• Composites Research
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• v.25 no.6
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• pp.217-223
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• 2012

This study investigates a geometrical nonlinear dynamic behaviors of laminated skew plates made of advanced composite materials (ACM). Based on the first-order shear deformation plate theory (FSDT), the Newmark method and Newton-Raphson iteration are used for the nonlinear dynamic solution. The effects of cutout sizes, skew angles and lay up sequences on the nonlinear dynamic response for various parameters are studied using a nonlinear dynamic finite element program developed for this study. The several numerical results were in good agreement with those reported by other investigators for square composite plates with or without central cutouts, and the new results reported in this paper show the significant interactions between the cutout, skew angles and layup sequence in the laminate. Key observation points are discussed and a brief design guideline of skew laminates is given.

• Journal of the KSME
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• v.26 no.2
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• pp.96-101
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• 1986

유한요소해석과 관련하여 그 분야와 과정을 소개하고 각각에 대하여 현재 연구의 중점방향과 예상되는 장래 집중연구 과제등을 기술하였다. 특히 공통적 기하학적 자료베이스에서부터 해 법자체와 나아가서 이들 결과의 설계응용의 자동화 또는 전문가 시스템화의 종합적인 방향이 장래 전문적인 제품설계의 방향으로 될 것을 주장하였다. 구분적인 연구는 사용자 편의의전. 후처리 프로그램, 대변형 비선형문제, 비선형 재료문제, 비선형 동적문제, 유한요소 모델링 기법, 설계와의 연계등에서 큰 진전이 있을 것으로 보고 이를 중심으로 기술하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1999.10a
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• pp.22-22
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• 1999

로켓의 노즐의 확대부와 같은 내열특성 증진이 필요한 곳에 주로 적용되어온 Involute 구조는 얇은 두께의 fabric 프리 프레그룰 일정한 패턴에 맞추어 재단한 후 적층하여 제작되어진다. 이렇게 제작된 노즐 확대부와 같은 구조물은 내삭마 및 구조 특성이 향상되고, 적층 및 성형 중 발생하는 링클과 보이드도 많이 예방할 수 있는 장점을 가진 것으로 알려져 있다. 이와 같은 장점 때문에 60년대부터 제작되어 노즐 확대부에 적용되어온 Involute 구조는 기하학적 복잡성으로 인해서 본질적으로 구조물의 비등방성 및 비균질성을 수반하게 되며, 이에 따른 열 및 구조해석의 어려움이 존재하게 된다. 70년대 Pagano에 의해서 그 기하학적복잡성이 수학적으로 규명되기 시작하여 80년대 가장 활발한 구조해석이 수행되어 노즐의 설계에 적용되었으며, 90년대 들어와서는 비선형 해석 및 최적설계 기법을 도입한 Involute 구조물의 기하학적 형상 및 구조적 최적화가 진행되고 있다. 하지만 국내에서는 아직까지 Involute 구조의 구조해석이 생소한 분야로서, 앞에서 언급한 일련의 진행 과정과 특징 등을 요약 및 정리할 필요가 있다 따라서, 본 발표는 비등방성 및 비균질성의 Involute 구조물에 대한 구조해석 기법들을 파악하고 그 적용 방법을 생각해 보고자 한다.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.14 no.1
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• pp.93-103
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• 1994

Two beam/column elements are developed in order to analyze the geometric nonlinear plane irames including the effects of internal hinge and transverse shear deformation. In the case of the first element (finite segment method), tangent stiffness matrix is derived by directly integrating the equilibrium equations whereas in the case of the second element (finite element method) elastic and goemetric stiffness matrices are calculated by using the hermitian polynomials including the effects of internal hinge and shear deformation as the shape function. Numerical results are presented for the selected test problems which demonstrate that both elements represent reliable and highly accurate tools.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.8 no.3
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• pp.1-10
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• 1988

A higher order plate bending finite element using cubic in-plane displacement profiles is proposed for geometrically nonlinear analysis of thin and thick plates. The higher order plate bending element has been derived from the three dimensional plate-like continuum by discretization of the equations of motion by Galerkin weighted residual method, together with enforcing higher order plate assumptions. Total Lagrangian formulation has been used for geometrically nonlinear analysis of plates and consistent linearization by Newton-Raphson method has been performed to solve the nonlinear equations. The element characteristics have been computed by, selective reduced integration technique using Gauss quadrature to avoid shear locking phenomenon in case of extremely thin plates. Several numerical examples were solved with FEAP macro program to demonstrate versatility and accuracy of the present higher order plate bending element.

• Computational Structural Engineering
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• v.3 no.3
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• pp.133-140
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• 1990

Analysis of cable structures is complex because their force - displacement relationships are highly nonlinear and also because large deformations introduce geometric nonlinearity. Therefore, we must take account their geometric nonlinearity in the analysis and find the equilibrated shape of cable structures. In this paper, to slove these problems, numerical procedures involving geometrical nonlinearity are introduced. They are applicable to general cable net, flexible transmission lines and suspended cable roof. These procedures are divided into two parts; one is to obtain the equilibrated shapes and stresses of the cable structures with uniform load by flexibility iteration method, the other is to analyse the equilibrated structures subjected to nodal external forces by nonlinear finite element method.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.13 no.5
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• pp.85-98
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• 1993

A method of analysis for the material and geometric nonlinear analysis of planar prestressed concrete cable-stayed bridges including the time-dependent effects due to load history, creep, shrinkage, aging of concrete and relaxation of prestress is described. The analysis procedure, based on the finite element method, is capable of predicting the response of these structures through elastic, cracking, inelastic and ultimate ranges. The nonlinear formulation for the description of motion is based on the updated Lagrangian approach. To account for the material nonlinearity, nonlinear stress-strain relationship and cracking of concrete, nonlinear stress-strain relationships of reinforcing steel, prestressing steel, and cable, including load reversal are given. Results from a numerical examples on ultimate analyses of cable-stayed bridges are presented to illustrate the analysis method.

• Journal of Aerospace System Engineering
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• v.17 no.1
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• pp.24-32
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• 2023

This paper studied HART II in descending flight using rotorcraft analysis code based on geometrically exact beam (GEB) model. The present GEB model expressed by a mixed variational formulation could capture the geometrically nonlinear behavior of the blade without arbitrary assumptions. In previous results, correlation of airloads with structural moments for HART II was not as good as blade deflections. However, in present results, predictions of airloads and structural loads are fairly correlated with measured data.

• Journal of Korean Society of Steel Construction
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• v.14 no.4
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• pp.489-497
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• 2002

Nonlinear behavior and large deformation cannot be analyzed using techniques based on linear theory. Nonetheless, they are emerging as gradually huge and complex structures. In addition, the optimum design of structure is necessary in the development of high-performance computation and numerical methods. as well as stricter design-criterion. Therefore, the structural problems in engineering that are limited to the linear region must be extended to the nonlinear region. Likewise, structural behavior must be accurately analyzed. In turn, this requires considering the expected problems beforehand. Only then can an efficient, economical, and optimized structure be designed. This paper presents the solution of the geometrical nonlinear problem of anisotropic cylindrical shell. The characteristics of the geometrical nonlinear behavior of anisotropic circular cylindrical shells may vary according to several causes. e.g., change of fibers, curvature in the circumferential direction, subtended angle, aspect, etc. Parametric studies were conducted to determine the effect of factors on the large deflection behavior of laminated shells, with interesting observations.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.28 no.5
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• pp.485-490
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• 2015

This paper presents development of a geometrically nonlinear triangular planar element including rotational degrees of freedom, based on the co-rotational(CR) formulation. The CR formulation is one of the efficient geometrically nonlinear formulations and it is based on the assumptions on small strain and large rotation. In this paper, modified CR formulation is suggested for the developemnt of a triangular planar element. The present development is validated regarding the static and time transient problems. The present results are compared with the results predicted by the previous researchers and those obtained by the existing commercial software.