• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2001년도 춘계학술대회논문집
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• pp.133-137
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• 2001

Active control of flexural vibrations of smart laminated composite beams has been carried out using piezoceramic sensor/actuator and viscoelastic material. The beams with passive constrained-layer damping have been analyzed by formulating the equations of motion through the use of extended Hamilton's principle. The dynamic characteristics such as damping ratio and modal damping of the beam are calculated for various fiber orientations by means of iterative complex eigensolution method, This paper addresses a design strategy of laminated composite under flexural vibrations to design structure with maximum possible damping capacity.

• 한국안전학회지
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• 제19권1호
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• pp.94-101
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• 2004

In this study, composite laminated conical shells with ring stiffeners are analyzed. A versatile 4-node shell element which is useful for the analysis of conical shell structures is used. An improved flat shell element is established by the combined use of the addition of non-conforming displacement modes and the substitute shear strain fields. The proposed element has six degrees of freedom per node and permits an easy connection to other types(beam element) of Optimum location and optimum section properties of ring stiffeners are obtained. It is shown that the thickness of conical shell is reduced about 20% by optimum ring stiffeners.

• Structural Engineering and Mechanics
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• 제42권5호
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• pp.729-745
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• 2012

This study presents dynamic analysis of laminated beams traversed by moving loads using a multilayered beam element based on the first-order shear deformation theory. The present element consists of N layers with different thickness and material property, and has (3N + 7) degrees of freedom corresponding three axial, four transversal, and 3N rotational displacements. Delamination and interfacial slip are not allowed. Comparisons with analytical and/or numerical results available in literature for some illustrative examples are made. Numerical results for natural frequencies, deflections and stresses of laminated beams are given to explain the effect of load speed, lamina layup, and boundary conditions.

• 대한기계학회논문집A
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• 제30권4호
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• pp.409-419
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• 2006

The actuating performance of plate-type unimorph piezoelectric composite actuators having various stacking sequences was evaluated by three dimensional finite element analysis on the basis of thermal analogy model. Thermal residual stress distribution at each layer in an asymmetrically laminated plate with PZT ceramic layer and thermally induced dome height were predicted using classical laminated plate theory. Thermal analogy model was applied to a bimorph cantilever beam and LIPCA-C2 actuator in order to confirm its validity. Finite element analysis considering thermal residual deformation showed that the bending behavior of piezoelectric composite actuator subjected to electric loads was significantly different according to the stacking sequence, thickness of constituent PZT ceramic and boundary conditions. In particular, the increase of thickness of PZT ceramic led to the increase of the bending stiffness of piezoelectric composite actuator but it did not always lead to the decrease of actuation distance according to the stacking sequences of piezoelectric composite actuator. Therefore, it is noted that the actuating performance of unimorph piezoelectric composite actuator is rather affected by bending stiffness than actuation distance.

• 한국강구조학회 논문집
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• 제13권3호
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• pp.233-244
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• 2001

본 연구에서는 다층 층간분리된 복합보의 휨강성 감소를 고찰하였다. 휨강성 감소를 평가하기 위해서 이론해석을 수행하였다. 층간분리가 복합보에 휨강성 감소에 주는 영향을 고찰하기 위해서 지배운동방정식이 유도되었고, 층간분리된 각각의 분할보는 연속조건을 이용한 반복관계를 이용하여 구해졌다. 복합적층보에 층간분리가 여러 층에서 발생한 경우에 대해 다양한 적층순서와 여러 가지 형태의 층간분리 형상으로 모델링하여 결과를 비교하였다. 다층 층간분리가 존재하는 적층복합보의 휨강성을 평가하는데 있어서 본 연구는 유용하게 활용될 수 있다.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2002년도 봄 학술발표회 논문집
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• pp.489-496
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• 2002

The lateral buckling of a laminated composite beam is studied. A general analytical model applicable to the lateral buckling of a composite beam subjected to various types of loadings is derived. This model is based on the classical lamination theory, and accounts for the material coupling for arbitrary laminate stacking sequence configuration and various boundary conditions. The effects of the location of applied loading on the buckling capacity are also included in the analysis. A displace-based one-dimensional finite element model is developed to predict critical loads and corresponding buckling modes for a thin-walled composite beam with arbitrary boundary conditions. Numerical results are obtained for thin-walled composites under central point load, uniformly distributed load, and pure bending with angle-ply and laminates. The effects of fiber orientation location of applied load, and types of loads on the critical buckling loads are parametrically studied.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2008년도 춘계 학술발표회 제20권1호
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• pp.233-236
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• 2008

구조재로서 목재는 자연에서 쉽게 얻을 수 있는 재료로서 뛰어난 미관, 가공성 등으로 인해 전통가옥이나 사찰 등에 널리 사용되어져 왔지만, 콘크리트나 강재에 비해 연소와 부식의 우려 등 내구성에 문제를 가지고 있다. 따라서, 목재를 구조부재로 활용하기 위해서는 타 재료와의 하이브리드화가 필요하다. 따라서, 본 연구에서는 구조용집성재보(100${\times}$200${\times}$3000(mm)), 콘크리트슬래브(800${\times}$100${\times}$3000(mm), fck=21MPa) 및 전단연결재(볼트, 래그스크류)로 구성된 합성보의 탄소성거동을 평가하기 위하여 구조 실험을 수행하였다. 실험결과, 전단연결재의 종류와 간격에 무관하게 항복비(항복내력/최대내력)가 크고, 항복 후에는 바로 취성파괴로 연계되었다. 따라서, 이러한 취성파괴를 방지할 수 있는 휨보강(철근, 섬유쉬트 등)이 필요할 것으로 판단된다. 또한, 전단연결재 배치간격이 좁을수록 합성효과가 우수하여 사용성이 뛰어나기 때문에 경제적 설계와 재료의 효율적 사용이 가능할 것으로 판단된다.

• 한국건축시공학회지
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• 제24권3호
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• pp.331-341
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• 2024

본 연구에서는 구조용 집성재 보의 휨강도 및 연성능력을 보완하고자 강재-목재 합성보의 휨성능을 평가하였다. 실험체는 구조용 집성재 보 1식과 강재-목재 합성보 2식으로 구성하였다. 강재-목재 합성보는 부착 방법에 따라 액상형 접착제와 나사못을 사용하여 휨성능을 평가하였다. 실험결과, 강재-목재 합성보는 구조용 집성재 보에 비하여 구조성능이 약 2~3배 높아 휨강도 및 연성능력이 충분히 확보된 것으로 나타났다. 또한, 액상형 접착제를 사용한 경우가 나사못을 적용한 실험체에 비하여 우수한 구조성능을 보여주었다.

• Steel and Composite Structures
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• 제26권4호
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• pp.453-461
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• 2018

In this paper, nonlinear vibrations of the unsymmetrical laminated composite beam (LCB) on a nonlinear elastic foundation are studied. The governing equation of the problem is derived by using Galerkin method. Two different end conditions are considered: the simple-simple and the clamped-clamped one. The Hamiltonian Approach (HA) method is adopted and applied for solving of the equation of motion. The advantage of the suggested method is that it does not need any linearization of the problem and the obtained approximate solution has a high accuracy. The method is used for frequency calculation. The frequency of the nonlinear system is compared with the frequency of the linear system. The influence of the parameters of the foundation nonlinearity on the frequency of vibration is considered. The differential equation of vibration is solved also numerically. The analytical and numerical results are compared and is concluded that the difference is negligible. In the paper the new method for error estimation of the analytical solution in comparison to the exact one is developed. The method is based on comparison of the calculation energy and the exact energy of the system. For certain numerical data the accuracy of the approximate frequency of vibration is determined by applying of the suggested method of error estimation. Finally, it has been indicated that the proposed Hamiltonian Approach gives enough accurate result.

• Steel and Composite Structures
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• 제34권2호
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• pp.241-260
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• 2020

This article presented a comprehensive model to study static buckling stability and associated mode-shapes of higher shear deformation theories of sandwich laminated composite beam under the compression of varying axial load function. Four higher order shear deformation beam theories are considered in formulation and analysis. So, the model can consider the influence of both thick and thin beams without needing to shear correction factor. The compression force can be described through axial direction by uniform constant, linear and parabolic distribution functions. The Hamilton's principle is exploited to derive equilibrium governing equations of unified sandwich laminated beams. The governing equilibrium differential equations are transformed to algebraic system of equations by using numerical differential quadrature method (DQM). The system of equations is solved as an eigenvalue problem to get critical buckling loads and their corresponding mode-shapes. The stability of DQM in determining of buckling loads of sandwich structure is performed. The validation studies are achieved and the obtained results are matched with those. Parametric studies are presented to figure out effects of in-plane load type, sandwich thickness, fiber orientation and boundary conditions on buckling loads and mode-shapes. The present model is important in designing process of aircraft, naval structural components, and naval structural when non-uniform in-plane compressive loading is dominated.