• Structural Engineering and Mechanics
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• 제9권1호
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• pp.99-110
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• 2000

The objective of this paper is to extend the use of the improved degenerated shell element to the linear and the large displacement analysis of plates and shells with laminated composites. In the formulation of the element stiffness, the combined use of three different techniques was made. This element is free of serious shear/membrane locking problems and undesirable compatible/commutable spurious kinematic deformation modes. The total Lagrangian approach has been utilized for the definition of the deformation and the solution to the nonlinear equilibrium equations is obtained by the Newton-Raphson method. The applicability and accuracy of this improved degenerated shell element in the analysis of laminated composite plates and shells are demonstrated by solving several numerical examples.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1994년도 추계학술대회 논문집
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• pp.843-846
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• 1994

The bucking and postbuckling behavior of composite laminated long cylinders under lateral pressure are investigated by the nonlinear finite element method. A long cylinder of 3-D shell problem is modelled as 2-D plane strain problem for analysis. And for the finite element analysis, eight nodes quadratic element is utilized. Arc-length method is adopted for the iteration and load-increment along postbuckling equilibrium path. The composite laminated cylinders in study are composed of cross-plied uniaxially reinforced shells. As a prsult, buckling load and postbuckling behavior are discussed.

• 복합신소재구조학회 논문집
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• 제1권3호
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• pp.24-34
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• 2010

본 논문은 전단변형효과를 고려한 복합신소재 적층 쉘을 해석하기 위하여, 일반 쉘의 지배방정식을 유도하고, 이 방정식을 풀기 위하여 수치해석 기법중 하나인 유한차분법을 수행하였다. 유한차분법을 미분방정식을 지배방정식으로 가지는 구조물 해석시 간편하게 사용될 수 있고, 오차의 범위를 선택적으로 정할수 있는 장점이 있다. 수치해석 결과의 타당성을 검증하기 위하여 수렴도 분석과 범용 구조해석 프로그램인 LUSAS의 해석결과와 비교하였다. 본 논문의 목적은 전단변형 효과를 고려한 일반 쉘의 거동 특징 및 분석, 복합재료로 구성되었을 경우 정확한 거동을 분석하고, 쉘 구조물이 보다 높은 강성을 가질 수 있도록 하는 적절한 화이버의 보강방안과 다양한 조건 변화를 통해서 최적의 쉘 구조물을 제시하는 것이다. 쉘의 곡률의 변화에 따른 거동과 합응력의 변화를 분석하고, 쉘의 높이-너비 비와 화이버 보강각도 변화에 따른 처짐 및 합응력의 변화를 비교, 분석하여 보다 유리한 쉘 구조물을 제시하였다. 또한 다양한 하중을 가하여 쉘의 형상 변화를 비교 분석함으로서 비등방성 재료로 이루어진 일반 쉘의 거동에 대하여 분석하였다.

• Steel and Composite Structures
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• 제28권3호
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• pp.389-401
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• 2018

An isoparametric six-node triangular element is utilized for geometrically nonlinear analysis of functionally graded (FG) shells. To overcome the shear and membrane locking, the element is improved by using strain interpolation functions. The Total Lagrangian formulation is employed to include the large displacements and rotations. Finding the nonlinear behavior of FG shells via laminated modeling is also the goal. A power function is employed to formulate the variation of elastic modulus through the thickness of shells. The results are presented in two ways, including the general FGM formulation and the laminated modeling. The equilibrium path is obtained by using the Generalized Displacement Control Method. Some popular benchmarks, including hyperbolical shell structures are solved to declare the correctness and accuracy of proposed formulations.

• Steel and Composite Structures
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• 제22권6호
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• pp.1445-1463
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• 2016

The effects of moisture and temperature on buckling of laminated composite cylindrical shell panels are investigated both numerically and experimentally. A quadratic isoparametric eight-noded shell element is used in the present analysis. First order shear deformation theory is used in the present finite element formulation for buckling analysis of shell panels subjected to hygrothermal loading. A program is developed using MATLAB for parametric study on the buckling of shell panels under hygrothermal field. Benchmark results on the critical loads of hygrothermally treated woven fiber glass/epoxy laminated composite cylindrical shell panels are obtained experimentally by using universal testing machine INSTRON 8862. The effects of curvature, lamination sequences, number of layers and aspect ratios on buckling of laminated composite cylindrical curved panels subjected to hygrothermal loading are considered. The results are presented showing the reduction in buckling load of laminated composite shells with the increase in temperature and moisture concentrations.

• 전산구조공학
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• 제8권3호
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• pp.135-141
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• 1995

자유 모양을 한 적층판 형태의 복합 회전체 쉘 구조물은 원추형 쉘 요소의 조합으로 나타낼 수 있다. 이에 이 논문에서는 원추형 쉘 요소에 대한 유한요소해석 모델을 개발하고자 한다. 또한 이 모델의 타당성을 입증하기 위해 기존의 원통형 쉘으 고유진동 이론해와 비교한다. 여러 형태의 복합 원통형 쉘에 대해 여러 가지 인자변환 실험을 행한다. 실험을 통하여서 이 논문에서 제시한 모델을 이용한 고유진동 주파수 결과와 이론해에서 구한 결과가 매우 흡사하다는 것을 알았으며 그로 말미암아 이 모델의 적합성을 확인하였다. 이 원추형 쉘 요소의 개발로 말미암아 어떠한 형태의 적층 이방성 복합 회전체 쉘에 대해서도 해석이 용이하다.

• 한국강구조학회 논문집
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• 제9권3호통권32호
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• pp.333-340
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• 1997

본 연구에서는 복합재료로 구성된 복합적층판 및 쉘에 대하여 3차 전단 변형이론을 이용한 변위를 가정하여 단순지지 경계조건을 만족하는 변위형상함수를 퓨리예급수로 전개하고 동적 평형 방정식을 유도하여 뉴마크의 수치적분법을 사용하여 단면특성계수, 재료의 특성, 층의 배열에 따른 복합적층판 및 쉘의 비감쇄 동적응답특성을 연구하였다.

• Steel and Composite Structures
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• 제22권5호
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• pp.1193-1214
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• 2016

In this paper, the 3D stress state and inter-laminar stresses in a rotating thin laminated cylinder shell are studied. The thickness of the cylinder is supposed to be thin and it is made of laminated composite material and can have general layer stacking. The governing equations of the cylindrical shell are obtained by employing the Layerwise theory (LWT). The effect of rotation is considered as rotational body force which is induced due to the rotation of the cylinder about its axis. The Layerwise theory (LWT), is used to discrete the partial differential equations of the problem to ordinary ones, in terms of the displacements of the mathematical layers. By applying the Free boundary conditions the solution of the governing equations is completed and the stress state, the inter-laminar stresses, and the edge effect in the rotating cylindrical shells are investigated in the numerical results. To verify the results, LWT solution is compared with the results of the FEM solution and good agreements are achieved. The inter-laminar normal and shear stresses in rotating cylinder are studied and effects of layer stacking and angular velocity is investigated in the numerical results.

• 대한기계학회논문집
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• 제13권5호
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• pp.807-819
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• 1989

본 연구에서는 Donnell과 Flugge 셸 이론을 이용하여 단순지지된 비원형 단면을 가진 angle-ply 적층원통셸의 좌굴과 진동해석을 Soldatos의 해석과정을 따라 수행하고, 적층방법(stacking sequence)과 섬유각(fiber angle)의 변화에 따른 고유진 동수와 좌굴하중의 변화를 고찰하였으며, 초기 축하중을 받는 경우에 대한 고유진동수 의 변화에 대해서고 고찰하였다.

• International Journal of Aeronautical and Space Sciences
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• 제13권3호
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• pp.332-348
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• 2012

The present study deals with the parametric resonance behaviour of laminated composite curved shell panels in a hygrothermal environment using Bolotin's approach. A simple laminated model is developed using first order shear deformation theory (FSDT) for the vibration and dynamic stability analysis of laminated composite shells subjected to hygrothermal conditions. A computer program based on the finite element method (FEM) in a MATLAB environment is developed to perform all necessary computations. Quantitative results are presented to show the effects of curvature, ply-orientations, degree of orthotropy and geometry of laminates on the parametric instability of composite curved shell panels for different temperature and moisture concentrations. The excitation frequencies of laminated composite panels decrease with the increase of temperature and moisture due to reduction of stiffness for all laminates.