• 제목/요약/키워드: simply supported

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Thermoelastic damping in generalized simply supported piezo-thermo-elastic nanobeam

  • Kaur, Iqbal;Lata, Parveen;Singh, Kulvinder
    • Structural Engineering and Mechanics
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    • 제81권1호
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    • pp.29-37
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    • 2022
  • The present paper deals with the application of one dimensional piezoelectric materials in particular piezo-thermoelastic nanobeam. The generalized piezo-thermo-elastic theory with two temperature and Euler Bernoulli theory with small scale effects using nonlocal Eringen's theory have been used to form the mathematical model. The ends of nanobeam are considered to be simply supported and at a constant temperature. The mathematical model so formed is solved to obtain the non-dimensional expressions for lateral deflection, electric potential, thermal moment, thermoelastic damping and frequency shift. Effect of frequency and nonlocal parameter on the lateral deflection, electric potential, thermal moment with generalized piezothermoelastic theory are represented graphically using the MATLAB software. Comparisons are made with the different theories of thermoelasticity.

FE modelling of low velocity impact on RC and prestressed RC slabs

  • Ganesan, Partheepan;Kumar, S. Venkata Sai
    • Structural Engineering and Mechanics
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    • 제71권5호
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    • pp.515-524
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    • 2019
  • The present study deals with the simulation of low velocity impact on prestressed and reinforced concrete (RC) slabs supported with different end conditions. The prestress is pre-applied on the RC slab in an analytical approach for the prestressed slab. RC slabs with dimensions $500{\times}600{\times}60mm$, $500{\times}600{\times}80mm$ and $500{\times}600{\times}120mm$ were used by changing support condition in two different ways; (i) Opposite sides simply supported, (ii) Adjacent sides simply supported with opposite corner propped. Deflection response of these specimens were found for the impact due to three different velocities. The effect of grade of concrete on deflection due to the impact of these slabs were also studied. Deflection result of $500{\times}500{\times}50mm$ slab was calculated numerically and compared the result with the available experimental result in literature. Finite element analyses were performed using commercially available ANSYS 16.2 software. The effectiveness of prestressing on impact resistant capacity of RC slabs are demonstrated by the way of comparing the deflection of RC slabs under similar impact loadings.

Dynamic Responses and Fuzzy Control of a Simply Supported Beam Subjected to a Moving Mass

  • Kong, Yong-Sik;Ryu, Bong-Jo;Shin, Kwang-Bok;Lee, Gyu-Seop;Lee, Hong-Gi
    • Journal of Mechanical Science and Technology
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    • 제20권9호
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    • pp.1371-1381
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    • 2006
  • This paper deals with the active vibration control of a simply-supported beam traversed by a moving mass using fuzzy control. Governing equations for dynamic responses of a beam under a moving mass are derived by Galerkin's mode summation method, and the effect of forces (gravity force, Coliolis force, inertia force caused by the slope of the beam, transverse inertia force of the beam) due to the moving mass on the dynamic response of a beam is discussed. For the active control of dynamic deflection and vibration of a beam under the moving mass, the controller based on fuzzy logic is used and the experiments are conducted by VCM (voice coil motor) actuator to suppress the vibration of a beam. Through the numerical and experimental studies, the following conclusions were obtained. With increasing mass ratio y at a fixed velocity of the moving mass under the critical velocity, the position of moving mass at the maximum dynamic deflection moves to the right end of the beam. With increasing velocity of the moving mass at a fixed mass ratio ${\gamma}$, the position of moving mass at the maximum dynamic deflection moves to the right end of the beam too. The numerical predictions of dynamic deflection of the beam have a good agreement with the experimental results. With the fuzzy control, more than 50% reductions of dynamic deflection and residual vibration of the tested beam under the moving mass are obtained.

불균일 단면을 갖는 단순지지 보의 모달해석 및 실험 (Modal Analysis and Experiment of a Simply-supported Beam with Non-uniform Cross Sections)

  • 김인우;유봉조;김영식
    • 한국산학기술학회논문지
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    • 제16권12호
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    • pp.8654-8664
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    • 2015
  • 기계, 건축, 토목공학 분야 등에는 불균일 단면을 갖는 보 형태의 구조물들이 널리 사용되고 있다. 본 논문은 양단이 단순 지지된 보 구조물들의 동특성과 진동에 대한 문제를 다루며, 국부좌표를 사용한 지배방정식이 유도된다. 갤러킨의 모드합 방법으로 해가 가정되고, 고유진동수를 구하는 행렬식을 푸는 데는 이분법을 적용하였다. 유한요소법이 단지 기하학적 경계조건만을 만족시키는 허용함수를 사용하는 반면, 본 논문에서는 갤러킨의 모드합 방법을 적용하여, 지배방정식과 경계조건을 모두 만족하는 고유함수를 사용하였다. 계의 동특성을 알기위해, 네 종류의 불균일 단면을 갖는 단순 지지 보에 대해 모달 해석과 시험이 수행되었으며, 해석 결과는 실험 결과와 근사한 일치를 나타내었다.

프리스트레스트 콘크리트 보의 부정정 스트럿-타이 모델 (An Indeterminate Strut-Tie Model for Prestressed Concrete Beams)

  • 채현수;윤영묵
    • 대한토목학회논문집
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    • 제35권4호
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    • pp.801-814
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    • 2015
  • 이 논문에서는 스트럿-타이 모델을 이용한 프리스트레스트 콘크리트 보의 해석 및 설계 시 프리스트레스트 콘크리트 보의 비선형 파괴거동 특성 및 복잡한 하중전달 메커니즘을 합리적인 방법으로 반영할 수 있는 단순한 형태의 부정정 스트럿-타이 모델을 제안하였다. 또한 현행 설계기준서의 스트럿-타이 모델 규정을 이 연구에서 제안한 부정정 스트럿-타이 모델에 접목시켜 프리스트레스트 콘크리트 보의 해석 및 설계를 수행할 수 있는 부정정 스트럿-타이 모델의 하중분배율을 제안하였다. 이 연구에서 제안한 부정정 스트럿-타이 모델 및 하중분배율의 적합성을 검증하기 위해 파괴실험이 수행된 47개의 프리스트레스트 콘크리트 보의 극한강도를 평가하였으며, 그 결과를 현행 설계기준서의 스트럿-타이 모델 방법에 의한 평가결과와 비교분석 하였다.

Stress concentration and deflection of simply supported box girder including shear lag effect

  • Yamaguchi, Eiki;Chaisomphob, Taweep;Sa-nguanmanasak, Jaturong;Lertsima, Chartree
    • Structural Engineering and Mechanics
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    • 제28권2호
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    • pp.207-220
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    • 2008
  • The shear lag has been studied for many years. Nevertheless, existing research gives a variety of stress concentration factors. Unlike the elementary beam theory, the application of load is not unique in reality. For example, concentrated load can be applied as point load or distributed load along the height of the web. This non-uniqueness may be a reason for the discrepancy of the stress concentration factors in the existing studies. The finite element method has been often employed for studying the effect of the shear lag. However, not many researches have taken into account the influence of the finite element mesh on the shear lag phenomenon, although stress concentration can be quite sensitive to the mesh employed in the finite element analysis. This may be another source for the discrepancy of the stress concentration factors. It also needs to be noted that much less studies seem to have been conducted for the shear lag effect on deflection while some design codes have formulas. The present study investigates the shear lag effect in a simply supported box girder by the three-dimensional finite element method using shell elements. The whole girder is modeled by shell elements, and extensive parametric study with respect to the geometry of a box girder is carried out. Not only stress concentration but also deflection is computed. The effect of the way load is applied and the dependency of finite element mesh on the shear lag are carefully treated. Based on the numerical results thus obtained, empirical formulas are proposed to compute stress concentration and deflection that includes the shear lag effect.

분포하중(分布荷重)을 받는 구형판(矩形板)의 탄성해석(彈性解析) (Analysis of Rectangular Plates under Distributed Loads of Various Intensity with Interior Supports at Arbitrary Positions)

  • 장석윤
    • 대한조선학회지
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    • 제13권1호
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    • pp.17-23
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    • 1976
  • Some methods of analysis of rectangular plates under distributed load of various intensity with interior supports are presented herein. Analysis of many structures such as bottom, side shell, and deck plate of ship hull and flat slab, with or without internal supports, Floor systems of bridges, included crthotropic bridges is a problem of plate with elastic supports or continuous edges. When the four edges of rectangular plate is simply supported, the double Fourier series solution developed by Navier can represent an exact result of this problem. If two opposite edges are simply supported, Levy's method is available to give an "exact" solution. When the loading condition and supporting condition of a plate does not fall into these cases, no simple analytic method seems to be feasible. Analysis of a simply supported rectangular plate under irregularly distributed loads of various intensity with internal supports is carried out by applying Navier solution well as the "Principle of Superposition." Finite difference technique is used to solve plates under irregularly distributed loads of various intensity with internal supports and with various boundary conditions. When finite difference technique is applied to the Lagrange's plate bending equation, any of fourth order derivative term in this equation produces at least five pivotal points leading to some troubles when the resulting linear algebraic equations are to be solved. This problem was solved by reducing the order of the derivatives to two: the fourth order partial differential equation with one dependent variable, namely deflection, is changed to an equivalent pair of second order partial differential equations with two dependent variables. Finite difference technique is then applied to transform these equations to a set of simultaneous linear algebraic equations. Principle of Superposition is then applied to handle the problems caused by concentrated loads and interior supports. This method can be used for the cases of plates under irregularly distributed loads of various intensity with arbitrary conditions such as elastic supports, or continuous edges with or without interior supports, and this method can also be solve the influence values of deflection, moment and etc. at arbitrary position of plates under the live load.

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Using an equivalent continuum model for 3D dynamic analysis of nanocomposite plates

  • Tahouneh, Vahid
    • Steel and Composite Structures
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    • 제20권3호
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    • pp.623-649
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    • 2016
  • Most of the early studies on plates vibration are focused on two-dimensional theories, these theories reduce the dimensions of problems from three to two by introducing some assumptions in mathematical modeling leading to simpler expressions and derivation of solutions. However, these simplifications inherently bring errors and therefore may lead to unreliable results for relatively thick plates. The main objective of this research paper is to present 3-D elasticity solution for free vibration analysis of continuously graded carbon nanotube-reinforced (CGCNTR) rectangular plates resting on two-parameter elastic foundations. The volume fractions of oriented, straight single-walled carbon nanotubes (SWCNTs) are assumed to be graded in the thickness direction. In this study, an equivalent continuum model based on the Eshelby-Mori-Tanaka approach is employed to estimate the effective constitutive law of the elastic isotropic medium (matrix) with oriented, straight carbon nanotubes (CNTs). The proposed rectangular plates have two opposite edges simply supported, while all possible combinations of free, simply supported and clamped boundary conditions are applied to the other two edges. The formulations are based on the three-dimensional elasticity theory. A semi-analytical approach composed of differential quadrature method (DQM) and series solution is adopted to solve the equations of motion. The fast rate of convergence of the method is demonstrated and comparison studies are carried out to establish its very high accuracy and versatility. The 2-D differential quadrature method as an efficient and accurate numerical tool is used to discretize the governing equations and to implement the boundary conditions. The convergence of the method is demonstrated and to validate the results, comparisons are made between the present results and results reported by well-known references for special cases treated before, have confirmed accuracy and efficiency of the present approach. The novelty of the present work is to exploit Eshelby-Mori-Tanaka approach in order to reveal the impacts of the volume fractions of oriented CNTs, different CNTs distributions, various coefficients of foundation and different combinations of free, simply supported and clamped boundary conditions on the vibrational characteristics of CGCNTR rectangular plates. The new results can be used as benchmark solutions for future researches.

단순지지 RC 깊은 보 부정정 스트럿-타이 모델의 하중분배율- (I) 하중분배율의 제안 (Load Distribution Ratios of Indeterminate Strut-Tie Models for Simply Supported RC Deep Beams - (I) Proposal of Load Distribution Ratios)

  • 김병헌;윤영묵
    • 대한토목학회논문집
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    • 제28권2A호
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    • pp.259-267
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    • 2008
  • 철근콘크리트 깊은 보는 콘크리트와 전단철근에 의한 전단저항 메커니즘의 성능에 의해 극한강도가 지배된다. 깊은 보의 거동은 전단지간대 유효깊이의 비, 휨철근비, 하중점과 지지점의 조건, 그리고 사용재료의 성질 등의 여러 변수간의 복합적인 역학관계로 인해 매우 복잡하다. 본 논문에서는 이러한 깊은 보의 강도 및 거동 특성을 모두 반영하여 단순지지 철근콘크리트 깊은 보의 설계를 수행할 수 있는 부정정 스트럿-타이 모델을 제안하였다. 또한 현 스트럿-타이 모델 설계기준을 부정정 스트럿-타이 모델을 이용한 단순지지 철근콘크리트 깊은 보의 설계에 합리적으로 적용하기 위해 수직 트러스 메커니즘에 의해 전달되는 하중의 크기 즉 부정정 스트럿-타이 모델의 하중분배율을 제안하였다. 하중분배율의 결정 시 단순지지 철근콘크리트 깊은 보의 전단에 대한 연성파괴거동을 확보하기 위하여 깊은 보의 전단저항 메커니즘을 구성하는 콘크리트 스트럿과 수직철근 타이가 동시에 파괴된다는 전단평형철근비 개념을 도입하였으며, 다양한 수치해석결과를 바탕으로 단순지지 깊은 보의 강도 및 거동에 영향을 미치는 전단지간대 유효깊이의 비, 휨철근비, 그리고 콘크리트의 압축강도 등의 설계변수를 고려하였다. 본 논문의 후속편에서는 기존의 여러 설계방법들과 본 연구에서 제안한 방법을 이용하여 파괴실험이 수행된 다양한 종류의 단순지지 깊은 보의 강도를 평가하고, 본 연구에서 제안한 방법의 적합성을 검증하였다.

대변형을 가지는 사각형 박형유리판의 비선형 차분해석 (A Finite Difference Large Displacement Analysis of Rectangular Thin Glass Plate)

  • Kim, Chi-Kyung
    • 한국안전학회지
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    • 제10권2호
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    • pp.129-133
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    • 1995
  • 균등한 종방향 압력을 받고있는 유연성 물질인 게스킷 상의 얇은 사각형유리판을 새로운 접근방법으로 해석하였다. 본-카만의 판의 이론에 의거 단순지지의 얇은 유리판의 응력과 처짐을 차분법으로 해석하였으며 비선형적으로 계산되는 컴퓨터 프로그램을 발전시켰다. 해의 보다 빠른 수렴을 위한 새로운 반복법을 전개시켰다.

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