• 소음진동
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• 제7권1호
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• pp.127-134
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• 1997

The dynamic stability of classical plates and Mindlin plates subjected to pulsating follower forces is investigated in this paper. Using the finite element method, the induced equation is reduced to that of one with finite degrees of freedom. Then, the multiple scales method is applied to analyze the dynamic instability region. The effects of aspect ratio, Poisson ratio, rotary inertia and shear deformation on the dynamic stability of plates are studied in this paper.

• Structural Engineering and Mechanics
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• 제7권1호
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• pp.19-33
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• 1999

The critical buckling loads of unsymmetrically laminated rectangular plates with a given material system and subjected to combined lateral and inplane loads are maximized with respect to fiber orientations by using a sequential linear programming method together with a simple move-limit strategy. Significant influence of plate aspect ratios, central circular cutouts, lateral loads and end conditions on the optimal fiber orientations and the associated optimal buckling loads of unsymmetrically laminated plates has been shown through this investigation.

• Journal of Advanced Marine Engineering and Technology
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• 제26권3호
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• pp.344-352
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• 2002

In the analysis of the 3 dimensional plate structures by the finite element method, the triangular elements are generally used for the global stiffness matrix of the analyzed system. But the triangular elements of the plates have some problems in the process of formulation and in the precision of analysis. The formulation of the finite element method to analyze 3 dimensional plate structures using quadrilateral elements is presented in this paper. The degree of freedom off nodal point is 6, that is, the displacements in the direction off-y-z is and the rotations about x-y-z axis and then the degree of freedom off element is 24. For the comparison of the analysis using triangular elements and quadrilateral elements, the rectangular plates subjected to the uniform load and a concentrated load on the centroid of the plate, for which the theoretical solutions have been obtained, are analyzed. The calculated deflections of the rectangular plates using the finite element method by the triangular elements and the quadrilateral elements are also compared with the deflections of the plates calculated by theoretical solutions. The defections of the rectangular plates calculated by the finite element method using the quadrilateral elements are closer to the theoretical solutions than the defections calculated by the finite element method using the triangular elements. The deflection of the centroid of plate, calculated by the finite element method, converges to that of theoretical solution as the number of elements is increased. This convergence is much more rapid for the case of using the quakrilateral elements than fir the case of using triangular elements.

• 한국강구조학회 논문집
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• 제25권3호
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• pp.267-278
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• 2013

본 연구에서는 개단면 리브를 갖는 보강판에서 발생하는 국부처짐과 모멘트가 정사각형 재하크기에 따라 어떻게 변화하는지 분석하여 이를 정형화 하고자 하였다. 평강 리브와 역T형 리브를 갖는 보강판에 대하여 각각의 재하크기별로 여러 가지 제원 변화에 따른 비율함수를 구하여 분석한 결과, 재하크기에 따라 기준 보강판의 값에는 차이가 있으나 리브 간격을 제외하고, 각 제원별 비율 함수에는 큰 차이가 없어 재하크기를 통합하여 표현 가능함을 알 수 있었다. 또한, 평강 리브와 역T형 리브의 차이도 크지 않아 리브 형태와 상관없이 통합한 하나의 함수로 사용 가능함을 알 수 있었으며, 이러한 통합된 하나의 비율함수식을 적용한 결과 상당한 정확도를 나타내었다. 본 연구에서 제안한 통합 함수를 L형 리브와 직사각형 재하에 적용한 결과, 타당한 결과를 나타내어 통합 함수의 적용성을 확인할 수 있었다. 따라서 본 연구에서 제안한 통합 비율함수식을 이용하면, 개단면 리브를 갖는 보강판에서 발생하는 국부처짐과 국부 모멘트 결과를 간편하게 얻을 수 있을 것으로 판단된다.

• Steel and Composite Structures
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• 제34권2호
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• pp.215-226
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• 2020

The aim of this study is to investigate free vibration of functionally graded porous nanocomposite rectangular plates where the internal pores and graphene platelets (GPLs) are distributed in the matrix either uniformly or non-uniformly according to three different patterns. The elastic properties of the nanocomposite are obtained by employing Halpin-Tsai micromechanics model. The GPL-reinforced plate is modeled using a semi-analytic approach composed of generalized differential quadrature method (GDQM) and series solution adopted to solve the equations of motion. The proposed rectangular plates have two opposite edges simply supported, while all possible combinations of free, simply supported and clamped boundary conditions are applied to the other two edges. The 2-D differential quadrature method as an efficient and accurate numerical tool is used to discretize the governing equations and to implement the boundary conditions. The convergence of the method is demonstrated and to validate the results, comparisons are made between the present results and those reported by well-known references for special cases treated before, have confirmed accuracy and efficiency of the present approach. New results reveal the importance of porosity coefficient, porosity distribution, graphene platelets (GPLs) distribution, geometrical and boundary conditions on vibration behavior of porous nanocomposite plates. It is observed that the maximum vibration frequency obtained in the case of symmetric porosity and GPL distribution, while the minimum vibration frequency is obtained using uniform porosity distribution.

• 한국강구조학회 논문집
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• 제19권2호
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• pp.161-170
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• 2007

본 연구에서는 직교이방성 판 해석의 정확도 문제를 개선하기 위하여 평강 리브를 갖는 보강판에 대하여 리브 제원을 고려한 직교이방성 휨 강성 수정 계수를 제안하고자 하였다. 이를 위하여 먼저, 직교이방성 휨 강성과 최대 처짐에 대하여 보강판 제원에 따른 민감도 분석을 실시하였으며, 보강판의 직교이방성 휨 강성 수정 계수에 대한 매개변수 연구를 수행하였다. 연구 결과, 수정 계수의 비율은 판 두께와 상관없이 리브 높이, 간격, 두께별로 하나의 함수로 표현 가능함을 알 수 있었으며, 이러한 수정 계수의 비율 함수로부터 간편하게 수정 휨 강성을 산정할 수 있음을 알 수 있었다. 지지 조건, 변장비, 리브 배치 및 재하 크기가 다른 여러 가지 보강판에 계수 함수를 적용한 결과, 참고 문헌에 비하여 직교이방성 판 해석의 정확도가 향상됨을 알 수 있었다. 따라서, 본 연구에서 제안한 계수 함수식을 사용하면 평강 리브를 갖는 보강판의 직교이방성 판 해석 시 간편하게 상당한 정확도의 결과를 얻을 수 있을 것으로 판단된다.

• 전산구조공학
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• 제3권2호
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• pp.77-88
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• 1990

환경조건 및 내부의 유공부 크기와 위치가 변화함에 따라 평판의 두개의 고유치(고유 진동수와 탄성 임계하중)는 어떻게 변화하며, 이들 고유치 상호간의 관계는 어떻게 되는지 검토 하기로 한다. 이상과 같은 검토 목적에는 수치 해석법이 적당한데 본 논문에서는 그 중의 하나인 유한 요소법을 채택하기로 한다. 유한 요소법에서 이용할 요소는 각 절점에서 자유도가 3, 따라서 요소 전체의 자유도가 12인 사각형 요소이다.

• 대한조선학회지
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• 제14권3호
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• pp.5-12
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• 1977

In shipyard production processes, lots of steel plates are assembled by welding. Some rectangular steel plates are buttwelded to build a large block in panel production lines. There are some advantages to take the tandem arc welding in butt joints of rectangular plates with respect to welding speed. Hence, the thermal stresses and the temperature distribution of the tandem arc welding are studied in this paper. The solutions in the case of the infinite plate with two instantaneous point heat sources have been obtained. And then the solutions have been extended to the case of two moving heat sources corresponding to the tandem arc welding with the aid of Duhamel's superposition integral. It was found that the temperature distribution was good agreement with the results of the experiments by Rosenthal and Park and the thermal stresses calculated were acceptable with respect to a physical phenomenon. These solutions are able to be applied to the problem such as a line heating.

• 대한기계학회논문집
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• 제18권8호
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• pp.1899-1909
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• 1994

This work presents the experimental and FEM results for the free vibration of cantilevered, symmetrically and antisymmetrically laminated composite rectangular plates. The natural frequencies, mode shapes and contour plots of a number of CFRP, GFRP, DFRP-Aluminum, GFRP-Aluminum and DFRP-GFRP hybrid composite plates are experimentally obtained. Determination of Young's modulus and test procedures are described. The natural frequencies are determined for a wide range of parameters : e.g. , composite material constants, fiber angles and stacking sequences. Natural frequency and nondimensional frequency parameter results are compared with the finite element analysis and existing literatures. Agreement between experimental and calculated frequencies is excellent. The effects of varing the parameters upon the free vibration frequencies and mode shapes are discussed.

• 한국항만학회지
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• 제14권1호
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• pp.87-95
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• 2000

This stability of a plate structure is very crucial problem which results in wrinkle and buckling. In this study, the effect of the pattern of spot-welding points of the two rectangular plates on the compressive and shear buckling load is studied with respect to the thickness, aspect ratio of plates and number of welding spots. Buckling coefficient of the plate not welded was compared with that of two plates with various thickness to extract the effect of thickness. The effect of number of welding spots are studied in two directions, longitudinal and transverse directions. The conclusions obtained were that the reinforcement effect was maximized when the aspect ratio was close to 1.75 at compressive load condition and that the effect of number of welding spots in transverse direction was larger than that in longitudinal direction at shearing load condition.