• 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.

• Earthquakes and Structures
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• 제9권2호
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• pp.415-430
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• 2015

Integral abutment bridges have many advantages over bridges with expansion joints in terms of economy and maintenance costs. However, in the design of abutments of integral bridges temperature loads play a crucial role. In addition, seismic loads are readily transferred to the substructure and affect the design of these components significantly. Currently, the European and American bridge design codes consider these two load cases separately in their recommended design load combinations. In this paper, the importance and necessity of combining the thermal and seismic loads is investigated for integral bridges. A 2D finite element combined pile-soil-structure interactive model is used in this evaluation. Nonlinear behavior is assumed for near field soil behind the abutments. The soil around the piles is modeled by nonlinear springs based on p-y curves. The uniform temperature changes occurring at the time of some significant earthquakes around the world are gathered and applied simultaneously with the corresponding earthquake time history ground motions. By comparing the results of these analyses to prescribed AASHTO LRFD load combinations it is observed that pile forces and abutment stresses are affected by this new load combination. This effect is more severe for contraction mode which is caused by negative uniform temperature changes.

• 한국초전도저온공학회:학술대회논문집
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• 한국초전도저온공학회 2003년도 추계학술대회 논문집
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• pp.313-315
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• 2003

The heat loads invaded from the environment to several parts of superconduct cable cooling system were measured by liquid boiloff calorimetry. The measuring system was verified by the measurement to a uniform heat loads. The heat loads by the tubes for relief and pressure gauges were greater than the estimated.

• 소음진동
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• 제4권4호
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• pp.451-457
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• 1994

A numerical method is presented to obtain natural frequencies and mode shapes of uniform elastic beams with static deflections due to dead loads. The differential equation governing the free vibration of beam taken into account the static deflection due to deal loads is derived and solved numerically. The hinged-hinged, clamped-clamped and clamped-hinged end constraints are applied in the numerical examples. As the numerical results, the lowest three nondimensional frequency parameters are reported as functions of nondimensional system parameters; the load parameters, and the slenderness rations. And some typical mode shapes of free vibrations are also presented in figures.

• Earthquakes and Structures
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• 제1권4호
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• pp.411-425
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• 2010

The effect of dead loads on dynamic responses of uniform elastic beams is examined by means of a governing equation which takes into account initial bending stress due to dead loads. First, the governing equation of beams which includes the effect of dead loads is briefly presented from the author's paper (Takabatake 1990). In the formulation the effect of dead loads is considered by strain energy produced by conservative initial stresses produced by the dead loads. Second, the effect of dead loads on dynamical responses produced by live loads in simply supported beams and clamped beams is confirmed by the results of numerical computations with the Galerkin method and Wilson-${\theta}$ method. It is shown that the dynamical responses, like dynamic deflections and bending moments produced by dynamic live loads, are decreased in a heavyweight beam when the effect of dead loads is included. Third, an approximate solution for dynamic deflections including the effect of dead loads is presented in closed-form. The proposed solution shows good in agreement with results of numerical computations with the Galerkin method and Wilson-${\theta}$ method. Finally, a method reflecting the effect of dead loads for dynamic responses of beams on the magnitude of live loads is presented by an example.

• 대한토목학회논문집
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• 제11권4호
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• pp.55-66
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• 1991

본 논문에서는 교량의 합리적인 설계하중결정과 설계기준을 유도하기 위한 연구를 수행하였다. 현행의 설계기준은 하중과 부재저항의 불확실성을 합리적으로 고려하지 못하고 있어 교량의 지간길이에 따라 안전도 수준이 서로 다르게 나타나고 있다. 따라서, 본 논문에서는 교량의 일반적인 지간길이에 따라 일정한 안전도수준을 갖을 수 있는 교량의 합리적인 설계하중과 설계기준을 유도하여 제시하였다. 본 연구에서 제시한 설계하중은 우리나라 도로상의 실제 통행차량 조사자료에 근거하였으며, 이에 따른 설계기준도 진보된 개념의 하중-저항계수형식으로 유도하였다. 또한, 통행량증가에 따른 영향을 고려하기 위하여 통행량에 따른 활하중계수를 유도하였다. 본 논문에서 유도된 설계하중과 설계기준은 교량의 지간길이에 따라 일정한 안전도로수준을 나타내고 있으며, 활하중 증가에 따른 영향을 합리적으로 고려하고 있어 앞으로 우리나라 도로설계기준에 유용한 자료를 제공할 것으로 사료된다.

• 한국항공우주학회지
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• 제46권2호
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• pp.106-113
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• 2018

발사체 발사 시 제트화염에 의해 발생하는 강력한 음향파는 음향하중의 형태로 비행체를 가진한다. 대표적인 경험적 음향하중 예측기법인 DSM-II(Distributed Source Method-II)는 제트화염 축을 따라 소음원을 배치하는 방법으로 계산비용 및 정확성 측면에서 장점을 갖는다. 하지만 소음원 배치 방법의 한계로 인해 다양한 발사대 환경을 정확하게 반영하기에는 한계가 있다. 본 연구에서는 넙스(Non-Uniform Rational B-Spline, NURBS) 곡선 모델링을 경험적 예측기법에 도입하여 자유롭게 소음원을 배치할 수 있는 음향하중 예측기법에 대한 연구를 수행하였다. 넙스 기법이 새롭게 도입된 해석기법의 검증을 위하여 Epsilon 로켓의 곡선형 저소음 발사대 형상에 대한 음향하중 예측을 수행하였고 해석 결과를 기존의 예측방법 및 실험 결과와 비교하였다.

• Steel and Composite Structures
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• 제21권1호
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• pp.37-55
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• 2016

In this study, the influence of centrally placed circular and square cutouts on vibration and buckling characteristics of different ply-oriented laminated panels under the action of compressive and/or tensile types of non-uniform in-plane edge loads are investigated. The panels are inspected under the action of uniaxial compression, uniaxial tension and biaxial, compression-tension, loading configurations. Furthermore, the effects of different degrees of edge restraints and panel aspect ratios are also addressed in this work. Towards this, a nine-node heterosis plate element has been adopted which includes the effect of shear deformation and rotary inertia. According to the results, the tensile buckling loads are higher than that of compressive buckling loads. However, the tensile buckling load continuously reduces with the increased cutout sizes irrespective of ply-orientations. This is also true for compressive buckling loads except for some particular ply-orientations with higher sized cutouts.

• Structural Engineering and Mechanics
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• 제48권2호
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• pp.195-205
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• 2013

The buckling problem of linearly tapered micro-columns is investigated on the basis of modified strain gradient elasticity theory. Bernoulli-Euler beam theory is used to model the non-uniform micro column. Rayleigh-Ritz solution method is utilized to obtain the critical buckling loads of the tapered cantilever micro-columns for different taper ratios. Some comparative results for the cases of rectangular and circular cross-sections are presented in graphical and tabular form to show the differences between the results obtained by modified strain gradient elasticity theory and those achieved by modified couple stress and classical theories. From the results, it is observed that the differences between critical buckling loads achieved by classical and those predicted by non-classical theories are considerable for smaller values of the ratio of the micro-column thickness (or diameter) at its bottom end to the additional material length scale parameters and the differences also increase due to increasing of the taper ratio.

• Advances in Computational Design
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• 제5권4호
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• pp.349-362
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• 2020

Dynamic characteristics of a scale-dependent porous metal foam cylindrical shell under a traveling load have been explored within this article based on a numerical approach. Within the material texture of the metal foams, uniform and non-uniform porosities may be dispersed. Based upon differential quadrature method (DQM) and Laplace transforms, the equations of motion for a shear deformable scale-dependent shell may be solved numerically. Scale-dependent shell modeling has been provided based upon strain gradient elasticity. Solving the equations will give the shell deflection as a function of load speed. Also, it is reported that shell deflection relies on the porosity dispersion and strain gradient influences.