• 제목/요약/키워드: Orthotropic properties

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직교이방성 적층 복합재료 원추셸의 자유진동 (Free Vibration of Orthotropic Laminated Composite Conical Shells)

  • 이영신;강인식
    • 대한기계학회논문집
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    • 제13권4호
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    • pp.595-603
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    • 1989
  • 본 연구에서는 양단이 단순지지되어 있는 특수 직교이방성 적층 복합재료 원추셸의 자유진동에 관한 지배방정식을 Flugge 이론으로부터 유도하고 Galerkin 방법을 적용하여 해를 구하였으며, 원추셸의 기하학적 매개변수 및 직교이방성 매개 변수의 변화에 따르는 진동특성을 고찰하였다.

FINITE ELEMENT ANALYSIS OF A STEADY-STATE ROLLING TIRE TAKING THE EFFECT OF TREAD PATTERN INTO ACCOUNT

  • KIM K. W.
    • International Journal of Automotive Technology
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    • 제7권1호
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    • pp.101-107
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    • 2006
  • The force and moment simulation of a steady-state rolling tire taking the effect of tread pattern into account is described using a steady-state transport method with ABAQUS. Tread meshes can not fully consider a tread pattern because detailed tread meshes are not allowed in the steady-state transport method. Therefore, the tread elements are modeled to have orthotropic property instead of isotropic property. The force and moment simulation has been carried out for the cases of both isotropic and orthotropic properties of tread elements. Both cases of simulation results are then compared with the experimental results. It is verified that the orthotropic case is in a better agreement with the experimental result than the isotropic case. Angle effects of tread pattern have been studied by changing the orientation angle of orthotropic property of tread. It is shown that the groove angle in the tread shoulder region has a more effect on force and moment of a tire than that in the tread center region.

광탄성 직교이방성체의 물성치와 응력 프린지치 간이 측정법 (The simple measurement of physical properties and stress fringe value for photo-elastic orthotropic material)

  • 황재석;이광호
    • 대한기계학회논문집
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    • 제14권1호
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    • pp.23-36
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    • 1990
  • 본 연구에서는 Iosipescu의 전단 시험법을 사용하여 직접 측정한 응력 프린지 치(f$_{LT}$ )와 Sampson의 응력-광법칙에 의하여 구한 f$_{LT}$ 와 서로 비교하여 Sampson의 응력-광법칙이 f$_{LT}$ 를 간접적으로 측정하는데 사용할 수 있는가를 확 인한다. 그리고 직교 이방성 재료를 광탄성 실험에 의하여 해석하는 경우에 필요한 기본물성치와 응력 프린지치 관계를 구하여 이 관계가 상온과 고온에서도 성립하는가 를 확인하고 또 직접 물성치를 측정하는 대신에 각 물성치에 대응되는 응력 프린지치 에 의하여 물성치를 구하는 방법을 개발하는데 이 연구의 목적을 둔다.

Numerical analysis of center cracked orthotropic fgm plate: Crack and material axes differ by θ°

  • Kaman, Mete Onur;Cetisli, Fatih
    • Steel and Composite Structures
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    • 제13권2호
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    • pp.187-206
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    • 2012
  • In this study, fracture analysis of orthotropic FGM (Functionally Graded Material) plate having center crack is performed, numerically. Material axis arbitrarily oriented and there is an angle ${\theta}^{\circ}$ between material and crack axes. Stress intensity factors at the crack tips for Mode I are calculated using Displacement Correlation Method (DCM). In numerical analysis, effects of material properties and variation of angle ${\theta}^{\circ}$ between material and crack axes on the fracture behavior are investigated for four different boundary conditions. Consequently, it is found that the effect of ${\theta}^{\circ}$ on stress intensity factor depends on variation of material properties.

국부하중 을 받는 직교이방성 원통셀 의 해석 (Analysis of Orthotropic Cylindrical Shells Subjected to Localized Loads)

  • 이영신;박정화;옹장우
    • 대한기계학회논문집
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    • 제8권5호
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    • pp.408-415
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    • 1984
  • 본 연구에서는 기존연구에 비하여 해의 형태가 간단하고 비교적 오차가 적은 해를 구하기 위하여 MorleyKoiter의 등방성 원통셸의 변위 및 응력상태를 2중 Fourier 급수를 적용하여 해석하였으며 수치예를 통하여 이들 값의 직교이방특성 및 셸형상에 따른 영향을 고찰하였다.

선하중을 받는 직교이방성 원통셀의 Novozhilov셀 이론에 의한 응력해석 (Stress analysis for the orthotropic cylindrical shells subjected to line load based on Novozhilov's shell theory)

  • 이영신;최병두
    • 대한기계학회논문집
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    • 제11권5호
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    • pp.789-799
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    • 1987
  • 본 연구에서는 기존연구에 비하여 해의 형태가 간단한 폐형태로 주어지는 엄 밀한 해를 구하기 위해, 직교이방성원통셸의 지배방정식을 Novozhilov 형복소미분방정 식으로 유도하였다. 수치예로서 모선전체 및 부분적으로 작용하는 선하중하에 원통 셸의 변립 및 응력상태를 해석하여 기존의 연구와 비교하였으며, 직교이방특성과 셸기 하학적 매개변수에 따르는 영향을 고찰하였다.

Free vibration analysis of elliptic and circular plates having rectangular orthotropy

  • Chakraverty, S.;Petyt, M.
    • Structural Engineering and Mechanics
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    • 제7권1호
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    • pp.53-67
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    • 1999
  • The natural frequencies and modes of free vibration of specially orthotropic elliptic and circular plates are analysed using the Rayleigh-Ritz method. The assumed functions used are two-dimensional boundary characteristic orthogonal polynomials which are generated using the Gram-Schmidt orthogonalization procedure. The first five natural frequencies are reported here for various values of aspect ratio of the ellipse. Results are given for various boundary conditions at the edges i.e., the boundary may be any of clamped, simply-supported or fret. Numerical results are presented here for several orthotropic material properties. For rectilinear orthotropic circular plates, a few results are available in the existing literature, which are compared with the present results and are found to be in good agreement.

등방성체와 직교이방성체의 접합계면네 내재된 동적모드 III 균열의 등속전파 (Dynamic Mode III Crack Propagated with Constant Velocity at Interface Between Isotropic and Orthotropic Material)

  • 이광호;황재석;유재용
    • 대한기계학회논문집A
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    • 제20권12호
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    • pp.3828-3837
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    • 1996
  • The dynamic problems of interface crack propagated with constant velocity along the interface of bimateraial composed of isotropic and orthotropicmaterial under antiplane loading condition are studied in this paper. The general dynamic stress fields and displacement fields of mode III are derived when interface crack between isotropic and orthotropic material is propagating with constant velocity. The general dynamic stress fields and displacement fields in isotropic material. Finally, the characteristics of interface crack propagation are studied with various properties of isotropic and orthotropic material and crack propagarion velocities.

계면균열을 갖는 반무한체에 접합된 직교이방성 층의 좌굴 (Buckling of an Orthotropic Layer Bonded to a Half-Space with an Interface Crack)

  • 정경문;범현규
    • 한국정밀공학회지
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    • 제18권12호
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    • pp.95-103
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    • 2001
  • The buckling of an orthotropic layer bonded to an orthotropic half-space with an interface crack subjected to compressive load under plane strain is analyzed. General solution to the stability equations describing the buckling behavior of both the layer and the half-space is expressed in terms of displacement functions. The displacement functions are represented by the solution of Cauchy-type singular integral equations, which are numerically solved. Numerical results of the critical buckling loads are presented fur various geometric parameters and material properties of both the layer and half-space.

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Stability of the porous orthotropic laminated composite plates via the hyperbolic shear deformation theory

  • Ferruh Turan
    • Steel and Composite Structures
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    • 제48권2호
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    • pp.145-161
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    • 2023
  • This study investigates the influences of porosity on the stability of the orthotropic laminated plates under uniaxial and biaxial loadings based on the hyperbolic shear deformation theory. Three different porosity distribution are considered with three specific functions through the plate thickness. The stability equations of porous orthotropic laminated plates are derived by the virtual work principle. Applying the Galerkin method to partial differential equations, the critical buckling load relation of porous orthotropic laminated plates is obtained. After validating the accuracy of the proposed formulation in accordance with the available literature, a parametric analysis is performed to observe the sensitivity of the critical buckling load to shear deformation, porosity, orthotropy, loading factor, and different geometric properties.