• Wind and Structures
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• 제22권4호
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• pp.429-454
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• 2016

In this paper, a shear deformation plate theory based on neutral surface position is developed for free vibration analysis of functionally graded material (FGM) plates. The material properties of the FGM plates are assumed to vary through the thickness of the plate by a simple power-law distribution in terms of the volume fractions of the constituents. During manufacture, defects such as porosities can appear. It is therefore necessary to consider the vibration behavior of FG plates having porosities in this investigation. The proposed theory is based on assumption that the in-plane and transverse displacements consist of bending and shear components, in which the bending components do not contribute toward shear forces and, likewise, the shear components do not contribute toward bending moments. The neutral surface position for a functionally graded plate which its material properties vary in the thickness direction is determined. The equation of motion for FG rectangular plates is obtained through Hamilton's principle. The closed form solutions are obtained by using Navier technique, and then fundamental frequencies are found by solving the results of eigenvalue problems. Numerical results are presented and the influences of the volume fraction index and porosity volume fraction on frequencies of FGM plates are clearly discussed.

• 대한토목학회논문집
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• 제26권3A호
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• pp.447-455
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• 2006

순수변위 비선형 4절점 쉘요소의 정식화를 제안하여 철근 콘크리트, 강재및 복합재료등 범용 목적의 구조물의 해석에 적합하도록 하였다. 기하강성의 정식은 2차 운동역학적 관계를 이용하여 쉘이 중립면에서 정의되었고 이러한 기하강성은 면내응력, 휨 모멘트와 수직 전단력의 형태로 구성되어 두꺼운 판 및 쉘의 해석에 효과적이다. 가정된 자연 변형률 방법을 사용하여 전단잠김 문제를 제거한 복합 쉘 요소는 얇은 판및 쉘의 경우에도 정확한 해를 구할 수 있다. 콘크리트 경우 소성이론 및 탄소성 파괴역학에 근거한 비탄성 해석이 가능하며 강재경우 폰미스의 항복이론과 이바노브의 항복이론을 이용한 소성해석이 가능하다. 복합 재료의 수직전단 강성 행렬은 평형방정식으로부터 유도하여 구성하였다. 본 연구에서 제안한 쉘 요소는 해석 예제들이 참고문헌과 잘 일치하여 정확성이 입증되었으며 범용목적의 박판구조 해석에 적합한 것으로 사료 되었다.

• 대한토목학회논문집
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• 제14권1호
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• pp.93-103
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• 1994

본(本) 논문(論文)에서는 내부(內部)힌지가 있는 평면(平面) 뼈대구조(構造)의 기하학적(幾何學的)인 비선형(非線型)을 수행하기 위한 두 가지 해석방법(解析方法) 즉, 유한분절법(有限分節法)과 유한요소법(有限要素法)을 제시한다. 유한분절법(有限分節法)의 경우에는 내부(內部)힌지에 대한 경계조건(境界條件)이 고려된 평형방정식(平衡方程式)과 힘-변위(變位) 관계식(關係式)을 직접(直接) 적분(積分)하여 엄밀한 접선강도(接線剛度) 매트릭스를 유도한다. 유한요소법(有限要素法)의 경우에는 내부(內部)힌지와 전단변형(剪斷變形)의 영향이 고려된 Hermitian 다항식(多項式)을 형상함수(形狀凾數)로 사용하여 탄성(彈性) 및 기하학적(幾何學的)인 강도(剛度)매트릭스를 산정한다. 제시된 이론(理論)의 정확성(正確性)과 타당성(妥當性)을 입증(立證)하기 위하여, 선택된 예제(例題)의 해석결과(解析結果)를 제시한다.

• Smart Structures and Systems
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• 제22권1호
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• pp.27-40
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• 2018

The governing equations of motion are derived for analysis of a sandwich microbeam in this paper. The sandwich microbeam is including an elastic micro-core and two piezoelectric micro-face-sheets. The microbeam is subjected to transverse loads and two-dimensional electric potential. Higher-order sinusoidal shear deformation beam theory is used for description of displacement field. To account size dependency in governing equations of motion, strain gradient theory is used to mention higher-order stress and strains. An analytical approach for simply-supported sandwich microbeam with short-circuited electric potential is proposed. The numerical results indicate that various types of parameters such as foundation and material length scales have significant effects on the free vibration responses and dynamic results. Investigation on the influence of material length scales indicates that increase of both dimensionless material length scale parameters leads to significant changes of vibration and dynamic responses of microbeam.

• 한국강구조학회 논문집
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• 제9권1호통권30호
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• pp.65-79
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• 1997

Composite materials are consist of two or more different materials to produce desirable properties for structural strength. Because of their superiority in strength, corrosion resistance, and weight reduction, they are used extensively as structural members. The objective of this study is to present the effectivness of the laminated composite elements by analyzing in-plane displacement and stress of the anisotropic laminated annular elements. Anisotropic laminated structures are very difficult to analyze and apply, compared with isotropic and orthotropic cases for arbitrary boundaries and fiber angle -ply. Boundary conditions for the examples used in this study consist of two opposite edges clamped and the other two edges free, and finite difference method is used in this study for numerical analysis. From the numerical result, it is found that the program used in this study can be used to obtain the displacement of the straight beams considering it's transverse shear deformation as well as anisotropic laminated elements. Several numerical examples show the advantages of the stiffness increase when the angle-ply composite materials are used. Therefore it gives a guide in deciding how to make use of fiber's angle for the subtended angle, load cases, and boundary conditions.

• Advances in nano research
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• 제1권1호
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• pp.1-11
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• 2013

The thermal buckling properties of double-walled carbon nanotubes (DWCNTs) are studied using nonlocal Timoshenko beam model, including the effects of transverse shear deformation and rotary inertia. The DWCNTs are considered as two nanotube shells coupled through the van der Waals interaction between them. The geometric nonlinearity is taken into account, which arises from the mid-plane stretching. Considering the small-scale effects, the governing equilibrium equations are derived and the critical buckling temperatures under uniform temperature rise are obtained. The results show that the critical buckling temperature can be overestimated by the local beam model if the nonlocal effect is overlooked for long nanotubes. In addition, the effect of shear deformation and rotary inertia on the buckling temperature is more obvious for the higher-order modes. The investigation of the thermal buckling properties of DWCNTs may be used as a useful reference for the application and the design of nanostructures in which DWCNTs act as basic elements.

• Structural Engineering and Mechanics
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• 제17권5호
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• pp.641-654
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• 2004

This paper presents a theoretic model of a smart structure, a transversely isotropic piezoelectric thick square plate constructed with three laminas, piezoelectric-elastic-piezoelectric layer, by adopting the first order shear deformation plate theory and piezoelectric theory. This model assumes that the transverse displacements through thickness are linear, and the in-plane displacements in the mid-plane of the plate are not taken to be account. By using Fourier's series expansion, an exact Navier typed analytical solution for deflection and electric potential of the simply supported smart plate is obtained. The electric boundary conditions are being grounded along four vertical edges. The external voltage and non-external voltage applied on the surfaces of piezoelectric layers are all considered. The convergence of the present approach is carefully studied. Comparison studies are also made for verifying the accuracy and the applicability of the present method. Then some new results of the electric potentials and displacements are provided. Numerical results show that the electrostatic voltage is approximately linear in the thickness direction, while parabolic in the plate in-plane directions, for both the deflection and the electric voltage. These results are very useful for distributed sensing and finite element verification.

• Structural Engineering and Mechanics
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• 제40권6호
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• pp.783-800
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• 2011

This paper addresses the finite strip formulations for the stability analysis of viscoelastic composite plates with variable thickness in the transverse direction, which are subjected to in-plane forces. While the finite strip method is fairly well-known in the buckling analysis, hitherto its direct application to the buckling of viscoelastic composite plates with variable thickness has not been investigated. The equations governing the stiffness and the geometry matrices of the composite plate are solved in the time domain using both the higher-order shear deformation theory and the method of effective moduli. These matrices are then assembled so that the global stiffness and geometry matrices of a moderately thick rectangular plate are formed which lead to an eigenvalue problem that is solved to determine the magnitude of critical buckling load for the viscoelastic plate. The accuracy of the proposed model is verified against the results which have been reported elsewhere whilst a comprehensive parametric study is presented to show the effects of viscoelasticity parameters, boundary conditions as well as combined bending and compression loads on the critical buckling load of thin and moderately thick viscoelastic composite plates.

• Composites Research
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• 제33권6호
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• pp.377-382
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• 2020

본 연구에서는 Rayleigh-Ritz 법을 이용하여 열린 단면보로 보강된 복합재료 주름판의 자유진동 특성을 연구하였다. 복합재료 주름판에 대해 등가균질모델을 이용하였으며, 이 등가모델은 주름판을 두 수직방향에 대해 서로 다른 재료특성을 갖도록 직교이방성판으로 취급한다. 등가 직교이방성판의 운동은 회전 관성 및 횡전단변형을 고려하기 위해 1차 전단변형이론을 기초로 표현된다. 또한 진동형상에서 보강재의 위치에 따른 국부 형상을 표현하기 위해 이산보강이론이 적용되었다. 제안된 해석 방법에 대한 타당성을 검증하기 위해 ANSYS를 이용한 유한요소해석을 수행하였으며, 두 방법을 이용해 얻은 진동수 및 진동형상을 비교하였다.

• Coupled systems mechanics
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• 제9권6호
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• pp.499-519
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• 2020

The effect of porosity on the thermo-mechanical behavior of simply supported functionally graded plate reposed on the Winkler-Pasternak foundation is investigated analytically in the present paper using new refined hyperbolic shear deformation plate theory. Both even and uneven distribution of porosity are taken into account and the effective properties of FG plates with porosity are defined by theoretical formula with an additional term of porosity. The present formulation is based on a refined higher order shear deformation theory, which is based on four variables and it still accounts for parabolic distribution of the transverse shearing strains and stresses through the thickness of the FG plate and takes into account the various distribution shape of porosity. The elastic foundation is described by the Winkler-Pasternak model. Anew modified power-law formulation is used to describe the material properties of FGM plates in the thickness direction. The closed form solutions are obtained by using Navier technique. The present results are verified in comparison with the published ones in the literature. The results show that the dimensionless and stresses are affected by the porosity volume fraction, constituent volume fraction, and thermal load.