• 제목/요약/키워드: Partial Edge Loading

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제형파형강판의 지압 거동에 영향을 미치는 기하학적 인자에 관한 연구 (A Study on the Geometric Parameters that Influence the Trapezoidally Corrugated Webs Under Partial Edge Loading)

  • 최용주;이종원;신철호;이학은
    • 한국강구조학회 논문집
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    • 제18권1호
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    • pp.81-91
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    • 2006
  • 파형 강판은 파형 형상으로 가공한 강판으로 교량, 건축물, 암거 등의 구조물에 많이 사용된다. 파형강판을 이용한 거더의 구조물 적용시 국부적인 면내 압축하중에 의해 크리플링현상이 발생할 수 있는데 높은 면외방향의 강성을 갖는 파형강판의 특성 때문에 보강재를 사용하지 않는 경우가 많이 있고 파형형상에 따라 지압하중의 경계조건이 달라진다. 몇 연구자들이 제형파형강판의 지압강도에 대한 연구를 하였으나 파형형상이 지압강도에 미치는 영향이 크게 고려되지 않았다. 따라서 본 연구에서는 이에 따른 영향을 유한 요소해석법을 통하여 여러 가지 파형형상에 대한 변수해석을 하고 지압강도를 복부판 내하력과 플랜지 내하력으로 나누어 파형 형상과 지압강도와의 상관관계를 파악하였다.

Instability and vibration analyses of FG cylindrical panels under parabolic axial compressions

  • Kumar, Rajesh;Dey, Tanish;Panda, Sarat K.
    • Steel and Composite Structures
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    • 제31권2호
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    • pp.187-199
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    • 2019
  • This paper presents the semi-analytical development of the dynamic instability behavior and the dynamic response of functionally graded (FG) cylindrical shallow shell panel subjected to different type of periodic axial compression. First, in prebuckling analysis, the stresses distribution within the panels are determined for respective loading type and these stresses are used to study the dynamic instability behavior and the dynamic response. The prebuckling stresses within the shell panel are the same as applied in-plane edge loading for the case of uniform and linearly varying loadings. However, this is not true for the case of parabolic loadings. The parabolic edge loading produces all the stresses (${\sigma}_{xx}$, ${\sigma}_{yy}$ and ${\tau}_{xy}$) within the FG cylindrical panel. These stresses are evaluated by minimizing the membrane energy via Ritz method. Using these stresses the partial differential equations of FG cylindrical panel are formulated by applying Hamilton's principal assuming higher order shear deformation theory (HSDT) and von-$K{\acute{a}}rm{\acute{a}}n$ non-linearity. The non-linear governing partial differential equations are converted into a set of Mathieu-Hill equations via Galerkin's method. Bolotin method is adopted to trace the boundaries of instability regions. The linear and non-linear dynamic responses in stable and unstable region are plotted to know the characteristics of instability regions of FG cylindrical panel. Moreover, the non-linear frequency-amplitude responses are obtained using Incremental Harmonic Balance (IHB) method.

Axisymmetric large deflection analysis of fully and partially loaded shallow spherical shells

  • Altekin, Murat;Yukseler, Receb F.
    • Structural Engineering and Mechanics
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    • 제47권4호
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    • pp.559-573
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    • 2013
  • Geometrically non-linear axisymmetric bending of a shallow spherical shell with a clamped or a simply supported edge under axisymmetric load was investigated numerically. The partial load was introduced by the Heaviside step function, and the solution was obtained by the finite difference and the Newton-Raphson methods. The thickness of the shell was considered to be uniform and the material was assumed to be homogeneous and isotropic. Sensitivity analysis was made for three geometrical parameters. The accuracy of the algorithm was checked by comparing the central deflection, the radial membrane stress at the edge, or the transverse shear force with the solutions of plates and shells in the literature and good agreement was obtained. The main findings of the study can be outlined as follows: (i) If the shell is fully loaded the central deflection of a clamped shell is larger than that of a simply supported shell provided that the shell is not very shallow, (ii) if the shell is partially loaded the central deflection of the shell is sensitive to the parameters of thickness, depth, and partial loading but the influence of the boundary conditions is negligible.

부분입사형 초음속 터빈 익렬내 유동 특성에 관한 수치적 연구 (A Numerical Analysis on the Flow Characteristics within Blades of A Partial Admission Supersonic Turbine)

  • 신봉근;조종재;정수인;김귀순;이은석
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1738-1743
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    • 2004
  • Turbo-pump system, an essential component of liquid rockets and induced weapons, adopts a partial admission axial turbine which drives pump. And the turbine of a turbo-pump system is usually operated at supersonic condition due to its high loading chracteristics. Therefore, reseaches about flow and performance characteristics of a partial admission supersonic turbine must be preceeded to progress the aerospace and defense industries as well as the development of turbo-pump systems. In this study, flow characterisitics within blades of the partial admission supersonic turbine are numerically investigated by using Fine Turbo, a commercial CFD Code. Before performing the numercial analyses, to verify accuracy of the numerical result computed by Fine Turbo, I performed the comparison between the numerical results with J.J.Cho' experimental results. It is found that the numerical results show good agreement with the experimental results. Computations about the partial admission supersonic turbine have been performed to investigate flow characteristics including shock patterns. It is also found that the flow and performance of partial admission supersonic turbine are largely depend on shocks ocurred in the nozzle and at the leading edge of blades, expansion or compression at exit of nozzle and separations occurred in passage.

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A review of effects of partial dynamic loading on dynamic response of nonlocal functionally graded material beams

  • Ahmed, Ridha A.;Fenjan, Raad M.;Hamad, Luay Badr;Faleh, Nadhim M.
    • Advances in materials Research
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    • 제9권1호
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    • pp.33-48
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    • 2020
  • With the use of differential quadrature method (DQM), forced vibrations and resonance frequency analysis of functionally graded (FG) nano-size beams rested on elastic substrate have been studied utilizing a shear deformation refined beam theory which contains shear deformations influence needless of any correction coefficient. The nano-size beam is exposed to uniformly-type dynamical loads having partial length. The two parameters elastic substrate is consist of linear springs as well as shear coefficient. Gradation of each material property for nano-size beam has been defined in the context of Mori-Tanaka scheme. Governing equations for embedded refined FG nano-size beams exposed to dynamical load have been achieved by utilizing Eringen's nonlocal differential law and Hamilton's rule. Derived equations have solved via DQM based on simply supported-simply supported edge condition. It will be shown that forced vibrations properties and resonance frequency of embedded FG nano-size beam are prominently affected by material gradation, nonlocal field, substrate coefficients and load factors.

강한 지진 하중하에서 강재 교각의 손상 거동 연구 (A Study on Damage Process Analysis for Steel Pier Subjected to Seismic Excitation)

  • 박연수;박근구;박선준
    • 한국강구조학회 논문집
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    • 제12권3호통권46호
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    • pp.251-258
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    • 2000
  • 강구조물과 부재들의 지진 손상도 평가법에 새롭게 접근하기 위하여 강한 지진하중을 받는 강재 교각에 대해 수치해석을 수행하였다. 새로운 손상도 평가법에서 파괴 상태에 대한 기준은 지진하중이 재하되는 동안에 응력집중이 가장 심한 단면의 한 부분에서 누적소성변형율의 값이 90%에 이르게 되는 때를 의미한다. 단주기 특성의 지진하중에 대해서는 소성변형율의 누적에 의한 국부좌굴 파괴보다는 허용변위를 초과하는 전체좌굴에 의한 파괴가 지배적인 것으로 밝혀졌다. 장주기 특성의 지진하중에 대해서는 소성변형율이 강재교각 하부의 모서리 부분 요소에 누적되면서 누적 소성변형율에 의한 국부좌굴로 파괴되는 결과를 보였다.

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