• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2004년도 추계학술발표대회 논문집
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• pp.121-124
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• 2004

The purpose of this study is to define the optimized layer pattern of composite wind turbine blade by using a commercial FEM program and to perform the fatigue test of T-Bolt. FEM analysis is done by using a PATRAN and ABAQUS to get a information about stress distribution ,critical deformation shape and get a critical load factor in local buckling analysis. As a result of the linear and nonlinear structural analysis, layer pattern of blade was optimized. T-Bolt is a connecting part of wind turbine blade and rotor hub, therefore T-bolt is cirtical part of wind turbine blade. T-bolt fatigue test is conducted to get a information of life cycle of T-bolt. The test is done by using a hydraulic actuator system

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1998년도 가을 학술발표회 논문집
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• pp.208-215
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• 1998

A stability problems of isotropic shells under pure bending is investigated based on the classical shells theory. The governing equations of stability problem presented by Donnell and Love, are developed and the solutions for the cylindrical shells are obtained by using Galerkin method. Bending moment is applied at the ends of the cylindrical shell as a from of distributed load in the shape of sine curve. For the isotropic materials, the result of the general purpose structural analysis program based on the finite element method are compared with the critical moment obtained from the classical shell theories. The critical loads for the cylindrical shells with various geometry can not be evaluated with a simple equation. However, accurate solutions for the stability problems of cylindrical shells can be obtained through the equilibrium equation developed in the study.

• 한국강구조학회 논문집
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• 제29권1호
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• pp.13-24
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• 2017

사장교의 부재별 임계좌굴하중 산정에는 일반적으로 시스템 좌굴해석이 사용된다. 그러나 기존의 시스템 좌굴해석은 압축력이 미소한 부재에 대하여 과도하게 긴 유효좌굴길이를 산정하는 문제점을 내포하고 있다. 본 연구에서는 가상축력을 이용하여 강사장교 부재의 유효좌굴길이를 합리적으로 결정할 수 있는 좌굴해석 방법을 제안하였다. 또한, 수정된 유효접선탄성계수를 이용한 개선된 비탄성 좌굴해석방법을 제시하였다. 제안방법을 예제 사장교 모델에 적용하여 해석결과를 기존의 좌굴해석 방법과 비교 검증하였다. 검증결과, 제안된 방법은 강사장교 거더와 주탑의 유효좌굴길이를 합리적으로 예측할 수 있었다. 그리고 거더와 주탑에 일반강재 대신 HSB800 강재를 적용하였을 경우, 가상축력을 고려하지 않은 제안된 비탄성 좌굴해석에서는 유효좌굴길이가 축력이 작은 부분에서 약간 감소하였으나, 가상축력을 적용한 제안된 비탄성 좌굴해석에서는 유효좌굴길이의 변화가 거의 나타나지 않았다.

• Structural Engineering and Mechanics
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• 제58권6호
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• pp.949-966
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• 2016

The second order analysis taking place due to non-linear behavior of the structures under the mechanical and geometric factors through implementing exact and approximate methods is an indispensible issue in the analysis of such structures. Among the exact methods is the slope-deflection method that due to its simplicity and efficiency of its relationships has always been in consideration. By solving the differential equations of the modified slope-deflection method in which the effect of axial compressive force is considered, the stiffness matrix including trigonometric entries would be obtained. The complexity of computations with trigonometric functions causes replacement with their Maclaurin expansion. In most cases only the first two terms of this expansion are used but to obtain more accurate results, more elements are needed. In this paper, the effect of utilizing higher order terms of Maclaurin expansion on reducing the number of required elements and attaining more rapid convergence with less error is investigated for the Bernoulli beam with various boundary conditions. The results indicate that when using only one element along the beam length, utilizing higher order terms in Maclaurin expansion would reduce the relative error in determining the critical buckling load and kinematic parameters in the second order analysis.

• Steel and Composite Structures
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• 제35권3호
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• pp.385-404
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• 2020

Since the scaffold is composed of modular members, the total height of multi-story scaffolds does not often meet with the headroom of construction buildings. At this time, other supporting members need to be set up on the top of scaffolds. However, the mechanical behaviors of the combined system of scaffolds and other supporting members have seldom been discussed. This study explores the stability of the combined system of scaffolds and shores. The loading tests conducted in the laboratory show that the critical load of the combined system of two-story scaffolds and wooden shores is about half that of the three-story scaffold system with the same height. In the failure of both the "scaffold system" and the "combined system of scaffolds and shores' after loading, the deformation mainly occurs in the in-plane direction of the scaffold. The outdoor loading test shows that no failure occurs on any members when the combined system fails. Instead, the whole system buckles and then collapses. In addition, the top formwork of the combined system can achieve the effect of lateral support reinforcement with small lateral support forces in the outdoor loading test. This study proposes the preliminary design guidelines for the scaffolding structural design.

• 한국항해항만학회지
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• 제31권3호
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• pp.271-279
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• 2007

선체구조는 기본적으로 판부재의 조합으로 이루어져 있으며, 이러한 판부재의 하중분담 능력 혹은 최종강도 평가는 선체구조의 합리적인 설계 및 구조의 안정성 평가에 있어서는 아주 중요하다. 또한, 선체구조를 구성하고 있는 구조요소들은 작용외력에 대하여 개별적으로 작용하지 않으며 전체적으로 연속거동을 하게 된다. 실제 선박에서의 붕괴형태 중 한가지는 종방향 굽휨에 의해서 갑판 혹은 선저부에 좌굴 및 소성붕괴이다. 그래서, 합리적인 설계에서는 이러한 급작스런 붕괴형태를 방지하기 위하여 좌굴 및 소성붕괴 거동을 파악하는 것이 아주 중요하며, 실제 선박에서는 갑판부와 선저부에서는 하중분담 능력을 증가시키기 위하여 여러개의 종보강재를 가진 보강판 구조의 설계를 하게 된다. 본 연구에서는 선체 판넬구조의 모델링 방법에 따른 최종강도 거동의 차이를 분석하여, 합리적인 모델링영역을 규명하고자 한다. 사용된 해석 모델은 실제 상선의 이중저구조에서 사용되는 판넬에서 채택하였으며 유한요소해석 모델링 시 3가지 단면형상에 대해 각각 6가지 서로 다른 해석모델을 적용하였으며, 이때 보강재의 단면형상을 변화하였다. 본 연구의 목적은 압축하중이 작용하는 선체 보강판구조에서 해석영역에 대한 좌굴 및 최종강도 거동의 특성을 분석하였다.

• Steel and Composite Structures
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• 제5권2_3호
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• pp.181-192
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• 2005

The effective length method for flexural (column) buckling has been used for many decades but its use is somewhat limited in various contemporary design codes to moderately slender structures with elastic critical load factor (${\lambda}_{cr}$) less than 3 to 5. In pace with the use of higher grade steel in recent years, the influence of buckling in axial buckling resistance of a column becomes more important and the over-simplified assumption of effective length factor can lead to an unsafe, an uneconomical or a both unsafe and uneconomical solution when some members are over-designed while key elements are under-designed. Effective length should not normally be taken as the distance between nodes multiplied by an arbitrary factor like 0.85, 1.0, 2.0 etc. Further, the classification of non-sway and sway-sensitive frames makes the conventional design procedure tedious to use and, more importantly, limited to simple regular frames. This paper describes the practical use of second-order analysis with section capacity check allowing for $P-{\delta}$ and $P-{\Delta}$ effects together with member and system imperfections. Most commercial software considers only the $P-{\Delta}$ effect, but not member and frame imperfections nor $P-{\delta}$ effect, and engineers must be very careful in their uses. A verification problem is also given for validation of software for this type of powerful second-order analysis and design. It is a trend for popular and advanced national design codes in using the second-order analysis as a norm for analysis and design of steel structures while linear analysis may only be used in very simple structures.

• 한국정밀공학회지
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• 제23권6호
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• pp.136-142
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• 2006

Optimization of the aircraft panel assembly constructed by skin and stringers is investigated. For the design of panel assembly of the aircraft structure, it is necessary to determine the best shape of the stringer which accomplishes lowest weight under the condition of no instability. A panel assembly can fail in a variety of instability modes under compression. Overall modes of flexure or torsion can occur and these can interact in a combined flexural/torsion mode. Flexure and torsion can occur symmetrically or anti-symmetrically. Local instabilities can also occur. The local instabilities considered in this paper are buckling of the free and attached flanges, the stiffener web and the inter-rivet buckling. A program is developed to find out critical load for each instability mode at the specific stringer shape. Based on the developed program, optimization is performed to find optimum stringer shape. The developed instability analysis program is not adequate for sensitivity analysis, therefore RSM (Response Surface Method) is utilized instead to model weight and instability constraints. Since the problem has many local minimum, Genetic algorithm is utilized to find global optimum.

• 복합신소재구조학회 논문집
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• 제1권1호
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• pp.27-33
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• 2010

Static analyses and buckling analyses were carried out for buried GFRP pipes by using finite element method. Vehicle loads, vertical and lateral soil pressures were considered as external loads, and supplying water pressure was considered as an internal load. Nine types of the factory-manufactured GFRP pipes were analyzed. Their maximum stresses and displacements were compared with the limit displacements and ultimate stress. Additionally, stress analysis on an enhanced flange, which was designed to reduce stress concentration, was performed. A cantilever analysis was carried out to know the maximum stress on the neck of the flange, which is the critical part. And a static analysis was carried for the buried flange. The test results showed that GFRP pipes were safe and stable against the external loads. And they showed that the enhanced flange decreased about 35% of the stress concentration.

• Computers and Concrete
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• 제26권5호
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• pp.439-450
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• 2020

In this research, bending and buckling analyses of porous functionally graded (FG) plate under mechanical load are presented. The properties of the FG plate vary gradually across the thickness according to power-law and exponential functions. The material imperfection is considered to vary depending to a logarithmic function. The plate is modeled by a refined trigonometric shear deformation theory where the use of the shear correction factor is unnecessary. The governing equations of the FG plate are derived via virtual work principle and resolved via Navier solutions. The accuracy of the present model is checked by comparing the obtained results with those found in the literature. The various effects influencing the stresses, displacements and critical buckling loads of the plate are also examined and discussed in detail.