• 제목/요약/키워드: uniform loads

검색결과 277건 처리시간 0.207초

쉘 구조물의 경계적분법 (A Boundary Integral Method for Elastic Shallow Shell)

  • 김진우
    • 한국군사과학기술학회지
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    • 제7권3호
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    • pp.157-164
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    • 2004
  • This is a boundary integral formulation for elastic shallow shell structures subjected to both membrane and bending loads. Fundamental solutions for shell actions are determined from the plate solutions and, finally the corresponding kernel functions for shell BIEs can be constructed. It is illustrated by solving an example of uniform load of spherical cap.

Closest Open Location Rule in AS/RS

  • Park, Byung-Chun
    • 대한산업공학회지
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    • 제13권2호
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    • pp.87-95
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    • 1987
  • This article deals with the expected travel distances under Closest Open Location rule. In this paper it is shown that uniform distribution assumption over a rack, which is usually used when modeling randomized storage, is not valid under COL rule, where arrival loads follow Poisson process and duration times are independent of each other and have finite mean. We give both exact and approximate methods for the expected travel distances. Warehouse sizing problem is also included.

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Forced vibration of nanorods using nonlocal elasticity

  • Aydogdu, Metin;Arda, Mustafa
    • Advances in nano research
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    • 제4권4호
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    • pp.265-279
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    • 2016
  • Present study interests with the longitudinal forced vibration of nanorods. The nonlocal elasticity theory of Eringen is used in modeling of nanorods. Uniform, linear and sinusoidal axial loads are considered. Dynamic displacements are obtained for nanorods with different geometrical properties, boundary conditions and nonlocal parameters. The nonlocal effect increases dynamic displacement and frequency when compared with local elasticity theory. Present results can be useful for modeling of the axial nanomotors and nanoelectromechanical systems.

평판의 균일압축에 의한 좌굴현상에 관한 연구 (A Study on Buckling of Plate under Uniform Compressive Stress)

  • 김창옥
    • 대한기계학회논문집
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    • 제15권3호
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    • pp.1044-1056
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    • 1991
  • 본 연구에서는 균일압축력을 받으며 네변이 단순지지된 비균일 두께를 가진 평판의 좌굴응력을 Rayleigh-Ritz방법으로 해석하여 평판두께를 적절히 분포함으로써 동일한 평판중량으로 더 큰 좌굴하중을 얻을 수 있음을 보이며 또한 동일한 문제를 NASTRAN프로그램을 사용하여 해석함으로써 그 정확도를 입증한다.

굴착기에서의 리퍼의 형상에 따른 구조적 내구성 연구 (A Study on Structural Durability due to the Configuration of Ripper at Excavator)

  • 강민제;조재웅
    • 한국융합학회논문지
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    • 제5권2호
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    • pp.13-18
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    • 2014
  • 본 연구에서는 굴착기에서의 리퍼의 형상에 따른 구조 및 진동, 피로해석을 하였다. 2가지의 모델들 모두, 작업장치의 바디와 이어지는 축에서 최대 응력이 발생하였고 최대 변형량은 직접작업부에서 발생하였다. Model 1이 Model 2 보다 내구성면에서 구조적으로 더 안정적이라고 사료된다. 불규칙 피로 하중들 중에서는 하중의 변화가 극심한 'SAE bracket history'의 경우가 대체적으로 가장 불안정한 경향을 보이고 있고, 비교적 하중의 변화가 완만한 'Sample history'의 경우가 가장 안정함을 보이고 있다. 본 연구의 결과를 종합하여 굴착기에서의 리퍼의 설계에 응용한다면, 그 파손 방지 및 내구성을 검토하여 그 설계에 유용하게 활용될 것으로 사료된다.

실지진하중을 이용한 포화사질토의 액상화 저항강도에 관한 실험적 연구 (An Experimental Study for the Liquefaction Resistance Strength of Saturated Sand Using Real Earthquake Loading)

  • 심재욱;박근보;최재순;김수일
    • 한국지반공학회논문집
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    • 제18권4호
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    • pp.329-337
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    • 2002
  • 최근까지 지반의 액상화 저항강도를 산정하기 위한 실내시험의 대부분은 실지진하중을 재하하기보다는 Seed와 Idriss(1975)가 제안한 등가전단응력 개념에 기초하여 지진이 발생시키는 최대전단응력의 65%를 최대진폭으로 한 정현하중을 반복재하시켜왔다. 이러한 정현하중이 정확하게 실제 지반에 작용하는 불규칙한 지진력을 모사하고 있다고 볼 수 없으나, 시험상의 편의성으로 인해 현재까지도 이용이 빈번한 실정이다. 본 연구에서는 실제 지진하중 하에서 포화 사질토의 거동변화를 규명하고자 정현하중이 아닌 불규칙한 지진하중을 이용한 실험적 연구를 수행하였다. 다양한 지진규모의 실지진 시간이력을 진동하중으로 작용시킨 진동삼축시험을 통해 지진규모 및 지속시간의 변화에 따른 포화사질토의 동적 특성을 실험적으로 규명하고 기존의 등가전단응력 개념에 기초한 액상화 저항강도와 비교분석하였다. 또한, 중약진 지진대로 구분되는 국내 실정을 고려하여 다양한 지진규모에 적용가능한 수정계수를 제시하고 이를 기존의 연구결과와 비교분석하였다.

Collapse Initiation and Mechanisms for a Generic Multi-storey Steel Frame Subjected to Uniform and Travelling Fires

  • Rackauskaite, Egle;Kotsovinos, Panagiotis;Lange, David;Rein, Guillermo
    • 국제초고층학회논문집
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    • 제10권4호
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    • pp.265-283
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    • 2021
  • To ensure that fire induced collapse of a building is prevented it is important to understand the sequence of events that can lead to this event. In this paper, the initiation of collapse mechanisms of generic a multi-storey steel frame subjected to vertical and horizontal travelling fires are analysed computationally by tracking the formation of plastic hinges in the frame and generation of fire induced loads. Both uniform and travelling fires are considered. In total 58 different cases are analysed using finite element software LS-DYNA. For the frame examined with a simple and generic structural arrangement and higher applied fire protection to the columns, the results indicate that collapse mechanisms for singe floor and multiple floor fires can be each split into two main groups. For single floor fires (taking place in the upper floors of the frame (Group S1)), collapse is initiated by the pull-in of external columns when heated beams in end bays go into catenary action. For single floor fires occurring on the lower floors(Group S2), failure is initiated (i.e. ultimate strain of the material is exceeded) after the local beam collapse. Failure in both groups for single floor fires is governed by the generation of high loads due to restrained thermal expansion and the loss of material strength. For multiple floor fires with a low number of fire floors (1 to 3) - Group M1, failure is dominated by the loss of material strength and collapse is mainly initiated by the pull-in of external columns. For the cases with a larger number of fire floors (5 to 10) - Group M2, failure is dominated by thermal expansion and collapse is mainly initiated by swaying of the frame to the side of fire origin. The results show that for the investigated frame initiation of collapse mechanisms are affected by the fire type, the number of fire floors, and the location of the fire floor. The findings of this study could be of use to designers of buildings when developing fire protection strategies for steel framed buildings where the potential for a multifloor fire exists.

Optimum arrangement of stiffener on the buckling behaviour of stiffened composite panels with reinforced elliptical cutouts subjected to non-uniform edge load

  • Kalgutkar, Akshay Prakash;Banerjee, Sauvik;Rajanna, T.
    • Steel and Composite Structures
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    • 제42권4호
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    • pp.427-446
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    • 2022
  • Cutouts in the beams or plates are often unavoidable due to inspection, maintenance, ventilation, structural aesthetics purpose, and sometimes to lighten the structures. Therefore, there will be a substantial reduction in the strength of the structure due to the introduction of the cutouts. However, these cutouts can be reinforced with the different patterns of ribs (stiffener) to enhance the strength of the structure. The present study highlights the influence of the elliptical cutout reinforced with a different pattern of ribs on the stability performance of such stiffened composite panels subjected to non-uniform edge loads by employing the Finite element (FE) technique. In the present formulation, a 9-noded heterosis element is used to model the skin, and a 3-noded isoparametric beam element is used to simulate the rib that is attached around a cutout in different patterns. The displacement compatibility condition is employed between the plate and stiffener, and arbitrary orientations are taken care by introducing respective transformation matrices. The effect of shear deformation and rotary inertia are incorporated in the formulation. A new mesh configuration is developed to house the attached ribs around an elliptical cutout with different patterns. Initially, a study is performed on the panels with different stiffener schemes for various ply orientations and for different stiffener depth to width ratios (ds/bs) to determine an optimal stiffener configuration. Further, various parametric studies are conducted on an obtained optimal stiffened panel to understand the effect of cutout size, cutout orientation, panel aspect ratio, and boundary conditions. Finally, from the analysis, it can be observed that the arrangement of the stiffener attached to a panel has a major impact on the buckling capacity of the stiffened panel. The stiffener's depth to width ratio also significantly influences the buckling characteristic.

임의분포 사하중에 정적변위를 갖는 변단면 보의 자유진동 (Free Vibrations of Arbitrary Tapered Beams with Static Deflections due to Arbitrary Distributed Dead Loads)

  • 이병구;이용
    • 한국농공학회지
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    • 제38권3호
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    • pp.50-57
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    • 1996
  • A numerical method is presented to obtain the natural frequencies and mode shapes of the arbitrary tapered beams with static deflection due to arbitrary distributed dead loads. The differential equation governing free vibration of such beams is derived and solved numerically. The double integration method using the trapezoidal rule is used to solve the static behaviour of beams loaded arbitrary distributed dead load. Also, the Improved Euler method and the determinant search method are used to integrate the differential equation subjected to the boundary conditions and to determine the natural frequencies of the beams, respectively. In the numerical examples, the various geometries of the beams are considered : (1) linearly tapered beams as the arbitrary variable cross-section, (2) the triangular, sinusoidal and uniform loads as the arbitrary distributed dead loads and (3) the hinged-hinged, clamped-clamped and hinged-clamped ends as the end constraints. All numerical results are shown as the non-dimensional forms of the system parameters. The lowest three natural frequencies versus load parameter, slenderness ratio and section ratio are reported in figures. And for the comparison purpose, the typical mode shapes with and without the effects of static deflection are presented in the figure. According to the numerical results obtained in this analysis, the following conclusions may be drawn : (1) the natural frequencies increase when the effects of static deflections are included, (2) the effects are larger at the lower modes than the higher ones and (3) it should be betteF to include the effect of static deflection for calculating the frequencies when the beams are supported by both hinged ends or one hinged end.

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Full-scale tests and finite element analysis of arched corrugated steel roof under static loads

  • Wang, X.P.;Jiang, C.R.;Li, G.Q.;Wang, S.Y.
    • Steel and Composite Structures
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    • 제7권4호
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    • pp.339-354
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    • 2007
  • Arched Corrugated Steel Roof (ACSR) is a kind of thin-walled steel shell, composing of arched panels with transverse small corrugations. Four full-scale W666 ACSR samples with 18m and 30m span were tested under full and half span static vertical uniform loads. Displacement, bearing capacities and failure modes of the four samples were measured. The web and bottom flange in ACSR with transverse small corrugations are simplified to anisotropic curved plates, and the equivalent tensile modulus, shear modulus and Poisson's ratio of 18m span ACSR were measured. Two 18 m-span W666 ACSR samples were analyzed with the Finite Element Analysis program ABAQUS. Base on the tests, the limit bearing capacity of ACSR is low, and for half span loading, it is 74-75% compared with the full span loading. When the testing load approached to the limit value, the bottom flange at the sample's bulge place locally buckled first, and then the whole arched roof collapsed suddenly. If the vertical loads apply along the full span, the deformation shape is symmetric, but the overall failure mode is asymmetric. For half span vertical loading, the deformation shape and the overall failure mode of the structure are asymmetric. The ACSR displacement under the vertical loads is large and the structural stiffness is low. There is a little difference between the FEM analysis results and testing data, showing the simplify method of small corrugations in ACSR and the building techniques of FEM models are rational and useful.