• 제목/요약/키워드: critical buckling load

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The surface stress effects on the buckling analysis of porous microcomposite annular sandwich plate based on HSDT using Ritz method

  • Mohsen Emdadi;Mehdi Mohammadimehr;Borhan Rousta Navi
    • Computers and Concrete
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    • 제32권5호
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    • pp.439-454
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    • 2023
  • In this article, the surface stress effects on the buckling analysis of the annular sandwich plate is developed. The proposed plate is composed of two face layers made of carbon nanotubes (CNT) reinforced composite with assuming of fully bonded to functionally graded porous core. The generalized rule of the mixture is employed to predict the mechanical properties of the microcomposite sandwich plate. The derived potentials energy based on higher order shear deformation theory (HSDT) and modified couple stress theory (MCST) is solved by employing the Ritz method. An exact analytical solution is presented to calculate the critical buckling loads of the annular sandwich plate. The predicted results are validated by carrying out the comparison studies for the buckling analysis of annular plates with those obtained by other analytical and finite element methods. The effects of various parameters such as material length scale parameter, core thickness to total thickness ratio (hc/h), surface elastic constants based on surface stress effect, various boundary condition and porosity distributions, size of the internal pores (e0), Skempton coefficient and elastic foundation on the critical buckling load have been studied. The results can be served as benchmark data for future works and also in the design of materials science, injunction high-pressure micropipe connections, nanotechnology, and smart systems.

플레이트 거더교 지점부의 좌굴발생 원인분석 및 보강방안 수립 (Analysis of Buckling Causes and Establishment of Reinforcement Method for Support of Plate Girder Bridge)

  • 옥재호;임성순
    • 한국산학기술학회논문지
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    • 제20권11호
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    • pp.520-526
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    • 2019
  • 플레이트 거더교에서 I형은 매우 경제적인 단면으로 넓게 적용되고 있으며 지금까지 복합적층의 패널, 폐단면 리브로 보강된 곡판, 새로운 형태의 리브, 새로운 형식의 강박스거더 압축플랜지 개발 등의 좌굴거동에 대한 연구가 활발히 진행되었다. 하지만 이는 I형 거더의 복부판에서 발생한 국부좌굴의 원인을 정확하게 분석하는데 한계가 있었다. 따라서 본 논문에서는 실제 적용된 I형 거더의 복부판이 도로교설계기준에서 제시하는 최소두께 기준의 만족여부와 보강전과 후에 대하여 유한요소해석 프로그램 LUSAS 17.0을 사용하여 모델링하고 고정하중과 활하중에 대한 선형탄성 좌굴 해석을 수행 후 좌굴발생의 원인을 분석하였다. 보강 전은 1mode의 고유치(λ1) 값이 0.7025로 임계좌굴하중이 작용하중보다 작아 좌굴이 발생하였지만 보강 후는 거더 지점부의 복부판에 수직 및 수평보강재를 추가함에 따라 여기에 Nodal line이 형성되고 좌굴에 대한 저항강도가 증가하여 1mode의 고유치(λ1) 값이 1.5272로 좌굴하중에 대한 안정성을 확보한 것으로 분석되었다. 또한 지점부의 좌굴 흔적을 개선하기 위해 복부판의 일부에 덧댐판을 추가한 보강방안에 대한 좌굴해석 결과 1mode의 좌굴이 복부판의 지점부가 아닌 중앙부에서 발생하였고 고유치(λ1)값이 3.5299로 보강 후보다 2배 이상 커서 향후 지점부의 복부판 보강방안으로는 효과적일 것으로 기대된다.

Post-buckling of cylindrical shells with spiral stiffeners under elastic foundation

  • Shaterzadeh, Alireza;Foroutan, Kamran
    • Structural Engineering and Mechanics
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    • 제60권4호
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    • pp.615-631
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    • 2016
  • In this paper, an analytical method for the Post-buckling response of cylindrical shells with spiral stiffeners surrounded by an elastic medium subjected to external pressure is presented. The proposed model is based on two parameters elastic foundation Winkler and Pasternak. The material properties of the shell and stiffeners are assumed to be continuously graded in the thickness direction. According to the Von Karman nonlinear equations and the classical plate theory of shells, strain-displacement relations are obtained. The smeared stiffeners technique and Galerkin method is used to solve the nonlinear problem. To valid the formulations, comparisons are made with the available solutions for nonlinear static buckling of stiffened homogeneous and un-stiffened FGM cylindrical shells. The obtained results show the elastic foundation Winkler on the response of buckling is more effective than the elastic foundation Pasternak. Also the ceramic shells buckling strength higher than the metal shells and minimum critical buckling load is occurred, when both of the stiffeners have angle of thirty degrees.

Analytical study of buckling profile web stability

  • Taleb, Chems eddine;Ammari, Fatiha;Adman, Redouane
    • Structural Engineering and Mechanics
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    • 제53권1호
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    • pp.147-158
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    • 2015
  • Elements used in steel structures may be considered as an assembly of number of thin flat walls. Local buckling of these members can limit the buckling capacity of axial load resistance or flexural strength. We can avoid a premature failure, caused by effects of local buckling, by limiting the value of the wall slenderness which depend on its critical buckling stress. According to Eurocode 3, the buckling stress is calculated for an internal wall assuming that the latter is a simply supported plate on its contour. This assumption considers, without further requirement, that the two orthogonal walls to this wall are sufficiently rigid to constitute fixed supports to it. In this paper, we focus on webs of steel profiles that are internal walls delimited by flanges profiles. The objective is to determine, for a given web, flanges dimensions from which the latter can be considered as simple support for this web.

Hygrothermal effects on buckling of composite shell-experimental and FEM results

  • Biswal, Madhusmita;Sahu, Shishir Kr.;Asha, A.V.;Nanda, Namita
    • Steel and Composite Structures
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    • 제22권6호
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    • pp.1445-1463
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    • 2016
  • The effects of moisture and temperature on buckling of laminated composite cylindrical shell panels are investigated both numerically and experimentally. A quadratic isoparametric eight-noded shell element is used in the present analysis. First order shear deformation theory is used in the present finite element formulation for buckling analysis of shell panels subjected to hygrothermal loading. A program is developed using MATLAB for parametric study on the buckling of shell panels under hygrothermal field. Benchmark results on the critical loads of hygrothermally treated woven fiber glass/epoxy laminated composite cylindrical shell panels are obtained experimentally by using universal testing machine INSTRON 8862. The effects of curvature, lamination sequences, number of layers and aspect ratios on buckling of laminated composite cylindrical curved panels subjected to hygrothermal loading are considered. The results are presented showing the reduction in buckling load of laminated composite shells with the increase in temperature and moisture concentrations.

초기 불완전성을 고려한 공간 트러스의 분기좌굴과 라이즈-스팬 비에 따른 임계하중 특성 (Characteristics of Buckling Load and Bifurcation in Accordance with Rise-span Ratio of Space Truss Considering Initial Imperfection)

  • 이승재;손수덕
    • 한국강구조학회 논문집
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    • 제24권3호
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    • pp.337-348
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    • 2012
  • 본 연구는 초기조건에 민감한 공간 트러스를 대상으로 불완전성으로 인한 분기거동 및 불안정 특성에 대해서 연구하였으며, 접선강성행렬의 행렬식과 고유치해석으로 임계점과 좌굴하중을 구하였다. 고유모드의 민감성에 의한 불안정 현상을 고찰하기 위해서 2-자유절점공간 트러스와 스타 돔 및 3링 돔 모델을 예제로 채택하였으며, 라이즈-스팬 비 및 하중 파라메타에 따른 좌굴하중의 영향을 분석하였다. 2-자유절점 모델의 초기 형상불완전성에 따른 민감성은 고유모드에 따라 임계 후 평형경로가 바뀌었으며, 좌굴하중은 불완전 량의 증가에 따라 감소하는 결과를 얻었다. 예제에서 나타난 두 가지 민감한 좌굴패턴은 자유절점의 변위 위치를 살펴봄으로서 설명할 수 있었고, 형상 불완전성에 따른 거동은 비대칭 고유모드가 가장 큰 영향을 주었다. 민감한 고유모드는 단순화한 모델의 비신장 메커니즘 기저와 유사하였다. 스타 돔 모델은 라이즈-스팬 비가 높을수록 전체좌굴보다는 국부좌굴이 우세하며, 하중 파라메타 값이 클수록 평형경로 상에 분기점이 발생하였다. 또한 스타돔과 3링 모델의 좌굴하중은 각각 극한점 하중레벨의 약 50-70% 및 80-90%로 나타났다.

Strength and buckling of a sandwich beam with thin binding layers between faces and a metal foam core

  • Magnucki, Krzysztof;Jasion, Pawel;Szyc, Waclaw;Smyczynski, Mikolaj Jan
    • Steel and Composite Structures
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    • 제16권3호
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    • pp.325-337
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    • 2014
  • The strength and buckling problem of a five layer sandwich beam under axial compression or bending is presented. Two faces of the beam are thin aluminium sheets and the core is made of aluminium foam. Between the faces and the core there are two thin binding glue layers. In the paper a mathematical model of the field of displacements, which includes a share effect and a bending moment, is presented. The system of partial differential equations of equilibrium for the five layer sandwich beam is derived on the basis of the principle of stationary total potential energy. The equations are analytically solved and the critical load is obtained. For comparison reasons a finite element model of the beam is formulated. For the case of bended beam the static analysis has been performed to obtain the stress distribution across the height of the beam. For the axially compressed beam the buckling analysis was carried out to determine the buckling load and buckling shape. Moreover, experimental investigations are carried out for two beams. The comparison of the results obtained in the analytical and numerical (FEM) analysis is shown in graphs and figures. The main aim of the paper is to present an analytical model of the five layer beam and to compare the results of the theoretical, numerical and experimental analyses.

Prediction of the critical buckling load of SWCNT reinforced concrete cylindrical shell embedded in an elastic foundation

  • Timesli, Abdelaziz
    • Computers and Concrete
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    • 제26권1호
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    • pp.53-62
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    • 2020
  • Concrete is the most widely used substance in construction industry, so it's been required to improve its quality using new technologies. Nowadays, nanotechnology offers new frontiers for improving construction materials. In this paper, we study the stability analysis of the Single Walled Carbon Nanotubes (SWCNT) reinforced concrete cylindrical shell embedded in elastic foundation using the Donnell cylindrical shell theory. In this regard, we propose a new explicit analytical formula of the critical buckling load which takes into account the distribution of SWCNT reinforcement through the thickness of the concrete shell using the U, X, O and V forms and the elastic foundation using Winkler and Pasternak models. The rule of mixture is used to calculate the effective properties of the reinforced concrete cylindrical shell. The influence of diverse parameters on the stability behavior of the reinforced concrete shell is also discussed.

온도상승에 따른 H-형강 기둥의 내력에 관한 연구 (A Study on the Capacity of H-Shape Columns at Elevated Temperatures)

  • 구본율;장명웅;강문명
    • 한국공간구조학회논문집
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    • 제4권1호
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    • pp.87-95
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    • 2004
  • 본 논문은 화재시 온도상승에 따른 H-형강 기둥의 내력에 관한 연구이다. 주요 매개변수는 온도, 세장비와 하중비이다. 온도 상승시 강재의 물리적 특성은 EC3 Part1.2에 따랐다. 온도상승에 따른 국부좌굴의 임계온도는 재료의 항복강도와 판폭두께비가 클수록 더 낮아진다. 균등한 열을 받는 철골 기둥의 내혁 평가는 LRFD에 따른 축력과 강축 및 약축 모멘트에 대하여 고려하였다.

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Structural Optimization of a Thick-Walled Composite Multi-Cell Wing Box Using an Approximation Method

  • Kim, San-Hui;Kim, Pyung-Hwa;Kim, Myung-Jun;Park, Jung-sun
    • 항공우주시스템공학회지
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    • 제15권2호
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    • pp.1-9
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    • 2021
  • In this paper, a thickness compensation function is introduced to consider the shear deformation and warping effect resulting from increased thickness in the composite multi-cell wing box. The thickness compensation function is used to perform the structure optimization of the multi-cell. It is determined by minimizing the error of an analytical formula using solid mechanics and the Ritz method. It is used to define a structural performance prediction expression due to the increase in thickness. The parameter is defined by the number of spars and analyzed by the critical buckling load and the limited failure index as a response. Constraints in structural optimization are composed of displacements, torsional angles, the critical buckling load, and the failure index. The objective function is the mass, and its optimization is performed using a genetic algorithm.