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    Sloshing effects on supersonic flutter characteristics of a circular cylindrical shell partially filled with liquid

    , Article International Journal for Numerical Methods in Engineering ; 2018 ; 00295981 (ISSN) Zarifian, P ; Ovesy, H. R ; Dehghani Firouz Abadi, R ; Sharif University of Technology
    John Wiley and Sons Ltd  2018
    Abstract
    This paper aims to revisit the effect of sloshing on the flutter characteristics of a partially liquid-filled cylinder. A computational fluid-structure interaction model within the framework of the finite element method is developed to capture fluid-structure interactions arising from the sloshing of the internal fluid and the flexibility of its containing structure exposed to an external supersonic airflow. The internal liquid sloshing is represented by a more sophisticated model, referred to as the liquid sloshing model, and the shell structure is modeled by Sanders' shell theory. The aerodynamic pressure loading is approximated by the first-order piston theory. The initial geometric... 

    Development of an aeroelastic model based on system identification using boundary elements method

    , Article Aircraft Engineering and Aerospace Technology ; 2021 ; 17488842 (ISSN) Dehghani Firouz Abadi, R ; Borhan Panah, M. R ; Sharif University of Technology
    Emerald Group Holdings Ltd  2021
    Abstract
    Purpose: The purpose of this paper is to analyze the stability of aeroelastic systems using a novel reduced order aeroelastic model. Design/methodology/approach: The proposed aeroelastic model is a reduced-order model constructed based on the aerodynamic model identification using the generalized aerodynamic force response and the unsteady boundary element method in various excitation frequency values. Due to the low computational cost and acceptable accuracy of the boundary element method, this method is selected to determine the unsteady time response of the aerodynamic model. Regarding the structural model, the elastic mode shapes of the shell are used. Findings: Three case studies are... 

    Effect of multiphase fluid and functionally graded density fluid on the stability of spinning partially-filled shells

    , Article International Journal of Mechanical Sciences ; Volume 140 , 2018 , Pages 109-118 ; 00207403 (ISSN) Sahebnasagh, M ; Nikkhah Bahrami, M ; Dehghani Firouz Abadi, R ; Sharif University of Technology
    Elsevier Ltd  2018
    Abstract
    The effect of a multiphase fluid, including an arbitrary number of liquid phases, and a functionally graded density fluid on the stability of rotating partially-filled cylindrical shells is investigated. The first-order shear shell theory is used for modeling the structural dynamics of the shell and a 2D model is introduced based on the Navier–Stokes equations, for fluid motion. The multiphase and the functionally graded density fluids are arranged according to the mass density in a steady state condition due to centrifugal forces. Using the boundary conditions between liquid phases and the boundary conditions of the fluid on the cylinder wall, the coupled fluid-structure system model is... 

    Hydroelastic analysis of two degree of freedom hydrofoil using a reduced-order hydrodynamic model considering unsteady partial sheet cavity flows

    , Article Journal of Fluids and Structures ; Volume 81 , 2018 , Pages 116-130 ; 08899746 (ISSN) Alavi, S. M ; Haddadpour, H ; Dehghani Firouz Abadi, R ; Sharif University of Technology
    Academic Press  2018
    Abstract
    In the present study a new, fast, precise algorithm for studying hydroelastic stability of a typical section with two degrees of freedom (2DOF) is proposed based on the finite element method (FEM), while the partial sheet cavitation effects are considered. For this means, the steady cavity boundary is calculated by some conventional iterative procedures, developed based on the potential flow simulation. Thereafter, assuming that the amplitude and the frequency of the body oscillations are altered so that the cavity length in unsteady flow remains unchanged, the simulation of the unsteady hydrodynamic flow is performed by imposing some velocity fluctuations over the rigid cavity boundary. For... 

    Flexural instability of viscoelastic spinning cylinders partially filled with liquid

    , Article International Journal of Structural Stability and Dynamics ; Volume 9, Issue 1 , 2009 , Pages 45-60 ; 02194554 (ISSN) Dehghani Firouz Abadi, R ; Haddadpour, H ; Sharif University of Technology
    2009
    Abstract
    This paper deals with the determination of free vibration characteristics and instability conditions of flexible spinning cylinders partially filled with fluid. Using the linearized Navier-Stokes equations for the incompressible, inviscid flow, a 2D model is developed for fluid motion at each section of the cylinder. The forces exerted on the cylinder wall as a result of the fluid motion are calculated as functions of lateral acceleration of the cylinder axis in the Laplace domain. Applying the Hamilton principle, the governing equations of flexural motion of the cylinder are derived and then combined with the equations describing the fluid forces to obtain the coupled field equations of the... 

    Nonlinear Vibrations of Conical Shells with Concurrent Internal and External Flows

    , Ph.D. Dissertation Sharif University of Technology Rahmanian, Mohammad (Author) ; Dehghani Firouz Abadi, Ruhollah (Supervisor)
    Abstract
    In the current study, nonlinear vibration and stability of conical shells with both separate and concurrent internal and external flows are studied. External and internal flows are in the supersonic and subsonic regimes, respectively. The Krumhar’s aerodynamic piston theory is utilized to model the external loading on the structure as well as the compressible potential flow model to capture the internal fluid dynamics. The so-called compressible fluid model is obtained via simplification of the Navier-Stockes equations after applying the inviscid and irrotational assumptions. The nonlinear structural equations of motion are derived using the Hamiltonian dynamics approach and utilizing the... 

    Nonlinear dynamics of extensible viscoelastic cantilevered pipes conveying pulsatile flow with an end nozzle

    , Article International Journal of Non-Linear Mechanics ; Volume 91 , 2017 , Pages 22-35 ; 00207462 (ISSN) Askarian, A. R ; Haddadpour, H ; Dehghani Firouz Abadi, R ; Abtahi, H ; Sharif University of Technology
    Elsevier Ltd  2017
    Abstract
    Nonlinear dynamics of an extensible cantilevered pipe conveying pulsating flow is considered in this paper. The fluid flow fluctuates harmonically and exhausts via a nozzle attached to the end of the pipe. Taking into account the extensibility assumption, the coupled nonlinear lateral–longitudinal equations of motion are derived using Hamilton's principle and discretized via Galerkin's method. The adaptive time step Adams algorithm is applied to extract the time response, and then the bifurcation, power spectral density and phase plane maps are plotted for some case studies. Effects of some geometrical parameters such as flow mass, pulsating flow frequency, gravity, nozzle mass and nozzle... 

    Bending-torsional stability analysis of aerodynamically covered pipes with inclined terminal nozzle and concurrent internal and external flows

    , Article Journal of Fluids and Structures ; Volume 94 , 2020 Askarian, A. R ; Rahmanian, M ; Haddadpour, H ; Dehghani Firouz Abadi, R ; Sharif University of Technology
    Academic Press  2020
    Abstract
    Stability analysis of a cantilevered pipe with an inclined terminal nozzle as well as simultaneous internal and external fluid flows is investigated in this study. The pipe is embedded in an aerodynamic cover with negligible mass and stiffness simply to streamline the external flow and avoid vortex induced vibrations. The structure of pipe is modeled as an Euler–Bernoulli beam and effects of internal fluid flow including flow-induced inertia, Coriolis and centrifugal forces and the follower force induced by the exhausting jet are taken into account. In addition, neglecting the compressibility effect and using the unsteady Wagner model, aerodynamic loading is determined as a distributed... 

    Prediction of in-plane elastic properties of graphene in the framework of first strain gradient theory

    , Article Meccanica ; Volume 54, Issue 1-2 , 2019 , Pages 299-310 ; 00256455 (ISSN) Hassanpour, S ; Mehralian, F ; Dehghani Firouz Abadi, R ; Borhan Panah, M. R ; Rahmanian, M ; Sharif University of Technology
    Springer Netherlands  2019
    Abstract
    In the present study, the in-plane elastic stiffness coefficients of graphene within the framework of first strain gradient theory are calculated on the basis of an accurate molecular mechanics model. To this end, a Wigner–Seitz primitive cell is adopted. Additionally, the first strain gradient theory for graphene with trigonal crystal system is formulated and the relation between elastic stiffness coefficients and molecular mechanics parameters are calculated. Thus, the ongoing research challenge on providing the accurate mechanical properties of graphene is addressed herein. Using results obtained, the in-plane free vibration of graphene is studied and a detailed numerical investigation is... 

    Prediction of in-plane elastic properties of graphene in the framework of first strain gradient theory

    , Article Meccanica ; Volume 54, Issue 1-2 , 2019 , Pages 299-310 ; 00256455 (ISSN) Hassanpour, S ; Mehralian, F ; Dehghani Firouz-Abadi, R ; Borhan Panah, M. R ; Rahmanian, M ; Sharif University of Technology
    Springer Netherlands  2019
    Abstract
    In the present study, the in-plane elastic stiffness coefficients of graphene within the framework of first strain gradient theory are calculated on the basis of an accurate molecular mechanics model. To this end, a Wigner–Seitz primitive cell is adopted. Additionally, the first strain gradient theory for graphene with trigonal crystal system is formulated and the relation between elastic stiffness coefficients and molecular mechanics parameters are calculated. Thus, the ongoing research challenge on providing the accurate mechanical properties of graphene is addressed herein. Using results obtained, the in-plane free vibration of graphene is studied and a detailed numerical investigation is... 

    Study of Aeroelastic Instability at a Panel Located in a Fully Filled Fuel Tank Wall

    , M.Sc. Thesis Sharif University of Technology Daniali, Massoud (Author) ; Dehghani Firouz-Abadi, Rouhollah (Supervisor)
    Abstract
    One of the classic problems in the aeroelasticity field is panel Fluttr that occurs in supersonic flow. Panels as wing skins, fuselage missile, and so are prone to this phenomenon, which causes fatigue and structures, will be demolished.In many cases, the wall panels and a full tank of fuel, this in this case, the vibration of the fluid-filled panels will be affected. There is clearly fluid into a tank filled with considering the approximation of incompressible fluid dynamics and vibration modes of the panel will change. In this study, a three-dimensional rectangular tank is considered the high walls on the elastic and supersonic flow passes.Fuel density and structural dimensions of Full... 

    Calculating the Stiffness Matrix of VACNTs Using Structural or Continuum Modelling

    , M.Sc. Thesis Sharif University of Technology Vahidmoshtagh, Alireza (Author) ; Dehghani Firouz Abadi, Ruhollah (Supervisor)
    Abstract
    The goal of this research is investigation and analysis of a surface consists of vertically aligned carbon nanotubes (VACNTs) using continuum mechanics modeling. Today these kinds of surfaces also known as the darkest material have a particular importance in industries. Knowing the properties of a material is one of the most important things in analysis and designing using that kind of material, so extraxting the stiffness matrix of a material could be a big step for starting analyzing it. In this thesis a lattice of VACNTs with two different layouts and several unique geometrics is simulated using molecular dynamics approach using the Lammps software. The general stiffness matrix of the... 

    Nonlinear Aeroelastic Analysis of Composite Wing at a Hale Flight Vehicle

    , M.Sc. Thesis Sharif University of Technology Besharatlou, Mohammad (Author) ; Dehghani Firouz-Abadi, Roholla (Supervisor)
    Abstract
    The purpose of this study is aeroelastic stability analysis and nonlinear aeroelastic vibration of composite wing with nonlinear 1D beam model. Wing’s structure modelled as thin-walled composite single box beam in linear and nonlinear conditions. Thin-walled composite box beam developed by classical lamination theory and structural nonlinearity is von karman strain. Unsteady aerodynamic of wing modelled with modified strip theory. Aeroelastic equations of wing obtained from modal expansion (assumed mode) and Hamilton’s Principle. In order to stability analysis of wing, the linear aeroelastic equations in state space must be calculated and so with eigenvalue analysis instability speed will be... 

    A 3D BEM model for liquid sloshing in baffled tanks

    , Article International Journal for Numerical Methods in Engineering ; Volume 76, Issue 9 , June , 2008 , Pages 1419-1433 ; 00295981 (ISSN) Dehghani Firouz Abadi, R ; Haddadpour, H ; Noorain, M. A ; Ghasemi, M ; Sharif University of Technology
    2008
    Abstract
    The present work aims at developing a boundary element method to determine the natural frequencies and mode shapes of liquid sloshing in 3D baffled tanks with arbitrary geometries. Green's theorem is used with the governing equation of potential flow and the walls and free surface boundary conditions are applied. A zoning method is introduced to model arbitrary arrangements of baffles. By discretizing the flow boundaries to quadrilateral elements, the boundary integral equation is formulated into a general matrix eigenvalue problem. The governing equations are then reduced to a more efficient form that is merely represented in terms of the potential values of the free surface nodes, which... 

    Reverse time migration by Krylov subspace reduced order modeling

    , Article Journal of Applied Geophysics ; Volume 151 , April , 2018 , Pages 298-308 ; 09269851 (ISSN) Mahdavi Basir, H ; Javaherian, A ; Shomali, Z. H ; Dehghani Firouz Abadi, R ; Gholamy, S. A ; Sharif University of Technology
    Elsevier B.V  2018
    Abstract
    Imaging is a key step in seismic data processing. To date, a myriad of advanced pre-stack depth migration approaches have been developed; however, reverse time migration (RTM) is still considered as the high-end imaging algorithm. The main limitations associated with the performance cost of reverse time migration are the intensive computation of the forward and backward simulations, time consumption, and memory allocation related to imaging condition. Based on the reduced order modeling, we proposed an algorithm, which can be adapted to all the aforementioned factors. Our proposed method benefit from Krylov subspaces method to compute certain mode shapes of the velocity model computed by as... 

    Optimization of nonlinear unbalanced flexible rotating shaft passing through critical speeds

    , Article International Journal of Structural Stability and Dynamics ; Volume 22, Issue 1 , 2022 ; 02194554 (ISSN) Amirzadegan, S ; Rokn Abadi, M ; Firouz Abadi, R. D ; Sharif University of Technology
    World Scientific  2022
    Abstract
    This work studies the nonlinear oscillations of an elastic rotating shaft with acceleration to pass through the critical speeds. A mathematical model incorporating the Von-Karman higher-order deformations in bending is developed to investigate the nonlinear dynamics of rotors. A flexible shaft on flexible bearings with springs and dampers is considered as rotor system for this work. The shaft is modeled as a beam and the Euler-Bernoulli beam theory is applied. The kinetic and strain energies of the rotor system are derived and Lagrange method is then applied to obtain the coupled nonlinear differential equations of motion for 6 degrees of freedom. In order to solve these equations... 

    Investigation of Stability and Electromechanical Properties of a Nano Capacitor Made of Two Graphene Sheets

    , M.Sc. Thesis Sharif University of Technology Borhanpanah Mooshaki, Mohammad Reza (Author) ; Dehghani Firouz-Abadi, Rouhollah (Supervisor)
    Abstract
    Investigation of electrostatic properties of a nano capacitor made of graphene sheets, is the aim of current research. This nano capacitor is made of two adjacent parallel gr¬aphene sheets. Applying a voltage make an electric field between the sheets, which attracts the sheets together. This change in geometry, affects the electric field between sheets, therefore, the sheet's deformation and the electric field between them are coupled to each other. For modeling the deformation of the sheets, molecular dynamics analysis is employed. The electrostatic equations are used for modeling the electric field. The electric field is assumed to be static in this research, which means that the... 

    Free vibrations of single-walled carbon nanotubes in the vicinity of a fully constrained graphene sheet

    , Article Computational Materials Science ; Volume 53, Issue 1 , 2012 , Pages 12-17 ; 09270256 (ISSN) Firouz Abadi, R. D ; Hosseinian, A. R ; Sharif University of Technology
    2012
    Abstract
    Carbon nanotubes (CNTs) have been recently taken into consideration as mechanical resonators of distinguished capabilities. This study aims at investigating the free vibration characteristics of a single-walled CNT in the vicinity of a fully constrained graphene sheet. Using a molecular structural mechanics model and considering nonlinear van-der-Waals interactions, the static deformation of the nanotube is obtained using an iterative procedure. Then, the governing equations of motion are linearized about the static equilibrium state and the natural frequencies are obtained. The molecular structural mechanics model is verified using established results in literature and then a survey is... 

    Effect of liquid viscosity on instability of high-spinning partially-filled shell rotors

    , Article International Journal of Structural Stability and Dynamics ; Volume 13, Issue 6 , 2013 ; 02194554 (ISSN) Firouz Abadi, R. D ; Permoon, M. R ; Sharif University of Technology
    2013
    Abstract
    In this study, the instability of spinning cylindrical shells partially filled with viscous liquid is investigated. Based on the Navier-Stokes equations for the incompressible flow, a 2D model is developed for liquid motion at each section of the cylinder. The governing equations of the cylinder vibrations are obtained based on the first-order shear deformable shell theory. The nonpenetration and no-slip boundary conditions of the flow on the wetted surface of the cylinder relate the liquid motion to the shell vibrations. Also the liquid pressure exerted on the cylinder wall combines the vibrations of the rotary cylinder to the liquid motion. By using the obtained coupled liquid-structure... 

    Magnetoelastic instability of a long graphene nano-ribbon carrying electric current

    , Article Advances in Applied Mathematics and Mechanics ; Vol. 6, issue. 3 , 2014 , pp. 299-306 ; ISSN: 20700733 Firouz-Abadi, R. D ; Mohammadkhani, H ; Sharif University of Technology
    2014
    Abstract
    This paper aims at investigating the resonance frequencies and stability of a long Graphene Nano-Ribbon (GNR) carrying electric current. The governing equation of motion is obtained based on the Euler-Bernoulli beam model along with Hamilton's principle. The transverse force distribution on the GNR due to the interaction of the electric current with its own magnetic field is determined by the Biot-Savart and Lorentz force laws. Using Galerkin's method, the governing equation is solved and the effect of current strength and dimensions of the GNR on the stability and resonance frequencies are investigated