• 제목/요약/키워드: partial buckling

검색결과 58건 처리시간 0.023초

일축압축을 받는 직교로 보강된 판의 좌굴강도 (Buckling Strength of Orthogonally Stiffened Steel Plates under Uniaxial Compression)

  • 최동호;장동일;최항용
    • 한국강구조학회 논문집
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    • 제10권4호통권37호
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    • pp.731-740
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    • 1998
  • 직교로 보강된 판은 효율적인 하중분배능력과 좌굴안정성 때문에 장대교량의 강상판으로 사용되고 있다. 본 연구에서는 일축압축을 받는 직교로 보강된 판의 좌굴강도를 해석적 방법으로 추정하였다. 판이론을 사용하여 전체좌굴 및 부분좌굴과 같은 여러 모드에서의 좌굴응력식을 유도하고, 좌굴강도에 대한 횡리브와 종리브의 강성과 개수 등의 효과를 보이기 위하여 매개변수해석을 수행하였다. 정량적인 해석을 통해 종리브와 횡리브의 강성과 간격의 영향을 보였다.

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Accurate buckling analysis of rectangular thin plates by double finite sine integral transform method

  • Ullah, Salamat;Zhang, Jinghui;Zhong, Yang
    • Structural Engineering and Mechanics
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    • 제72권4호
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    • pp.491-502
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    • 2019
  • This paper explores the analytical buckling solution of rectangular thin plates by the finite integral transform method. Although several analytical and numerical developments have been made, a benchmark analytical solution is still very few due to the mathematical complexity of solving high order partial differential equations. In solution procedure, the governing high order partial differential equation with specified boundary conditions is converted into a system of linear algebraic equations and the analytical solution is obtained classically. The primary advantage of the present method is its simplicity and generality and does not need to pre-determine the deflection function which makes the solving procedure much reasonable. Another advantage of the method is that the analytical solutions obtained converge rapidly due to utilization of the sum functions. The application of the method is extensive and can also handle moderately thick and thick elastic plates as well as bending and vibration problems. The present results are validated by extensive numerical comparison with the FEA using (ABAQUS) software and the existing analytical solutions which show satisfactory agreement.

Thermal nonlinear dynamic and stability of carbon nanotube-reinforced composite beams

  • M. Alimoradzadeh;S.D. Akbas
    • Steel and Composite Structures
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    • 제46권5호
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    • pp.637-647
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    • 2023
  • Nonlinear free vibration and stability responses of a carbon nanotube reinforced composite beam under temperature rising are investigated in this paper. The material of the beam is considered as a polymeric matrix by reinforced the single-walled carbon nanotubes according to different distributions with temperature-dependent physical properties. With using the Hamilton's principle, the governing nonlinear partial differential equation is derived based on the Euler-Bernoulli beam theory. In the nonlinear kinematic assumption, the Von Kármán nonlinearity is used. The Galerkin's decomposition technique is utilized to discretize the governing nonlinear partial differential equation to nonlinear ordinary differential equation and then is solved by using of multiple time scale method. The critical buckling temperatures, the nonlinear natural frequencies and the nonlinear free response of the system is obtained. The effect of different patterns of reinforcement on the critical buckling temperature, nonlinear natural frequency, nonlinear free response and phase plane trajectory of the carbon nanotube reinforced composite beam investigated with temperature-dependent physical property.

Research Advances on Tension Buckling Behaviour of Aerospace Structures: A Review

  • Datta, Prosun Kumar;Biswas, Sauvik
    • International Journal of Aeronautical and Space Sciences
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    • 제12권1호
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    • pp.1-15
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    • 2011
  • This paper reviews most of the research done in the field of tensile buckling characteristics pertaining to aerospace structural elements with special attention to local buckling and parametric excitation due to periodic loading on plate and shell elements. The concepts of buckling in aerospace structures appear as the result of the application of a global compressive applied load or shear load. A less usual situation is the case, in which a global tensile stress creates buckling instability and the formation of complex spatial buckling pattern. In contrast to the case of a pure compression or shear load, here the applied macroscopic load has no compressive component and is thus globally stabilizing. The instability stems from a local compressive stress induced by the presence of a defect, such as a crack or a hole, due to partial or non-uniform applied load at the far end. This is referred to as tensile buckling. This paper discusses all aspects of tensile buckling, theoretical and experimental. Its far reaching applications causing local instability in aerospace structural components are discussed. The important effects on dynamic stability behaviour under locally induced periodic compression have been identified and influences of various parameters are discussed. Experimental results on simple and combination resonance characteristics on plate structures due to tensile buckling effects are elaborated.

Effect of shear deformation on the critical buckling of multi-step bars

  • Li, Q.S.
    • Structural Engineering and Mechanics
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    • 제15권1호
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    • pp.71-81
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    • 2003
  • The governing differential equation for buckling of a one-step bar with the effect of shear deformation is established and its exact solution is obtained. Then, the exact solution is used to derive the eigenvalue equation of a multi-step bar. The new exact approach combining the transfer matrix method and the closed form solution of one step bar is presented. The proposed methods is convenient for solving the entire and partial buckling of one-step and multi-step bars with various end conditions, with or without shear deformation effect, subjected to concentrated axial loads. A numerical example is given explaining the proposed procedure and investigating the effect of shear deformation on the critical buckling force of a multi-step bar.

Nonlinear Dynamic Buckling Behavior of a Partial Spacer Grid Assembly

  • Yoon, Kyung-Ho;Kang, Heung-Seok;Kim, Hyung-Kyu;Song, Kee-Nam;Jung, Yeon-Ho
    • Nuclear Engineering and Technology
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    • 제33권1호
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    • pp.93-101
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    • 2001
  • The spacer grid is one of the main structural components in the fuel assembly, which supports the fuel rods, guides cooling water, and protects the system from an external impact load, such as earthquakes. Therefore, the mechanical and structural properties of the spacer grids must be extensively examined while designing them. In this paper, a numerical method for predicting the buckling strength of spacer grids is presented. Numerical analyses on the buckling behavior of the spacer grids are performed for a various array of sizes of the grids considering that the spacer grid is an assembled structure with thin-walled plates and imposing proper boundary conditions by nonlinear dynamic finite element method using ABAQUS/Explicit. Buckling tests on several numbers of specimens of the spacer grid were also carried out in order to compare the results between the test and the simulation result. The drop test is accomplished by dropping a carriage on the specimen at a pre-determined position. From this test, the specimens are buckled only at the uppermost and the lowermost layer among the multi-cells, which is similar to the local buckling at the weakest point of the grid structure. The simulated results also similarly predicted the local buckling phenomena and were found to give good correspondence with the experimental values for the thin-walled grid structures.

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석고보드와 결합된 강재 샛기둥 패널의 부분 합성거동 (Partial Composite Action of Gypsum-Sheathed Cold-Formed Steel Wall Stud Panels)

  • 이영기
    • 한국강구조학회 논문집
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    • 제13권4호
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    • pp.373-380
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    • 2001
  • 본 연구에서는 벽 패널의 부분 합성거동 해석에 대하여 거론한다. 기 발표된 목재 바닥 시스템으로부터 유도된 처짐공식을 소개하고, 이 공식을 적용하여 석고보드와 강재 샛기둥으로 결합된 합성벽 패널의 중앙지점 처짐값을 산정한다. 나사연결부의 불완전성(미끄럼), 국부좌굴, 샛기둥 복부의 개구부, 그리고 인접 석고보드간의 불연속으로 야기 될 수 있는 강성의 감소 등을 처짐공식에 적절히 반영하는데 그 목적을 두었다. 적용된 처짐공식으로 산정된 처짐 기대치와 실험 관측치간의 비교에서는, 나사연결부의 상한 강성치를 사용한 처짐 기대치가 실험 관측치와 가장 근접한 결과를 보였다.

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Analytical and experimental postbuckling of conditioned cables

  • Rivierre, L.;Polit, O.;Billoet, J.L.
    • Structural Engineering and Mechanics
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    • 제12권6호
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    • pp.595-614
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    • 2001
  • This paper studies the behaviour of a homogeneous cable in a horizontal rigid duct and loaded by an axial compressive force. This behaviour is characterized by spatial buckling modes, named sinusoidal and helical, due to friction and total or partial cable locking. The evaluation of critical buckling loads involved by drilling technology has been studied by many authors. This work presents a new formulation, taking the friction effects into account, for the transmission of the axial load during the postbuckling process. New analytical expressions of pitches in both buckling cases are also given. A life-sized bench is presented, which permits to study the laying of optical fiber cables by squeezing them into an underground duct. Finally, analytical solutions are compared with experimental tests and finite element simulations.

Conventional problem solving on the linear and nonlinear buckling of truncated conical functionally graded imperfect micro-tubes

  • Linyun, Zhou
    • Advances in nano research
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    • 제13권6호
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    • pp.545-559
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    • 2022
  • This paper studies the buckling response of nonuniform functionally graded micro-sized tubes according to the high-order tube theory (HOTT) and classical beam theory (CBT) in addition to nonlocal strain gradient theory. The microtube is made of axially functionally graded material (AFGM). Both inner and outer tube radiuses are changed along the tube length; the microtube is the truncated conical type of tube. The nonlinear partial differential (PD) the formulations are obtained on the basis of the energy conservation method. Then, the linear and nonlinear results are computed via a powerful numerical approach. Finally, the impact of various parameters on the stability of axially functionally graded (AFG) microtube regarding the buckling analysis is discussed.