• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1991.04a
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• pp.111-116
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• 1991

주파수 영역에서 로터의 thickness noise는 블레이드의 여러가지 기하학적인 조건, 즉 블레이드 수, 블레이드의 사잇각, 에어포일의 모양 그리고 반경방향의 블레이드 끝모양에 따라서 해석되어진다. 본 논문은 비 등간격 로터의 기하학적 조건에 따른 음신호의 위상간섭 영향을 고찰하기 위해서 등간격을 이루는 로터에 대해서 해석된 Hanson의 방법을 확장하였다. thickness noise를 6개의 블레이드를 가진 로터에 대하여 15.deg., 30.deg., 45.deg., 비 등간격을 이루는 경우와 각각에 45 tip angle로 sweepback되었을 때 먼 거리의 음향학적 음신호와 그 스펙트럼을 계산하였다.

• Proceedings of the KIEE Conference
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• 1999.11c
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• pp.733-735
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• 1999

전압원을 포함한 대형회로망의 컴퓨터적 해법을 위한 도형적 접근 방법을 제시하였다. 기본적인 회로망 해석법으로 마디해석법을 사용하였고, 전압원은 등가변환이 어려운 직렬 임피던스가 없는 경우로 한정하였다. 방향성 그래프의 기하학적 작도와 전압원이 연결된 마디와 마디 사이의 상관 관계식에 의해 회로망 행렬을 구성하였다.

• Journal of the Korean Society for Railway
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• v.13 no.2
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• pp.147-151
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• 2010

Since the kinetic energy is dissipated through plastic deformation energy generated in expanding process of the tube by a die. In order to successfully absorb the kinetic energy there should be no buckling in the expansion tube during expanding process. The buckling instability of the expansion tubes is affected by the initial boundary conditions, tube thickness and length. In this study, the effects of the tube thickness except length and initial boundary condition on the buckling instability are studied using a finite element method. In addition, Analysis procedure for nonlinear post-buckling analysis of expansion tube is established. There are three kinds of finite element analysis procedures for buckling analysis of expansion tube, quasi-static analysis, linear buckling analysis and nonlinear post-buckling analysis. The effect of the geometry imperfections defined as linear superimposition of buckling modes is considered in the nonlinear post-buckling analysis. The results of finite element analysis indicate that the buckling load increase with increase of thickness of tube and geometry imperfection. Finial buckling shapes are changed with respect to the geometry imperfection.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.10 no.2
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• pp.1-9
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• 1990

A variational approach with reference volume and adjoint structure concepts is applied for the structural design densitivity analysis of geometrically nonlinear structures. A general form of sensitivity equation is used and then nonlinear finite element procedure is implemented for the discretized structural model. Usability and effectiveness of the variational approach for the design sensitivity analysis of geometrically nonlinear structural responses are verified through a numerical example.

• Proceedings of the Computational Structural Engineering Institute Conference
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• 2010.04a
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• pp.562-565
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• 2010

본 논문에서는 유한요소법을 이용하여 두 개의 층으로 이루어진 Si/SiGe 나노스프링의 기하학적 형상에 대한 연구가 수행된다. 나노스프링의 기하학적 형상에 영향을 미치는 주 설계요소로는 두께, 폭, 길이, 격자방향 등이 있으며, 두 개의 층으로 이루어진 Si/SiGe 박막이 나노스프링의 형상을 가지게 되는 주원인으로는 두 개의 층 경계면에서 발생하는 misfit strain이 있다. 본 연구에서는 두께, 폭, 길이, 격자방향 등의 설계요소를 변화시켜가면서 mistif strain에 의한 나노스프링의 곡률 변화에 대한 해석 결과가 제시된다. 또한 해석 결과의 검증을 위해 해석해의 결과와 분자동력학 전산모사 결과가 함께 제시된다.

• Journal of Korean Society of Steel Construction
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• v.11 no.4 s.41
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• pp.417-424
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• 1999

In this paper a nonlinear analysis of three-dimensional steel frames is developed. This analysis accounts for material and geometric nonlinearities. The material nonlinearity includes gradual yielding associated with flexural behaviors. The geometric nonlinearity includes the second-order effects associated with $P-{\delta}\;and\;P-{\Delta}$ effects. The material nonlinearity at the node is considered using the concept of P-M hinge consisting of many fibers. The geometric nonlinearity is considered by the use of stability function. The nonlinearity caused by shear and torsional interaction effects is neglected. The modified incremental displacement method is used as the solution technique. The load-displacements predicted by the proposed analysis compare well with those given by other approaches.

• Journal of the Korea institute for structural maintenance and inspection
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• v.15 no.2
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• pp.125-135
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• 2011

The latest study for formulation of finite element method and computation techniques has progressed widely. The classical method in the formulation of frame elements for geometrically nonlinear analysis derives the geometric stiffness directly from the governing differential equation for bending with axial force. From the computational viewpoint of this paper, the most common approach is the finite element method. Commonly, the formulation of frame elements for geometrically nonlinear structures is based on appropriate interpolation functions for the transverse and axial displacements of the member. The formulation of flexibility-based elements, on the other hand, is based on interpolation functions for the internal forces. In this paper, a new method is used to suppose that interpolation functions for the displacements from the curvatures is Lagrangian interpolation. This paper derives flexibility matrix from that displacement functions and is considered the application of it. Using the flexibility matrix, this paper apply the program considered geometrically nonlinear analysis to common problems.

• Journal of the Society of Naval Architects of Korea
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• v.29 no.2
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• pp.132-139
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• 1992

This paper presents geometrically nonlinear formulation of shell problems using the three-dimensional curved shell element, which includs large displacements and large rotations. Formulations of the geometrically nonlinear problems can be derived in a variety of ways, but most of them have been obtained by assuming that nodal rotations are small. Hence, the tangent stiffness matrix is derived under the assumptions that rotational increments are infinitesimal and the effect of finite rotational increments have to be considered during the equilibrium iterations. To study the large displacement and large rotation problems, the restrictions are removed and the formulations of the curved shell element including the effect of large rotational increments are developed in this paper. The displacement based finite element method using this improved formulation are applied to the analyses of the geometrically nonlinear behaviors of the single and double curved shells, which are compared with the results by others.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.13 no.2
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• pp.209-220
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• 2000

For non-linear analysis of stiffened shell structures, the total Lagrangian formulation is presented based upon the degenerated shell element. Geometrically correct formulation is developed by updating the direction of normal vectors and taking into account second order rotational terms in the incremental displacement field. Assumed strain concept is adopted in order to overcome shear locking phenomena and to eliminate spurious zero energy mode. The post-buckling behaviors of stiffened shell structures are traced by modeling the stiffener as a shell element and considering general transformation between the main structure and the stiffener at the connection node. Numerical examples to demonstrate the accuracy and the effectiveness of the proposed shell element are presented and compared with references' results.

• Computational Structural Engineering
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• v.11 no.4
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• pp.321-330
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• 1998

막구조의 초기형상을 결정하기 위하여 막요소의 기하학적 비선형을 고려한 평형방정식을 유도하고, 등장력곡면(equally stressed surface)을 결정하기 위한 알고리즘을 정식화한다. 막구조는 대변형에 의한 기하학적 비선형성을 포함하고, 막구조의 특성상 초기장력에 의한 초기변형을 고려해야 하므로, 본 논문에서는 막구조와 같은 인장구조물의 비선형 수치해석을 수행하기 위한 해석기법으로써, 동적이완법(Dynamic Relaxation Method)에 대한 해석알고리즘을 적용하고, 이 방법에 의해 수행한 해석결과를 검토함으로써 막구조 해석에 적용 가능한 수치해석기법을 제시하고, 수치해석에 대한 예를 통해 본 해석법의 타당성을 검증한다.