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    Developing a Compact Finite Difference Method for Solving Fluid - Solid Interaction in Incompressible Flow

    , M.Sc. Thesis Sharif University of Technology Parseh, Kaveh (Author) ; Hejranfar, Kazem (Supervisor)
    Abstract
    In this study, fluid-solid interaction (FSI) is simulated computationally by using a high-order accurate numerical method. The two-dimensional incompressible viscous flows are considered in the fluid domain. The primary problem with solutions of the incompressible Navier–Stokes equations is the difficulty of coupling changes in the velocity field with changes in the pressure field while satisfying the continuity equation. Herein, the artificial compressibility method is used to overcome this difficulty. Preconditioning is implemented to reduce the stiffness of the system of equations to increase the convergence rate of the solution. Using preconditioning, physical solutions even at low... 

    On the Stability of Rotating Cylinder Conveying Flow in an External Fluid Medium

    , M.Sc. Thesis Sharif University of Technology Hojjati, Mohammad (Author) ; Dehghani Firoozabadi, Rouhollah (Supervisor)
    Abstract
    The present study aims at investigating the stability of flexible spinning cylinders conveying flow in an external fluid Medium. Using the linearized Navier-Stokes equations for the flow, a two-dimensional model is developed governing the fluid motion. The resultant force exerted on the flexible cylinder wall due to the fluid interactions is calculated as a function of the lateral acceleration. Applying the Hamilton principle, the governing equations of flexural vibration of the rotary flexible cylinder mounted on simply supported axles are derived. Having the forces due to the conveying fluid calculated and substituting into the governing equations, a coupled field governing equations of... 

    Aeroelastic Analysis of a Complete Aircraft Via State Space Modeling

    , M.Sc. Thesis Sharif University of Technology Ghobadi, Amir Hossein (Author) ; Keshavarz Haddad, Gholamreza (Supervisor)
    Abstract
    This dissertation presents aeroelastic stability analysis (flutter) pertinent to the complete flexible aircraft based on analytical dynamics, structural dynamics and aerodynamics. The unified formulation is based on fundamental principles and incorporates in a natural manner both rigid body motions of the aircraft as a whole and elastic deformations of the flexible components (fuselage, wing and empennage), as well as the aerodynamic, propulsion and gravity forces. The aircraft motion is described in terms of three translations and three rotations of a reference frame attached to the undeformed fuselage, and acting as aircraft body axes, and elastic displacements of each of the flexible... 

    Heterogeneities in polymer structural and dynamic properties in graphene and graphene oxide nanocomposites: molecular dynamics simulations

    , Article Macromolecular Theory and Simulations ; Volume 26, Issue 2 , 2017 ; 10221344 (ISSN) Azimi, M ; Mirjavadi, S. S ; Salem Hamouda, A. M ; Makki, H ; Sharif University of Technology
    Wiley-VCH Verlag  2017
    Abstract
    The effect of graphene (G) and graphene oxide (GO), used as the nanofiller in polymer nanocomposites (NC), on the structural and dynamic properties of polymer chains, has been studied by means of molecular dynamics (MD) simulations. Two polymers, i.e., poly(propylene) and poly(vinyl alcohol), are employed as matrices to cover a wider range of polymer–filler interactions. The local structural properties, e.g., density profile, average Rg, and end-to-end distance as well as dynamic properties, e.g., estimated translational and orientational relaxation times, of polymer chains are studied. In addition, the interaction energies are estimated between polymers and nanofillers for different hybrid... 

    Probability density evolution for time-varying reliability assessment of wing structures

    , Article Aviation ; Volume 22, Issue 2 , 2018 , Pages 45-54 ; 16487788 (ISSN) Saraygord Afshari, S ; Pourtakdoust, S. H ; Sharif University of Technology
    Vilnius Gediminas Technical University  2018
    Abstract
    Reliability evaluation is a key factor in serviceability and safety analysis of air vehicles. Structural health monitoring methods have grown to a degree of maturity in many industries. However, there is a challenging interest to tie in SHM with reliability assessment. In this respect, consideration of stochastic structural dynamics with SHM data and random loadings opens a new chapter in failure prevention. The current study focuses on the stochastic behavior of structures as a way to relate SHM data with reliability. In this respect, uncertain factors such as atmospheric turbulence, structural parameters, and sensor outputs are considered in the process of reliability assessment. Firstly,... 

    Dynamic response of euler-Bernoulli, Timoshenko and higher-Order beams under a moving mass via RKPM

    , Article 7th European Conference on Structural Dynamics, EURODYN 2008, 7 July 2008 through 9 July 2008 ; 2008 ; 9780854328826 (ISBN) Nikkhoo, A ; Kiani, K ; Mehri, B ; Sharif University of Technology
    University of Southampton, Institute of Sound Vibration and Research  2008
    Abstract
    Discrete motion equations of an Euler-Bernoulli, Timoshenko and higher-order beams under a moving mass are derived for different boundary conditions. To this end, the reproducing kernel particle method (RKPM) has been utilized for spatial discretization, beside the extension of Newmark-β method for time discretization of the beams motion equations. The effects of significant parameters such as the beam's slenderness and velocity of the moving mass on the maximum deflection and bending moment of different beams are studied in some details. The results indicate the existence of a critical beam's slenderness mostly as a function of beam's boundary conditions, in which for slenderness lower than... 

    Dynamic analysis of a multi-Span bridge subjected to a moving vehicle using moving node technique

    , Article 7th European Conference on Structural Dynamics, EURODYN 2008, 7 July 2008 through 9 July 2008 ; 2008 ; 9780854328826 (ISBN) Ghafoori, E ; Souri, J ; Sharif University of Technology
    University of Southampton, Institute of Sound Vibration and Research  2008
    Abstract
    In this paper dynamic analysis of multi-span bridges subjected to a moving vehicle is investigated. Finite element method is used to model the problem, and the Newmark technique is used for direct integration of the governing equations. In this regard, the moving node technique is applied to represent the dynamic responses of the multi-span bridge, and the vehicle is idealized as a sprung-mass system. Results indicate that the maximum vertical deflection of the multi-span bridge occurs at the span under the vehicle. It was found that the mid-span vertical deflection of spans for dynamic and static loading are not the same, and the position of the vehicle for maximum deflection for dynamic... 

    Error estimate in calculating natural frequencies of a vibrating shaft by changing number of segments using lumped parameter model and transfer matrix method

    , Article 7th European Conference on Structural Dynamics, EURODYN 2008, 7 July 2008 through 9 July 2008 ; 2008 ; 9780854328826 (ISBN) Kargarnovin, M. H ; Sharif University of Technology
    University of Southampton, Institute of Sound Vibration and Research  2008
    Abstract
    In this paper using classical beam theory, the dynamical governing differential equations of a vibrating shaft are derived then by using lumped parameter technique and method of transfer matrix (TM) the induced eigen value problem is solved. In calculating natural frequencies of a vibrating shaft under different boundary conditions, primarily the shaft was divided into number of segments. In each segment different number of lumped properties like mass, damping and flexibility on overall massless elastic or rigid shaft were applied. One of the aims of this study was to find out the optimum value for number of segments under different aforementioned conditions. In order to estimate the natural... 

    Vibration analysis of spinning cylindrical shell made of functionally graded material using higher order shear deformation theory

    , Article 7th European Conference on Structural Dynamics, EURODYN 2008, 7 July 2008 through 9 July 2008 ; 2008 ; 9780854328826 (ISBN) Kargarnovin, M. H ; Mehrparvar, M ; Najafizadeh, A ; Sharif University of Technology
    University of Southampton, Institute of Sound Vibration and Research  2008
    Abstract
    In this paper the vibration of a spinning cylindrical shell made of functional graded material (FGM) made is investigated. After a brief introduction of FG materials, by employing higher order theory for shell deformation, constitutive relationships are derived. In the next step by utilizing energy method and Hamilton's principle governing deferential equation of spinning cylindrical shell is obtained. By making use of the principle of minimum potential energy, the characteristic equation of natural frequencies is derived. After verification of the results, the effect of changing different parameters such as material grade, L/R, h/R, and spinning velocity on the natural frequency are... 

    Free vibrations of a cord composite laminate thin cylindrical shell on a pasternak foundation

    , Article 7th European Conference on Structural Dynamics, EURODYN 2008, 7 July 2008 through 9 July 2008 ; 2008 ; 9780854328826 (ISBN) Kargarnovin, M. H ; Mamandi, A ; Younesian, D ; Sharif University of Technology
    University of Southampton, Institute of Sound Vibration and Research  2008
    Abstract
    The underground and buried oil and gas pipelines are continuously in contact with earthen soils on the outer surface and compressible fluids on the inner surface. Most these earthen soils can be appropriately represented by a model named Pasternak. Similarly, undersea oil and gas pipelines and tubes of heat exchangers remain in contact with fluids on both sides and also rockets and missiles filled with solid and liquid fuels and shallow shells supported on soft and light filaments in space vehicles, boilers and storage tanks on floor grid work in ships can also be considered as thin circular cylindrical shells on a Pasternak foundation. The basic aim of the presented study is investigation... 

    Dynamic analysis of gantry cranes subjected to a moving trolley hoisting a swinging object

    , Article 7th European Conference on Structural Dynamics, EURODYN 2008, 7 July 2008 through 9 July 2008 ; 2008 ; 9780854328826 (ISBN) Ghafoori, E ; Younesian, D ; Sharif University of Technology
    University of Southampton, Institute of Sound Vibration and Research  2008
    Abstract
    Vibration analysis of a gantry crane subjected to a moving trolley hoisting a swinging object is studied in this paper. The finite element method is used to model the dynamical system. Newmark's and Runge-Kutta techniques are used for direct integration of the equation of motion of the structure and the moving object respectively. The moving suspended load is modeled with a non-linear equation of motion including two degrees of freedom i.e. hoisting in conjunction with swinging. A series of numerical simulations are carried out to provide a comprehensive parametric study. The study is directed to identify dynamic characteristics of the coupled non-linear system as well as to provide... 

    Effect of boundary conditions on dynamic behaviour of bridges

    , Article Proceedings of the Institution of Civil Engineers: Structures and Buildings ; Volume 169, Issue 2 , 2016 , Pages 121-140 ; 09650911 (ISSN) Samanipour, K ; Vafai, H ; Sharif University of Technology
    Thomas Telford Services Ltd 
    Abstract
    A moving vehicle, owing to its vibration and mass inertia, has significant effects on the dynamic response of structures. Most bridge codes define a factor called the dynamic load allowance, which is applied to the maximum static moment under static loading due to traffic load. This paper presents how to model an actual truck on bridges and how the maximum dynamic stresses of bridges change during the passage of moving vehicles. Furthermore, an algorithm to solve the governing equation of the bridge simultaneous with the equations of motion of an actual European truck is presented. Subsequently, 32 dynamic analyses of different bridges with different spans, road profiles and boundary... 

    Assessment of cell-centered and cell-vertex finite volume approaches for computation of 2d structural dynamics on arbitrary quadrilateral grids

    , Article CMES - Computer Modeling in Engineering and Sciences ; Volume 106, Issue 6 , 2015 , Pages 395-439 ; 15261492 (ISSN) Hejranfar, K ; Azampour, M. H ; Sharif University of Technology
    Tech Science Press  2015
    Abstract
    In this study, cell-centered (CC) and cell-vertex (CV) finite volume (FV) approaches are applied and assessed for the simulation of two-dimensional structural dynamics on arbitrary quadrilateral grids. For the calculation of boundary nodes displacement in the CC FV approach, three methods are employed. The first method is a simple linear regression of displacement of boundary nodes from the displacement of interior cell centers. In the second method, an extrapolation technique is applied for this purpose and, in the third method; the line boundary cell technique is incorporated into the solution algorithm in an explicit manner. To study the effects of grid irregularity on the results of CC... 

    Novel aspects of elastic flapping wing: analytical solution for inertial forcing

    , Article Advances in Aircraft and Spacecraft Science ; Volume 5, Issue 3 , May , 2018 , Pages 335-348 ; 2287528X (ISSN) Zare, H ; Pourtakdoust, S. H ; Bighashdel, A ; Sharif University of Technology
    Techno Press  2018
    Abstract
    The structural dynamics (SD) behavior of Elastic Flapping Wings (EFWs) is investigated analytically as a novel approach in EFWs analysis. In this regard an analytical SD solution of EFW undergoing a prescribed rigid body motion is initially derived, where the governing equations are expressed in modal space. The inertial forces are also analytically computed utilizing the actuator induced acceleration effects on the wing structure, while due to importance of analytical solution the linearity assumption is also considered. The formulated initial-value problem is solved analytically to study the EFW structural responses, where the effect of structure-actuator frequency ratio,... 

    Evaluation of vierendeel peripheral frame as supporting structural element for prevention of progressive collapse

    , Article Steel and Composite Structures ; Volume 26, Issue 5 , March , 2018 , Pages 549-556 ; 12299367 (ISSN) Khaloo, A ; Omidi, H ; Sharif University of Technology
    Techno Press  2018
    Abstract
    Progressive building collapse occurs when failure of a structural component leads to the failure and collapse of surrounding members, possibly promoting additional failure. Global system collapse will occur if the damaged system is unable to reach a new static equilibrium configuration. The most common type of primary failure which led to the progressive collapse phenomenon, is the sudden removal of a column by various factors. In this study, a method is proposed to prevent progressive collapse phenomena in structures subjected to removal of a single column. A vierendeel peripheral frame at roof level is used to redistribute the removed column’s load on other columns of the structure. For... 

    Design of passive viscous fluid control systems for nonlinear structures based on active control

    , Article Journal of Earthquake Engineering ; Volume 23, Issue 6 , 2019 , Pages 1033-1054 ; 13632469 (ISSN) Zare, A. R ; Ahmadizadeh, M ; Sharif University of Technology
    Taylor and Francis Ltd  2019
    Abstract
    ABSTARCT: A practical procedure is developed for the design of passive control systems using viscous fluid dampers for nonlinear structures. The design methodology takes advantage of the modification of the damping, strength, and stiffness properties of the structure to achieve the desired relative displacement and absolute acceleration response. For this purpose, a study of poles in the complex plane is used to determine the required changes in the dynamic properties of nonlinear structures. Furthermore, a relatively simple relation between the ductility demands of highly damped single- and multiple-degree-of-freedom (SDF and MDF respectively) systems is established to reduce the... 

    A novel shape memory alloy-based element for structural stability control in offshore structures under cyclic loading

    , Article Ships and Offshore Structures ; Volume 15, Issue 8 , 2020 , Pages 844-851 Zareie, S ; Alam, M. S ; Seethaler, R. J ; Zabihollah, A ; Sharif University of Technology
    Taylor and Francis Ltd  2020
    Abstract
    Wind and ocean waves highly influence the performance and functionality of structures, requiring an efficient control element. The structural behavior of one of the most recent structural control elements, namely shape memory alloys (SMA)-based control element, under cyclic loadings of oceans waves, has been investigated. Shape memory alloys are one of the attractive smart materials with the ability to return to the initial shape after experiencing large deformation. Experimental tests have been conducted to study the effects of cyclic loads on several specimens of the SMA wires. The SMA wires are being used in the SMA-based structural control system to dissipate the energy of external... 

    A study of pre-straining shape memory alloy (SMA)-based control elements subject to large-amplitude cyclic loads

    , Article Ships and Offshore Structures ; 2020 Zareie, S ; Zabihollah, A ; Sharif University of Technology
    Taylor and Francis Ltd  2020
    Abstract
    Dynamic environmental loads, such as winds and waves, make the stability of offshore structures at high risk, requiring reliable yet efficient control elements to ensure the stability of such structures under lateral loads. Among the variety of control elements that have been developed to enhance the stability of a structure, shape memory alloy (SMA)-based control elements are promising as they are low-cost, easy to embed into the main control element, and do not need an external power supply. However, cyclic loads may highly influence the performance and functionality of SMA-based elements. The present work investigates the effects of pre-straining SMA components in energy dissipation... 

    Nonlinear vibration analysis of fractional viscoelastic cylindrical shells

    , Article Acta Mechanica ; Volume 231, Issue 11 , 2020 , Pages 4683-4700 Permoon, M. R ; Haddadpour, H ; Shakouri, M ; Sharif University of Technology
    Springer  2020
    Abstract
    Nonlinear vibrations of viscoelastic thin cylindrical shells are studied in this paper. The viscoelastic properties are modeled using the Kelvin–Voigt fractional-order constitutive relationship. Based on the nonlinear Love thin shell theory, the structural dynamics of the cylindrical shell is modeled by using the Newton’s second law, and the Galerkin method is used to discretize the nonlinear partial differential equations into the set of nonlinear ordinary differential equations. The method of multiple scales is used to solve the nonlinear ordinary differential equations, and the amplitude–frequency and phase–frequency equations are extracted. The obtained results are verified with... 

    Dynamic stability analysis of a sandwich beam with magnetorheological elastomer core subjected to a follower force

    , Article Acta Mechanica ; Volume 231, Issue 9 , 2020 , Pages 3715-3727 Rokn Abadi, M ; Yousefi, M ; Haddadpour, H ; Sadeghmanesh, M ; Sharif University of Technology
    Springer  2020
    Abstract
    In the present study, the effect of using magnetorheological elastomer materials and a magnetic field on the dynamic stability of a sandwich beam under a follower force has been investigated for various boundary conditions. The considered sandwich beam consists of a magnetorheological elastomer core constrained by elastic layers. The structural governing equations are derived using Hamilton’s principle and solved by the finite element method. The validity of the result is examined by comparison with those in the literature. The effects of variation in the parameters such as magnetic field intensity and the thickness of the layers on the stability of the sandwich beam are studied. Finally,...