• Structural Engineering and Mechanics
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• 제85권4호
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• pp.433-443
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• 2023

The current paper discusses the dynamic and stability responses of cross-ply composite laminated plates by employing a refined quasi-3D trigonometric shear deformation theory. The proposed theory takes into consideration shear deformation and thickness stretching by a trigonometric variation of in-plane and transverse displacements through the plate thickness and assures the vanished shear stresses conditions on the upper and lower surfaces of the plate. The strong point of the new formulation is that the displacements field contains only 4 unknowns, which is less than the other shear deformation theories. In addition, the present model considers the thickness extension effects (ε_z≠0). The presence of the Winkler-Pasternak elastic base is included in the mathematical formulation. The Hamilton's principle is utilized in order to derive the four differentials' equations of motion, which are solved via Navier's technique of simply supported structures. The accuracy of the present 3-D theory is demonstrated by comparing fundamental frequencies and critical buckling loads numerical results with those provided using other models available in the open literature.

• 대한토목학회논문집
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• 제34권1호
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• pp.61-71
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• 2014

본 연구에서는 건설용 복합소재 구조에 적합한 미시-거시적 멀티 스케일 접근 방법을 제시하고 고차항 이론에 기반한 유한요소 진동 해석을 수행하였다. 본 연구에서 제시하는 멀티-스케일 접근 방법에 의한 유한요소 모델은 해석의 정확성 뿐 만 아니라 재료 조합의 영향을 정확히 보여준다는 점에서 장점을 갖는다. 적용된 유한요소 모델은 화이버의 함침비율의 변화에 따른 적층 판 구조의 고유진동을 상세 분석하기 위하여 개발되었다. 특히, 본 연구에서 제시한 결과는 적층 구조의 보강각도, 적층배열, 그리고 길이-두께비 등과 화이버 함침비율의 변화의 상호작용을 분석하는 데 초점을 두었다. 수치해석 결과로부터 화이버와 모재의 조합의 영향은 거시적 동적 특성을 조절할 수 있으므로 무시되면 안되며, 최적 배합을 통하여 건설용으로서 우수한 동적 구조성능을 만족하도록 설계할 수 있음을 보여준다.

• Structural Engineering and Mechanics
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• 제28권5호
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• pp.603-633
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• 2008

A four-node plate finite element for the analysis of laminated composites which is developed using strain gradient notation is presented. The element is based on a first-order shear deformation theory and on the equivalent lamina assumption. Strains and stresses can be calculated at different points through the thickness of the plate. They are averaged values due to the equivalent lamina assumption. A shear correction factor is used as the transverse shear strain is taken to be constant over the plate thickness while its actual variation is parabolic. Strain gradient notation, which is physically interpretable, allows for the detailed a-priori analysis of the finite element model. The polynomial expansions are inspected and spurious terms responsible for modeling errors are identified in the shear strains polynomial expansions. The element is corrected by simply removing the spurious terms from the shear strains expansions. The element is implemented into a FORTRAN finite element code in two versions; namely, with and without spurious terms. Results are compared to show the effects of the spurious terms on the solutions. It is also shown that a refined mesh composed of corrected elements provides solutions which approximate very well the analytical solutions, validating the procedure.

• 산업기술연구
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• 제19권
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• pp.227-233
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• 1999

Simple equations which can predict "exact" values of the natural frequency of vibration for the special orthotropic laminates are presented. Many laminates with certain orientations have decreasing values of $B_{16}$ and $B_{26}$ as the number of plies increases. Such laminates, with $D_{16}=D_{26}{\rightarrow}0$, including the laminates with anti-symmetric configurations can be solved by the same equation for the special orthotropic laminates. If the quasi-isotropic constants are used, the equations for the isotropic plates can be used. Use of some coefficients cab produce "exact" value for laminates with such configurations. Natural frequencies of the plate with varying aspect ratios is presented.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1997년도 가을 학술발표회 논문집
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• pp.215-222
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• 1997

A method of calculating the natural frequency corresponding to the first mode of vibration of beams and tower structures, with irregular cross-sections and with arbitrary boundary conditions was developed and reported by D. H. Kim in 1974. This method has been developed for two-dimensional problems including the laminated composite plates and was proved to be very effective for the plates with arbitrary boundary conditions and irregular sections. In this paper, the result of application of this method to the subject problem is presented. This problem represents the building slabs with a kind of passive and active control devices. Any method may be used to obtain the deflection influence surfaces needed for this vibration analysis. Finite difference method is used for this purpose, in this paper. The influence of the modulus of the foundation on the natural frequency is thoroughly studied.

• Advances in aircraft and spacecraft science
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• 제1권2호
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• pp.145-175
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• 2014

The results of a series of numerical experiments are presented to verify some of the important developments made in the first part of this paper. Firstly, the static solution of an algebraic system obtained through Strong Formulation Finite Element Method (SFEM) is presented. Secondly, the stress and strain recovery procedure is descripted for the present technique. It will be clear that the present approach is suitable for any strong formulation finite element methodology, due to the presented general approach based on the unknown displacements and on the elasticity equations. Thirdly, the numerical solutions for some classical and other numerical results found in literature are exposed. Finally, an arbitrarily shaped composite plate is solved and good agreement is observed for all the presented cases.

• Structural Engineering and Mechanics
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• 제68권3호
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• pp.325-334
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• 2018

The Nonlinear dynamic response of a sandwich plate subjected to the low velocity impact is theoretically and experimentally investigated. The Hertz law between the impactor and the plate is taken into account. Using the Extended High Order Sandwich Panel Theory (EHSAPT) and the Ritz energy method, the governing equations are derived. The skins follow the Third order shear deformation theory (TSDT) that has hitherto not reported in conventional EHSAPT. Besides, the three dimensional elasticity is used for the core. The nonlinear Von Karman relations for strains of skins and the core are adopted. Time domain solution of such equations is extracted by means of the well-known fourth-order Runge-Kutta method. The effects of core-to-skin thickness ratio, initial velocity of the impactor, the impactor mass and position of the impactor are studied in detail. It is found that these parameters play significant role in the impact force and dynamic response of the sandwich plate. Finally, some low velocity impact tests have been carried out by Drop Hammer Testing Machine. The results are compared with experimental data acquired by impact testing on sandwich plates as well as the results of finite element simulation.

• International Journal of Naval Architecture and Ocean Engineering
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• 제9권4호
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• pp.373-381
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• 2017

A Collaborative Optimization (CO) methodology for ring-stiffened composite material pressure hull of underwater vehicle is proposed. Structural stability and material strength are both examined. Lamination parameters of laminated plates are introduced to improve the optimization efficiency. Approximation models are established based on the Ellipsoidal Basis Function (EBF) neural network to replace the finite element analysis in layout optimizers. On the basis of a two-level optimization, the simultaneous structure material collaborative optimization for the pressure vessel is implemented. The optimal configuration of metal liner and frames and composite material is obtained with the comprehensive consideration of structure and material performances. The weight of the composite pressure hull decreases by 30.3% after optimization and the validation is carried out. Collaborative optimization based on the lamination parameters can optimize the composite pressure hull effectively, as well as provide a solution for low efficiency and non-convergence of direct optimization with design variables.

• 한국강구조학회 논문집
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• 제16권5호통권72호
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• pp.621-628
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• 2004

본 연구에서는 보강판의 좌굴방지를 위해 기존에 주로 사용되는 보강재를 복합재료를 사용하여 대체하는 새로운 개념을 소개한다. 강재 보강재를 복합재료로 대체함으로써 용접의 불편함과 피로 등에 의한 손상 및 부식을 원천적으로 제거할 수 있다. 강판에 접착되는 복합재료는 강판이 좌굴할 때까지 완전히 접착된 것으로 가정하였다. 이렇게 구성되는 판은 길이와 폭 방향으로 변단면의 형태를 가지며 비등방성의 재료특성을 나타낸다. 이러한 비등방성 변단면 판의 좌굴해석을 위해 범용 유한요소 프로그램인 LUSAS를 사용하였으며 여러 가지 매개변수 변화 해석을 통해 비등방성 변단면 판의 좌굴거동 특성을 살펴보았다.

• 복합신소재구조학회 논문집
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• 제1권2호
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• pp.29-35
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• 2010

탄성계수와 함께 포아송비는 구조의 거동을 결정하는 중요 구조인수중의 하나이다. 따라서 구조응답의 불확실성에 미치는 포아송비의 독립적 영향에 대한 평가가 필요하다. 본 연구에서는 포아송비의 불확실성이 복합적층판의 거동에 미치는 영향을 산정하기 위한 정식화를 제안한다. 포아송비의 영향은 동일 차수인 임의인수의 영향을 포함하는 부행렬을 통하여 얻을 수 있으며, 이는 대상 인수의 평균을 중심으로 한 Taylor전개를 통하여 구할 수 있다. 제안방법의 검증을 위하여 예제 평판을 해석하였고, 그 결과를 몬테카를로 해석에 의한 결과와 비교하였다. 두 방법을 통하여 얻은 결과는 상화 잘 일치하는 결과를 나타내어, 제안한 방법이 적절함을 제시하였다.