• Advances in materials Research
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• 제13권5호
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• pp.335-353
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• 2024

In the present paper, a simple quasi-3D integral higher-order beam theory (HBT) is presented, in which both shear deformation and thickness stretching effects are included for mechanical analysis of advanced composite beams with simply supported boundary conditions, handling mainly bending, buckling, and free vibration problems. The kinematics is based on a novel displacement field which includes the undetermined integral terms and the parabolic function is used in terms of thickness coordinate to represent the effect of transverse shear deformation. The governing equilibrium equations are drawn from the dynamic version of the principle of virtual work; whereas the solution of the problem is obtained by assuming a Navier technique for simply supported advanced composite beams subjected to sinusoidally and uniformly distributed loads. The correctness of the present computational method is checked by comparing the obtained numerical results with quasi-3D solutions found in the literature and with those provided by other shear deformation beam theories. It can be confirmed that the proposed model, which does not involve any shear correction factor, is not only accurate but also simple and useful in solving the static and dynamic response of advanced composite beams.

• 대한토목학회논문집
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• 제34권5호
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• pp.1353-1362
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• 2014

최근 화석연료의 과도한 소비로 인해 다양한 환경문제가 발생하고 있으며, 이에 대한 대안으로 신재생에너지의 중요성과 그에 대한 시설의 수요가 꾸준히 증가하고 있다. 이러한 수요를 만족하기 위하여, 다수의 태양광발전 구조물들이 건설, 계획되고 있다. 그러나 대부분의 태양광발전 시설들은 육지에 시공되고 있기 때문에 토지 이용에 따른 건설비의 증가와 토지 개간에 의한 추가적인 환경문제 등이 발생하고 있다. 이러한 문제점을 해결하기 위하여 최근 국내에서는 FRP를 활용한 수상 부유식 태양광발전 구조물에 대한 연구를 지속적으로 수행하고 있다. FRP는 높은 강도와 내부식성 및 작은 단위중량 등의 장점을 가지고 있기 때문에 최근 토목분야에서 각광받고 있으며, 이러한 재료적 특성은 자중에 따라 부력체의 크기가 결정되는 수상 구조물에 특히 유용하다. 이 연구에서는 수상 부유식 태양광발전 구조물과 구조물을 구성하는 SMC FRP 수직재의 구조적 성능을 평가하기 위한 해석적, 실험적 연구를 수행하였다. 수상 부유식 태양광발전 구조물은 유한요소해석을 통해 정적거동을 평가하고, 실험을 통해 동적거동을 평가하였다. 또한 SMC FRP 수직재는 유한요소해석을 통해 구조안전성 및 좌굴안정성을 평가하였으며, 실험을 통해 압축 및 인발 하중에 대한 구조적 거동 특성을 검토하였다. 검토 결과 펄트루젼 FRP (pultruded FRP)와 SMC (Sheet Modoling Compound) FRP로 구성된 구조시스템은 외부하중에 대한 안전성을 확보하고 있음을 확인하였다.

• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2004년도 학술대회지
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• pp.408-413
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• 2004

High speed planning boats also have been required more and more the rational strength analysis and evaluation for the optimal structural design in respect of the structural lightness according to the high speed trend. Even though the suggestion of the simple type equation for the equivalent dynamic pressure is reasonable to design the scantling of ship structure conveniently, many research activities for more reasonable improvement of the simple design pressure, have been continued to suggest the more accurate equivalent static description of tire structural response such as the deflection and stress of hull structure. In this research, we focus on the aluminum bottom stiffened plate structure in which structural scantling is mainly depend on the local loads such as dynamic or impact pressure without other load effects and structural response for the simple dynamic equivalent pressure was investigated through the structural analysis. In order to investigate the structural response of the bottom stiffened plate structure subjected to the dynamic equivalent design pressure, linear and nonlinear structural analysis of the bottom stiffened plate structure of 4.3 ton aluminum planning boat was performed based on the equivalent static applied loads which were derived from the KR regulation and representative one among various dynamic equivalent pressure equations. From above analysis results, we found that the response such as deflection and stress of plate member was similar with the response results of one plate member model with fixed boundary, which was published previous paper and in case of KR design loading, all response of stiffened plate structure were within elastic limit. Through the nonlinear analysis, nearly elastic behavior including the slight geometrical nonlinear response was dominant but plastic local zone was appeared at $85\%$ limit load. Therefore, we can say that through tire linear and nonlinear analysis, this stiffened plate member has no structural strength problem based on the yield criteria in case within $60\%$ limit load except the other strength point of view such as the fatigue and buckling problem.

• Steel and Composite Structures
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• 제21권5호
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• pp.1017-1029
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• 2016

When a welded circular hollow section (CHS) tubular joint is subjected to brace axial loading, failure position is located usually at the weld toe on the chord surface due to the weak flexural stiffness of the thin-walled chord. The failure mode is local yielding or buckling in most cases for a tubular joint subjected to axial load at the brace end. Especially when a cyclic axial load is applied, fracture failure at the weld toe may occur because both high stress concentration and welding residual stress along the brace/chord intersection cause the material in this region to become brittle. To improve the ductility as well as to increase the static strength, a tubular joint can be reinforced by increasing the chord thickness locally near the brace/chord intersection. Both experimental investigation and finite element analysis have been carried out to study the hysteretic behaviour of the reinforced tubular joint. In the experimental study, the hysteretic performance of two full-scale circular tubular T-joints subjected to cyclic load in the axial direction of the brace was investigated. The two specimens include a reinforced specimen by increasing the wall thickness of the chord locally at the brace/chord intersection and a corresponding un-reinforced specimen. The hysteretic loops are obtained from the measured load-displacement curves. Based on the hysteretic curves, it is found that the reinforced specimen is more ductile than the un-reinforced one because no fracture failure is observed after experiencing similar loading cycles. The area enclosed by the hysteretic curves of the reinforced specimen is much bigger, which shows that more energy can be dissipated by the reinforced specimen to indicate the advantage of the reinforcing method in resisting seismic action. Additionally, finite element analysis is carried out to study the effect of the thickness and the length of the reinforced chord segment on the hysteretic behaviour of CHS tubular T-joints. The optimized reinforcing method is recommended for design purposes.

• Advances in aircraft and spacecraft science
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• 제3권4호
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• pp.427-445
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• 2016

Star sensors are the attitude estimation sensors of the satellite orbiting in its path. It gives information to the control station on the earth about where the satellite is heading towards. It captures the images of a predetermined reference star. By comparing this image with that of the one captured from the earth, exact position of the satellite is determined. In the process of imaging, stray lights are eliminated from reaching the optic lens by the mechanical enclosures of the star sensors called Baffles. Research in space domain in the last few years is mainly focused on increased payload capacity and reduction in launch cost. In this paper, a star sensor baffle made of Aluminium is considered for the study. In order to minimize the component weight, material wastage and to improve the structural performance, an alternate material to Aluminium is investigated. Carbon Fiber Reinforced Polymer is found to be a better substitute in this regard. Design optimisation studies are carried out by adopting suitable design modifications like implementing an additional L-shaped flange, Upward flange projections, downward flange projections etc. A better configuration of the baffle, satisfying the design requirements and achieving manufacturing feasibility is attained. Geometrical modeling of the baffle is done by using UNIGRAPHICS-Nx7.5(R). Structural behavior of the baffle is analysed by FE analysis such as normal mode analysis, linear static analysis, and linear buckling analysis using MSC/PATRAN(R), MSC-NASTRAN(R) as the solver to validate the stiffness, strength and stability requirements respectively. Effect of the layup sequence and the fiber orientation angle of the composite layup on the stiffness are also studied.

• 한국항공우주학회지
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• 제31권4호
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• pp.53-59
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• 2003

다목적실용위성(KOMPASA) 태양전지판을 전개하기 위해 사용되는 Strain Energy Hinge(SEH)는 신뢰성 있는 전개를 보장하지만, 태양전지판이 완전 전개되는 순간, 큰 좌굴충격력을 유발하여 위성의 구조적 안정성이나 자세제어에 심각한 영향을 미칠 수 있으므로 전개장치의 설계단계에서부터 동역학적인 평가가 필요하다. 더욱이 위성의 임무가 다양해짐에 따라 태양전지판의 면적이 커지면서 보다 실제적이고 정확한 해석을 위해서는 태양전지판의 탄성변형 효과도 고려되어야 한다. 본 연구에서는 SE H를 이용하여 탄성효과가 큰 태양전지판을 전개할 때 발생하는 동적 특성들을 예측할 수 있도록 동력학 해석절차를 제시하였으며 다목적실용위성 2호의 태양전지판 전개시험을 통하여 해석결과의 신뢰성을 검증하였다.

• Steel and Composite Structures
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• 제36권2호
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• pp.119-141
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• 2020

In this paper, wavy square absorbers were experimentally and numerically investigated. Numerical simulations were performed with LS-Dyna software on 36 wavy absorbers and their crushing properties were extracted and compared with the simple one. The effect of different parameters, including wave height, wave depth, and wave type; either internal or external on the crushing characteristics were also investigated. To experimentally create corrugation to validate the numerical results, a set of steel mandrel and matrix along with press machines were used. Since the initial specimens were brittle, they were subjected to heat treatment and annealing to gain the required ductility for forming with mandrel and matrix. The annealing of aluminum shells resulted in a 76%increase in ultimate strain and a 60% and 56% decrease in yield and ultimate stresses, respectively. The results showed that with increasing half-wave height in wavy square absorbers, the maximum force was first reduced and then increased. It was also found that in the specimen with constant diameter and half-wave depth, an increment in the half-wave height led to an initial increase in efficiency, followed by a decline. According to the conducted investigations, the lowe maximum force can be observed in the specimen with zero half-wave depth as compared to those having a depth of 1 cm.

• 한국지진공학회논문집
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• 제14권2호
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• pp.67-74
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• 2010

비닐하우스 아치구조에 고정햄머 및 이동가속도계 형식을 취한 충격진동실험을 수행하여 획득한 일련의 진동기록으로 부터 고유진동수, 감쇠율 및 모드형태 등과 같은 모달계수를 추출하기 위하여 최신 고급 주파수영역 시스템판별법인 PolyMAX 및 FDD를 적용하였다. 전자는 입력-출력 데이터 모두를 사용하며, 후자는 출력 데이터 만 을 사용한다. 본 연구의 비닐하우스 강재 파이프 아치와 같이 매우 세장한 구조물에 진동계측 등과 같은 비파괴 실험기법을 적용하여 정적좌굴 하중을 결정할 수 있는 지 여부 및 손상을 감지할 수 있는지 등에 대하여 중점적으로 조사하였다. 대체로 추출한 모달계수는 유한요소해석으로부터 획득한 결과와 좋은 일치를 나타냈으며, 지속적으로 수행 할 후속연구에 가능성을 제시하였다.

• 대한조선학회논문집
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• 제38권1호
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• pp.72-85
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• 2001

선박 판부재를 대상으로 중요한 하중경우의 하나인 양축방향 면내하중을 작용시키면서 이중판의 폭, 길이, 두께 및 주판(main plate) 부식 영향 등의 각종 파라메타 영향에 따른 이중판의 정적 강도평가를 주판의 접촉효과를 고려한 탄소성 대변형 비선형 시리즈 구조해석을 수행하였으며 이들 해석 결과로부터 각 파라메타의 변화에 따른 강성과 강도 특성을 분석하였다. 또한 이중판의 보강 효과가 최소한 새판으로 치환 보수한 평판 강도 수준으로 설계되어야 하므로 이를 손쉽게 파악할 수 있게 이중판으로 보강된 판부재를 등가 평판 두께로 환산할 수 있는 간이 평가식을 개발하였다. 이 개발식을 이용하여 각 이중판 설계의 영향인자 변화에 따른 등가 평판두께의 증감 정도를 파악하고 이로부터 적어도 새판으로 보수한 평판강도에 달할 수 있게 양축방향 면내 압축하중을 받는 이중판의 설계지침을 제시하였다. 마지막으로, 개발된 등가 평판 도출식은 고정밀 좌굴강도 평가식과 서로 일정한 상관관계가 있음을 확인하고 관계식을 정립하였다. 이 관계식을 각 경우별로 축적하여 앞으로 일일이 구조해석을 수행하지 않고도 설계된 이중판 강도를 등가 평판두께로 제시할 수 있는 간이 추정식의 개발에 이용될 수 있을 것으로 사료된다.

• 대한기계학회논문집A
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• 제25권2호
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• pp.250-263
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• 2001

The up and down speed of heddle frames that produce woven cloth by insertion of weft yarns between warp yarns has been increased recently much for productivity improvement, which induces higher inertial stresses and vibrations in the heddle frame. the heddle frame is required to reduce its mass because the heddle frame contributes the major portion of the stresses in the heddle frames during accelerating and decelerating. Conventional aluminum heddle frames have fatigue life of around 5 months at 550rpm due to their low fatigue flexural strength as well as low bending stiffness. In this work, since carbon/epoxy composite materials have high specific fatigue strength(S/p), high specific modulus(E/p), high damping capacity and sandwich construction results in lower deflections and higher buckling resistance, the sandwich structure composed of carbon/epoxy composite skins and polyurethane foam were employed for the high-speed heddle frame. The design map for the sandwich beams was accomplished to determine the optimum thickness and the stacking sequences for the heddle frames. Also the effects of the number of ribs on the stress of the heddle frame were investigated by FEM analyses. Finally, the high-speed heddle frames were manufactured with sandwich structures and the static and dynamic properties of the aluminum and the composite heddle frames were tested and compared with each other.