• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 춘계학술대회논문집
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• pp.877-882
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• 2005

Dynamic stability of an axially accelerating beam stucture is investigated in this paper. The equations of motion of a fixed-free beam are derived using the hybrid deformation variable method and the assumed mode method. Unstable regions due to periodical acceleration are obtained by using the Floquet's theory. Stability diagrams are presented to illustrate the influence of the dimensionless acceleration, amplitude, and frequency. Also, buckling occurs when the acceleration exceeds a certain value. It is found that relatively targe unstable regions exist around the first bending natural frequency, twice the first bending natural frequency, and twice the second bending natural frequency. The validity of the stability diagram is confirmed by direct numerical integration of the equations of motion.

• 한국소음진동공학회논문집
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• 제15권9호
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• pp.1053-1059
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• 2005

Dynamic stability of an axially accelerating beam structure is investigated in this paper. The equations of motion of a fixed-free beam are derived using the hybrid deformation variable method and the assumed mode method. Unstable regions due to periodical acceleration are obtained by using the Floquet's theory. Stability diagrams are presented to illustrate the influence of the dimensionless acceleration, amplitude, and frequency. Also, buckling occurs when the acceleration exceeds a certain value. It is found that relatively large unstable regions exist around the first bending natural frequency, twice the first bending natural frequency, and twice the second bending natural frequency. The validity of the stability diagram is confirmed by direct numerical integration of the equations of motion.

• Coupled systems mechanics
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• 제13권2호
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• pp.95-113
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• 2024

In this paper, we will analyse the thermo-elastic behavior of the plate element of a structure arranged in a climatically aggressive environment (extreme temperature), we use a refined four-variable thick plate theory to take the shear effect into consideration, the proposed theory less computationally expensive and more accurate so that it incorporates the shear effect into the formulation. The plate is assumed to be simply supported on its four edges, so exact (closed-form) solutions are found according to the Navier expansion, and the governing stability equations and associated boundary conditions of the problem are obtained via the virtual works principle. The plate studied ismade of laminated composite materials, so a parametric study is needed to see the effect of different types of parameters and coupling on the critical temperature value causing thermo-elastic instability of the plate and also on the natural frequency of free vibration, as well as for other parameters such as anisotropy, slenderness and aspect ratio of the plate and finally the lamination angle. Numerical results are obtained for specially orthotropic and antisymmetrical plates and are compared with those obtained by othertheoriesin the literature to validate the analysis approach used.

• 대한토목학회논문집
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• 제26권1A호
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• pp.191-203
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• 2006

가정 변형률 9절점 쉘 요소를 이용하여 스티프너로 보강된 적층 복합 보강판의 진동 특성을 연구하였다. 기존의 연구결과들과 비교하기 위하여 대칭으로 적층된 carbon-epoxy 복합재료 적층 판을 사용하였다. 또한 본 연구에서 스티프너를 쉘로 모델링 한 결과들은 보 요소로 모델링 된 결과들과 비교하였다. 비틀림에 약한 스티프너의 경우에 국부 좌굴이 스티프너에서 발생할 수 있다. 이 경우에 스티프너는 쉘로 모델링 하여야 한다. 본 연구는 면내 압축 및 전단하중을 받는 적층 복합 보강 판과 보강되지 않은 적층 복합 판의 연구에 집중되어 있다. 면내 압축 및 전단하중은 적층복합 판의 고유진동수와 진동 모우드를 변화시키고 압축 하중의 증가는 압축 하중이 임계 좌굴하중에 도달하여 진동수가 0 이 될 때 까지 진동수를 감소시킨다. 면내 전단하중의 작용은 그렇지 않은 경우에 비하여 진동수를 증가시켰다. 또한 진동수와 면내 하중 관계 곡선의 교차는 적층 복합 보강판의 진동 모우드를 교체 시킨다. 본 연구에서 제시한 쉘 요소로 적층 복합 보강판을 해석한 결과 참고문헌과 비교하여 매우 정확한 결과를 나타내었다. 그러므로 보강된 적층 복합 판의 면내 전단 및 압축하중의 종류와 크기는 특정한 진동수와 모우드 형상의 조절을 위해 적절하게 선택되어야 한다. 고유치 문제를 풀기 위하여 Lanzcos 방법을 사용하였다.

• 소음진동
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• 제10권6호
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• pp.1075-1082
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• 2000

본 논문은 이중 탄성기초 위에 놓인 테이퍼진 티모센코 보의 진동과 동적 안정성에 대한 연구로써, 이중 탄성기초는 지반모델에서 흔히 이용되는 분포 Winkler 스프링들과 전단기초층으로 구성된다. 보의 전단변형과 회전관성이 고려되고, 지배방정식은 Halmilton원리를 이용한 에너지 표현식에 의해 유도된다. 고유진동수와 좌굴하중을 구하기 위해 관계되는 고유치 문제를 풀며, 출력을 받는 보의 진동에 대한 수치해석결과들이 제시되는 다른 방법을 사용한 유용한 해의 결과들과 비교된다. 출력을 받고 탄성기초 위에 놓인 테이퍼진 티모센코 보의 고유진동수, 모드 형상, 그리고 임계하중 값들이 다양한 테이퍼 두께의 비, 전단기초 파라미터, Winkler 기초파라미터, 경계조건의 변화에 대해 조사된다.

• Advances in nano research
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• 제7권1호
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• pp.39-49
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• 2019

This paper focuses on two main objectives. The first one is to exploit an energy equivalent model and finite element method to evaluate the equivalent Young's modulus of single walled carbon nanotubes (SWCNTs) at any orientation angle by using tensile test. The calculated Young's modulus is validated with published experimental results. The second target is to exploit the finite element simulation to investigate mechanical buckling and natural frequencies of SWCNTs. Energy equivalent model is presented to describe the atomic bonding interactions and their chemical energy with mechanical structural energies. A Program of Nanotube modeler is used to generate a geometry of SWCNTs structure by defining its chirality angle, overall length of nanotube and bond length between two adjacent nodes. SWCNTs are simulated as a frame like structure; the bonds between each two neighboring atoms are treated as isotropic beam members with a uniform circular cross section. Carbon bonds is simulated as a beam and the atoms as nodes. A finite element model using 3D beam elements is built under the environment of ANSYS MAPDL environment to simulate a tensile test and characterize equivalent Young's modulus of whole CNT structure. Numerical results are presented to show critical buckling loads, axial and transverse natural frequencies of SWCNTs with different orientation angles and lengths. The understanding of mechanical behaviors of CNTs are essential in developing such structures due to their great potential in wide range of engineering applications.

• Steel and Composite Structures
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• 제27권6호
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• pp.761-775
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• 2018

In the present work, the recently developed non-polynomial shear deformation theories are assessed for thermo-mechanical response characteristics of laminated composite plates. The applicability and accuracy of these theories for static, buckling and free vibration responses were ascertained in the recent past by several authors. However, the assessment of these theories for thermo-mechanical analysis of the laminated composite structures is still to be ascertained. The response characteristics are investigated in linear and non-linear thermal gradient and also in the presence and absence of mechanical transverse loads. The laminated composite plates are modelled using recently developed six shear deformation theories involving different shear strain functions. The principle of virtual work is used to develop the governing system of equations. The Navier type closed form solution is adopted to yield the exact solution of the developed equation for simply supported cross ply laminated plates. The thermo-mechanical response characteristics due to these six different theories are obtained and compared with the existing results.

• Journal of Mechanical Science and Technology
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• 제17권1호
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• pp.85-96
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• 2003

In the present investigation, the nonlinear dynamic buckling of a curved plate subjected to sinusoidal loading is examined. By the theoretical analyses, a highly nonlinear snap-through motion of a clamped-free-clamped-free plate and its effect on the overall vibration response are investigated. The problem is reduced to that of a single degree of freedom system with the Rayleigh-Ritz procedure. The resulting nonlinear governing equation is solved using Runge-Kutta (RK-4) numerical integration method. The snap-through boundaries, which vary with different damping coefficient and linear circular frequency of the flat plate are studied and given in terms of force and displacement. The relationships between static and dynamic responses at the start of a snap-through motion are also predicted. The analysis brings out various characteristic features of the phenomenon, i.e. 1) small oscillation about the buckled position-softening spring type motion, 2) chaotic motion of intermittent snap-through, and 3) large oscillation of continuous snap-through motion crossing the two buckled positions-hardening spring type. The responses of buckled plate were found to be greatly affected by the snap-through motion. Therefore, better understanding of the snap-through motion is needed to predict the full dynamic response of a curved plate.

• 한국강구조학회 논문집
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• 제19권4호
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• pp.367-381
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• 2007

전력 수요의 증가로 인해 송전철탑의 고용량, 대용량화가 요구되어왔지만 아직 대부분을 차지하고 있는 345kV급 송전철탑에 대한 연구는 미흡한 실정이다. 현재 해석 설계되고 있는 방식은 2차원 트러스요소를 사용하여 양단은 힌지접합으로 축력만 작용하고 있는 것으로 가정한다. 이러한 방식을 3차원 트러스 요소에 적용하였을 때, 면 외로 작용하는 하중에 대해 무한변위가 발생하는 구조해석적인 문제점을 가지고 있다. 이에 본 연구는 보다 합리적인 요소 선택을 통한 구조해석 방식을 제안하기 위해 기존의 3차원 트러스요소 모델, 보요소 모델, 주주재와 수평재는 보요소로 모사하고 사재 및 기타 복재는 트러스로 모사한 보-트러스요소 모델 등 세 모델을 실제 설계 시공된 345kV급 송전철탑에 대해 설계하중 내에서 구조해석프로그램을 이용한 정적해석, 자유진동해석, 선형좌굴해석을 수행하였다. 구조해석 결과, 세 모델 모두 축력 및 축응력, 변위에서는 큰 차이가 나타나지 않았으나 보요소모델과 보-트러스요소 모델에서 휨응력의 비율이 축응력에 대해 크게 나타났다. 자유진동해석과 탄성좌굴해석의 결과를 통해 보-트러스요소 모델이 송전철탑 설계 및 해석에 있어서 더 안전측으로 고려될 수 있음을 확인하였다.

• International Journal of Aerospace System Engineering
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• 제3권1호
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• pp.10-16
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• 2016

A trigonometric Layerwise higher order shear deformation theory (TLHSDT) is developed and implemented for free vibration and buckling analysis of laminated composite and sandwich plates by analytical and finite element formulation. The present model assumes parabolic variation of out-plane stresses through the depth of the plate and also accomplish the zero transverse shear stresses over the surface of the plate. Thus a need of shear correction factor is obviated. The present zigzag model able to meet the transverse shear stress continuity and zigzag form of in-plane displacement continuity at the plate interfaces. Hence, botheration of shear correction coefficient is neglected. In the case of analytical method, the governing differential equation and boundary conditions are obtained from the principle of virtual work. For the finite element formulation, an efficient eight noded $C^0$ continuous isoparametric serendipity element is established and employed to examine the dynamic analysis. Like FSDT, the considered mathematical model possesses similar number of variables and which decides the present models computationally more effective. Several numerical predictions are carried out and results are compared with those of other existing numerical approaches.