• 제목/요약/키워드: higher-order formulation

검색결과 240건 처리시간 0.021초

최소 제곱 무요소법을 이용한 선형 탄성 변형 해석 (The Least-Squares Meshfree Method for Linear Elasticity)

  • 권기찬;박상훈;윤성기
    • 대한기계학회논문집A
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    • 제26권11호
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    • pp.2312-2321
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    • 2002
  • The first-order least-squares meshfree method for linear elasticity is presented. The conventional and the compatibility-imposed least-squares formulations are studied on the convergence behavior of the solution and the robustness to integration error. Since the least-squares formulation is a type of mixed formulation and induces positive-definite system matrix, by using shape functions of same order for both primal and dual variables, higher rate of convergence is obtained for dual variables than Galerkin formulation. Numerical examples also show that the presented formulations do not exhibit any volumetric locking for the incompressible materials.

Formulation Method for Solid-to-Beam Transition Finite Elements

  • 임장권;송대한;송병호
    • Journal of Mechanical Science and Technology
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    • 제15권11호
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    • pp.1499-1506
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    • 2001
  • Various transition elements are used in general for the effective finite element analysis of complicated mechanical structures. In this paper, a solid-to-beam transition finite element, which can b e used for connecting a C1-continuity beam element to a continuum solid element, is proposed. The shape functions of the transition finite element are derived to meet the compatibility condition, and a transition element equation is formulated by the conventional finite element procedure. In order to show the effectiveness and convergence characteristics of the proposed transition element, numerical tests are performed for various examples. As a result of this study, following conclusions are obtained. (1) The proposed transition element, which meets the compatibility of the primary variables, exhibits excellent accuracy. (2) In case of using the proposed transition element, the number of nodes in the finite element model may be considerably reduced and the model construction becomes more convenient. (3) This formulation method can be applied to the usage of higher order elements.

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Dynamic Analysis of Laminated Composite and Sandwich Plates Using Trigonometric Layer-wise Higher Order Shear Deformation Theory

  • Suganyadevi, S;Singh, B.N.
    • International Journal of Aerospace System Engineering
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    • 제3권1호
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    • pp.10-16
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    • 2016
  • A trigonometric Layerwise higher order shear deformation theory (TLHSDT) is developed and implemented for free vibration and buckling analysis of laminated composite and sandwich plates by analytical and finite element formulation. The present model assumes parabolic variation of out-plane stresses through the depth of the plate and also accomplish the zero transverse shear stresses over the surface of the plate. Thus a need of shear correction factor is obviated. The present zigzag model able to meet the transverse shear stress continuity and zigzag form of in-plane displacement continuity at the plate interfaces. Hence, botheration of shear correction coefficient is neglected. In the case of analytical method, the governing differential equation and boundary conditions are obtained from the principle of virtual work. For the finite element formulation, an efficient eight noded $C^0$ continuous isoparametric serendipity element is established and employed to examine the dynamic analysis. Like FSDT, the considered mathematical model possesses similar number of variables and which decides the present models computationally more effective. Several numerical predictions are carried out and results are compared with those of other existing numerical approaches.

A new refined nonlocal beam theory accounting for effect of thickness stretching in nanoscale beams

  • Kheroubi, Boumediene;Benzair, Abdelnour;Tounsi, Abdelouahed;Semmah, Abdelwahed
    • Advances in nano research
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    • 제4권4호
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    • pp.251-264
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    • 2016
  • In this paper, a simple and refined nonlocal hyperbolic higher-order beam theory is proposed for bending and vibration response of nanoscale beams. The present formulation incorporates the nonlocal scale parameter which can capture the small scale effect, and it considers both shear deformation and thickness stretching effects by a hyperbolic variation of all displacements across the thickness without employing shear correction factor. The highlight of this formulation is that, in addition to modeling the displacement field with only two unknowns, the thickness stretching effect (${\varepsilon}_z{\neq}0$) is also included in the present model. By utilizing the Hamilton's principle and the nonlocal differential constitutive relations of Eringen, the equations of motion of the nanoscale beam are reformulated. Verification studies demonstrate that the developed theory is not only more accurate than the refined nonlocal beam theory, but also comparable with the higher-order shear deformation theories which contain more number of unknowns. The theoretical formulation proposed herein may serve as a reference for nonlocal theories as applied to the static and dynamic responses of complex-nanobeam-system such as complex carbon nanotube system.

복합적층구조해석을 위한 1차전단변형이론의 간단한 수정방안 (A Simple Modification of the First-order Shear Deformation Theory for the Analysis of Composite Laminated Structures)

  • 천경식;지효선
    • 한국강구조학회 논문집
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    • 제23권4호
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    • pp.475-481
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    • 2011
  • 본 논문에서는 1차전단변형이론의 횡방향 전단응력과 전단변형률을 개선한 간단한 수정방법을 제시하였다. 고차전단변형이론, 층별이론과 같은 기존의 많은 제정된 방법들과 비교해서 본 방법은 매우 간단하게 $C^0$ 연속성만이 요구되는 유한요소에 적용할 수 있으며, 그 방정식 구성도 매우 간단하다. 본 방법의 기본 개념은 고차전단변형이론에 의한 수식으로 부터 두께방향에 따른 횡방향 전단응력과 전단변형률의 분포를 수정하는 것이다. 그러므로 1차전단변형이론처럼 전단보정계수는 더 이상 요구되지 않는다. 제안한 수식의 타당성을 검증하기 위하여 수치해석을 수행하였으며, 본 수정방법에 의한 해는 고차전단변형이론을 고려한 결과와 잘 일치하였다.

Higher Order Eigenfields in Mode II Cracks Under Elastic-Plastic Deformation

  • Insu Jeon;Lee, Yongwoo;Seyoung Im
    • Journal of Mechanical Science and Technology
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    • 제17권2호
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    • pp.254-268
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    • 2003
  • The explicit formulation of the J-integral and the M-integral is constructed in terms of the stress intensity factor and the higher order stress coefficients for Mode II cracks under small or large scale yielding. Furthermore, the stress intensity factor and the higher order stress coefficients as well are computed with the aid of the two-state J- and the M-integral, which is found to be accurate and efficient. It is found that the contribution from the higher order singularities to the J-integral is closely related to the configuration of the plastic zone.

Flutter analysis by refined 1D dynamic stiffness elements and doublet lattice method

  • Pagani, Alfonso;Petrolo, Marco;Carrera, Erasmo
    • Advances in aircraft and spacecraft science
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    • 제1권3호
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    • pp.291-310
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    • 2014
  • An advanced model for the linear flutter analysis is introduced in this paper. Higher-order beam structural models are developed by using the Carrera Unified Formulation, which allows for the straightforward implementation of arbitrarily rich displacement fields without the need of a-priori kinematic assumptions. The strong form of the principle of virtual displacements is used to obtain the equations of motion and the natural boundary conditions for beams in free vibration. An exact dynamic stiffness matrix is then developed by relating the amplitudes of harmonically varying loads to those of the responses. The resulting dynamic stiffness matrix is used with particular reference to the Wittrick-Williams algorithm to carry out free vibration analyses. According to the doublet lattice method, the natural mode shapes are subsequently used as generalized motions for the generation of the unsteady aerodynamic generalized forces. Finally, the g-method is used to conduct flutter analyses of both isotropic and laminated composite lifting surfaces. The obtained results perfectly match those from 1D and 2D finite elements and those from experimental analyses. It can be stated that refined beam models are compulsory to deal with the flutter analysis of wing models whereas classical and lower-order models (up to the second-order) are not able to detect those flutter conditions that are characterized by bending-torsion couplings.

Comparative dynamic studies of thick laminated composite shells based on higher-order theories

  • Ganapathi, M.;Patel, B.P.;Pawargi, D.S.;Patel, H.G.
    • Structural Engineering and Mechanics
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    • 제13권6호
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    • pp.695-711
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    • 2002
  • Here, the dynamic response characteristics of thick cross-ply laminated composite cylindrical shells are studied using a higher-order displacement model. The formulation accounts for the nonlinear variation of the in-plane and transverse displacements through the thickness, and abrupt discontinuity in slope of the in-plane displacements at any interface. The effect of inplane and rotary inertia terms is included. The analysis is carried out using finite element approach. The influences of various terms in the higher-order displacement field on the free vibrations, and transient dynamic response characteristics of cylindrical composite shells subjected to thermal and mechanical loads are analyzed.

고차(高次) 판(板) 사각형(四角形) 유한요소(有限要素) (Higher Order Quadrilateral Plate Bending Finite Element)

  • 신영식;신현묵;김명철
    • 대한토목학회논문집
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    • 제8권2호
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    • pp.25-32
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    • 1988
  • 본 연구에서는 8절점 28자유도를 갖는 사각형 고차 판 유한 요소를 면내고차 변위를 고려하여 3차원 연속체로부터 유도하였다. 요소매트릭스들은 판의 운동방정식으로부터 Galerkin 가중잔차법으로 유도하고 감차적분을 수행하여 구하였다. 고차 판 유한요소를 이용하여 판의 처짐해석과 자유진동해석을 수행한 결과 판의 두께와 경게조건에 관계없이 매우 정확한 결과를 나타내었다.

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제형의 차이가 제초제 Cyhalofop-butyl의 생물활성에 미치는 영향 (Effect of Different Formulations on the Biological Activity of Herbicide Cyhalofop-Butyl)

  • 한강완;조재영;노안성
    • Applied Biological Chemistry
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    • 제38권5호
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    • pp.440-446
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    • 1995
  • 제초제 Cyhalofop-butyl을 유효성분으로한 유제, microemulsion, 수화제 및 입제를 제조하여 수도에 대한 약해, 피에 대한 제초효과, 피의 경엽에 대한 부착량 및 흡수량을 측정한 결과는 다음과 같았다. 수화제에서는 원제를 액상화할 수 있는 보조제가 첨가되었을때 피에 대한 살초효과가 증가하였으며, 이는 경엽에의 흡수량 증가와 일치하였다. 그러나 수화제 살포 수용액의 피에 대한 부착력과 흡수량은 정확히 일치하지는 않았다. 유제는 수화제 보다 높은 살초 효과와 엽면 흡수량을 보였다. Microemulsion에서는 높은 부착력과 함께 엽면에 대한 흡수량도 가장 높게 나타났다. 또한 본 원제에 대해서 입제의 적용성을 검정한 결과 유효성분 부상성 입제의 가능성도 확인할 수 있었으며, 피에 대한 살초 효과도 높게 나타났다.

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