서 제안한 진동특성에 관한 간편산정식의 정당성과 사용성을 입증하기 위하여 수치예들로서 검토하였다.

• Journal of the Earthquake Engineering Society of Korea
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• v.1 no.2
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• pp.79-89
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• 1997

The objective of this paper is to investigate the mechanical characteristics of the laminated rubber bearings (LRBs) for the seismic isolation. The evaluations of the proposed equations of the LRB horizontal stiffness are carried out and these equations are extended to the visco-elastic problems to investigate the damping amplifications of LRBs. The stability evaluation of LRBs is also performed. For investigation of the dynamic characteristics of LRBs, the horizontal stiffness equations of the LRBs considering the P-delta effects are applied to the modeling of a seismically isolated structure and the earthquake response time history analyses are carried out. From this research, the proposed simple equation of the horizontal stiffness of LRB is so useful for the design loads and easily extended to the visco-elastic problems. Through the stability evaluation of LRB, the increasing ratio of the total rubber thickness of the LRB severely decrecises the bucking load than the increasing ratio of unit rubber thickness. From the comparison of the dynamic shear deflection of LRB, the analysis results are in good agreement with those of the experiments.

• Journal of the Korea Convergence Society
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• v.8 no.7
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• pp.219-224
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• 2017

This paper investigates equivalent stress and deformation happening at inner fiber structure when the tensile force acts on the specimen with arch type composed of carbon fiber. The countless many each fiber is applied on the unidirectional axis at CFRP and has the high specific strength and stiffness by comparing with iron. In this study, the distribution of stress due to radius is investigated at the structure of arch type composed with the optimum stacking angle of $60^{\circ}$. And the durability is seen to be lower as the radius increases at the same stacking angle. By applying the result of this study to the design of structure with arch type, it can be devoted to the safe design for the prevention of damage and the durabilty improvement. And it is possible to be grafted onto the convergence technique at the designed factor and show the esthetic sense.

• Journal of the Korean Society for Nondestructive Testing
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• v.23 no.3
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• pp.237-245
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• 2003

Since the velocity is dependent on the fiber orientation in anisotropic composites, the application of traditional acoustic emission (AE) source location techniques based on the constant velocity to composite structures has been practically impossible. The anisotropy makes the source location procedure complicated and deteriorates the accuracy of the location. In this study, we have divided the region of interest(ROI) into a set of finite elements, taken each element as a virtual source, and calculated the arrival time differences between sensors by using the velocities at every degree from 0 to 90. The calculated and the experimentally measured values of the arrival time difference aye then compared to minimize the location error. The results from two different materials, namely AA6061-T6 and CFRP(uni-directional; UD, $[0]_{32}4$) laminate confirmed the practical usefulness of the proposed method.