• Journal of the Computational Structural Engineering Institute of Korea
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• v.13 no.3
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• pp.329-336
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• 2000

A method for automatic extraction of 2-dimensional finite element connectivities by searching the shortest closed path from a certain node to the starting node was developed. Only the best path among the possible paths was probed. The uniqueness and validity of the extracted path were examined. The proposed method was proved to be complete. Examples show that the proposed method can extract elements exactly from the irregular mesh which can not be handled easily by the conventional automatic mesh generation.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.4
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• pp.35-43
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• 2003

In this paper, an efficient computational algorithm for the implementation of the newly proposed node activation technique is presented, and its computational aspects are thoroughly investigated. To verify the validity, convergence, and efficiency of the node activation technique, various numerical examples are worked out including the problems of Poisson equation, 2D elasticity problems, and 3D elasticity problems. From the numerical tests, it is verified that one can arbitrarily activate and handle the nodal points of interest in finite element model with very little loss of the numerical accuracy.

• Composites Research
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• v.29 no.1
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• pp.16-23
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• 2016

In this paper, numerical results of sectional analysis, stress recovery and energy release rate were compared with the results of VABS, 3-D FEM through the blade analysis library. The result of stress recovery analysis for one-dimensional model including the stiffness matrix is compared with stress results of three-dimensional FEM. We discuss the configuration of the blade analysis library and compare verifications of numerical analysis results of VABS. Blade analysis library through dimensional reduction and stress recovery is intended to be utilized in conjunction with pre- and post-processing of the analysis program of the composite blade, high-altitude uav's wing, wind blades and tilt rotor blade.

• Computational Structural Engineering
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• v.6 no.4
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• pp.107-118
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• 1993

New methods of visualizing the data from finite element analyses of 3-dimensional solids were developed in this study. Their efficiency and practicality were examined through their application and implementation into a finite element analysis software. The major effort of the study was to provide a way of representing data inside of volume, which is the most difficult problem in the postprocessing of 3-dimensional solids. Section representation, volume slice and separation, and isosurface representation were proposed for this purpose.

• Computational Structural Engineering
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• v.15 no.2
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• pp.73-78
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• 2002

• Proceedings of the Computational Structural Engineering Institute Conference
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• 2011.04a
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• pp.764-767
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• 2011

본 논문에서는 유한요소법을 이용하여 임의의 단면을 가지는 빔의 비틀림 문제를 해석 할 수 있는 방법론을 제시하였다. 빔 유한요소에서 연속적인 뒤틀림함수를 얻기 위해 각 절점에서 뒤틀림자유도를 정의한 후 빔의 길이 방향으로 보간하였다. 이러한 방법의 사용은 뒤틀림구속효과와 비선형문제에 쉽게 접근 할 수 있게 한다. 또한, 임의의 단면에 대한 뒤틀림함수는 각 단면에서 St.Venant 방정식을 유한요소법을 통해 수치적으로 계산된다. 단면에서 계산된 해는 3차원 일반 빔 요소의 변위장에 매핑된다. 위와 같은 절차를 통해 개발된 빔 유한요소를 사용하면 임의의 단면을 가진 빔 구조물을 자유/구속 뒤틀림조건에서 비틀림, 굽힘, 신축 변형이 복합적으로 고려하여 해석해 낼 수 있다. 이렇게 해석된 결과를 검증하기 위하여 사각단면과 L단면에서의 결과 값을 고찰하였다.

• Proceedings of the KIEE Conference
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• 2009.07a
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• pp.792_793
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• 2009

본 논문에서는 3차원 유한요소해석을 이용하여 단상유도전동기의 스큐유무에 따른 특성을 비교하였다. 기존 2차원 유한 요소 해석을 이용하는 경우 스큐를 갖는 유도전동기의 해석결과가 갖는 불합리점을 지적하였고 3차원해석과 2차원해석결과를 비교하였다. 그리고 스큐가 있는 경우와 없는 경우의 모델을 3차원 해석하였으며 이를 통해 얻은 다양한 결과를 제시하고 스큐의 영향을 분석하였다.

• Computational Structural Engineering
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• v.11 no.4
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• pp.253-265
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• 1998

본 논문에서는 연계논문에서 제시한 비대칭 박벽단면을 갖는 곡선보 및 직선보 이론을 토대로, 곡선보 요소 및 직선보 요소를 개발하고 이를 이용한 유한요소 정식화 과정을 제시한다. 유한요소 정식화 과정에서는 요소의 변위장을 도심에 대하여 정의한 후, 요소 변위벡터에 관한 3차의 Hermitian 다항식을 형상함수로 사용하고 가우스 적분을 행함으로써 탄성 강도행렬 및 기하학적 강도행렬을 산정하였다. 얻어진 강도행렬을 이용하여 고유치 문제를 계산함으로써 좌굴하중을 계산하였으며 다양한 해석 예제를 통하여 다른 연구자들의 해석 결과와 비교 검토함으로써 본 연구의 타당성과 우수성을 입증하고자 한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.45 no.12
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• pp.1021-1030
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• 2017

This paper describes the algorithm of computing thermal contact conductance between unmatched grid interfaces for finite element thermal analysis. Because grid interfaces should be coincident with adjacent meshes for finite element method, large amount of man hours and huge computations are required to match interfaces between many numbers of complex subdomains. A novel method that distributes feasibly the conductances to interface nodes is proposed. The aims of the method are described, and details of the nodal conductance distribution algorithm with less dependency on meshes are represented. The algorithm can be applied both the flat and curved interfaces in 3 dimensional space, and proposed method can combined with many finite element application including thermal analysis.

• Journal of the Korean Society for Advanced Composite Structures
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• v.3 no.1
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• pp.1-7
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• 2012

This study investigates free vibration characteristics of laminated composite structures with different embedded delamination sizes and locations using the solid element. The three-dimensional finite element (FE) delamination model described in this paper, in comparison with the conventional approaches, is more attractive not only because it shows better accuracy but also it shows the entire mode shape. The FE model using ABAQUS is used for studying free vibrations of laminates containing an various embedded delamination. The numerical results obtained are in good agreement with those reported by other investigators. In particular, new results reported in this paper are focused on the significant effects of the local vibration mode for various parameters, such as size of delamination, aspect ratio, and location of delamination.