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    Sloshing analysis of flowing liquid in 3D tank using boundary elements method

    , Article Journal of Pressure Vessel Technology, Transactions of the ASME ; Volume 135, Issue 2 , 2013 ; 00949930 (ISSN) Firouz Abadi, R. D ; Borhan Panah, M. R ; Sharif University of Technology
    2013
    Abstract
    A numerical model based on the boundary element method is proposed for the sloshing of a flowing liquid in a three-dimensional tank. Assuming a mean flow in the tank in addition to a perturbation flow, the nonlinear boundary conditions of the liquid free-surface are linearized. Using the boundary element method along with the modal analysis technique a reduced order model is obtained which is used to calculate the fundamental sloshing frequencies and modes in the tank with an inlet and outlet. The obtained results for a test case are compared with the literature data to validate the proposed model. The results are in a very good agreement with analytical results and show an acceptable... 

    Equivalent mechanical model of liquid sloshing in multi-baffled containers

    , Article Engineering Analysis with Boundary Elements ; Vol. 47, issue. 1 , Octobe , 2014 , p. 82-95 Ebrahimian, M ; Noorian, M. A ; Haddadpour, H ; Sharif University of Technology
    Abstract
    This study presents a method to determine an equivalent mechanical model (EMM) for multi-baffled containers with arbitrary geometries. The method is implemented for 2D and axisymmetric containers. The Laplace equation and Green's theorem are used to develop the fluid model and the boundary element method (BEM) is used to solve the fluid field governing equation. Moreover, a zoning method is utilized to model arbitrary arrangements of baffles in multi-baffled containers and a reduced order model is developed to model the free-surface sloshing. The exerted hydrodynamic pressure distribution, forces and moments on the walls of the container are determined based on the Bernoulli equation and a... 

    3D Modeling and nonlinear Control of a Satellite with 3D Fuel Slosh Dynamics

    , M.Sc. Thesis Sharif University of Technology Janalipour Shahrani, Alireza (Author) ; Fathi, Mohsen (Supervisor)
    Abstract
    The thrust vector control problem is studied for a Satellite with fuel slosh dynamics. The sloshing propellant is modeled as a 3D pendulum. The coupled equations of motion of the satellite and the fuel are expressed in terms of the three dimensional satellite translational velocity vector, the attitude, the angular velocity, and the internal coordinates representing the slosh modes. A nonlinear feedback control law with the idea of backstepping integrator is proposed to control the translational velocity vector and the attitude of the satellite, while attenuating the sloshing modes. A simulation example is included to illustrate the effectiveness of the control law  

    A boundary element method for investigation of sloshing in complex 3D containers

    , Article 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Waikiki, HI, 23 April 2007 through 26 April 2007 ; Volume 8 , 2007 , Pages 8288-8292 ; 02734508 (ISSN); 1563478927 (ISBN); 9781563478925 (ISBN) Firouz Abadi, R. D ; Haddadpour, H ; Ghasemi, M ; Sharif University of Technology
    2007
    Abstract
    This paper presents a matrix form model for determination of sloshing frequencies and modes in 3D liquid tanks. The governing equations of the incompressible inviscid potential flow are used to derive the governing boundary integral equation and then the boundary element method along with the collocation method is applied to obtain a matrix form standard eigenvalue problem. The sloshing mass and stiffness matrices are computed using analytical formulas which are given for quadratic boundary elements. Two typical examples are used to validate the introduced model and very good results are achieved in comparison with the exact results in the literature  

    Surface Waves Propagation in a Piezoelectric/Piezomagnetic Half Space Overlaid With a Finnite Layer

    , M.Sc. Thesis Sharif University of Technology Soltanian Fard, Mohammad Amin (Author) ; Skandari, Morteza (Supervisor)
    Abstract
    The propagation of the surface waves in the piezoelectric (PE) and piezomagnetic (PM) layered media are studied. The surface BG waves in the PE half-spaces overlaid by a layer are considered and the closed-form dispersion relations for the open and short electromechanical surface boundary conditions are obtained. The numerical results for the phase velocities and the electromechanical coupling factor for PZT-2 and PZT-8 media are presented. Furthermore, the propagation of the Rayleigh waves in the PE-PM layered media is considered. The effects of the imperfect bonding between the half-space and the layer are discussed. Later, we study the propagation of the Rayleigh waves in 4 different... 

    A reduced order model for liquid sloshing in tanks with flexible baffles using boundary element method

    , Article International Journal for Numerical Methods in Engineering ; Volume 89, Issue 13 , 2012 , Pages 1652-1664 ; 00295981 (ISSN) Noorian, M. A ; Firouz Abadi, R. D ; Haddadpour, H ; Sharif University of Technology
    2012
    Abstract
    In order to study the interaction of sloshing and structural vibrations of baffled tanks, a reduced order model based on modal analysis of structure model and boundary element method for fluids motion is developed. For this purpose, the governing equations of elastic structure and incompressible flow are used to derive simple models to simulate both fields. Using the modal analysis technique, the structural motions are applied to the fluid model and on the other hand by using boundary element method, the fluid loads are applied to the structural model. Based on this formulation, a code is developed which is applicable to an arbitrary elastic tank with arbitrary arrangement of baffles. The... 

    Numerical modeling of sloshing frequencies in tanks with structure using new presented DQM-BEM technique

    , Article Symmetry ; Volume 12, Issue 4 , 2020 Wei, Z ; Feng, J ; Ghalandari, M ; Maleki, A ; Abdelmalek, Z ; Sharif University of Technology
    MDPI AG  2020
    Abstract
    The sloshing behavior of systems is influenced by different factors related to the liquid level and tank specifications. Different approaches are applicable for the assessment of sloshing behavior in a tank. In this paper, a new numerical model based on the differential quadrature method and boundary element approaches is adopted to investigate the sloshing behavior of a tank with an elastic thin-walled beam. The model is developed based on small slope considerations of the free surface. The main assumption of fluid modeling is homogeneity, isotropy, inviscid, and only limited compressibility of the liquid. Indeed, the formulation is represented based on the reduced-order method and then is... 

    New mathematical model to analysis fluid sloshing in 3D tanks with slotted middle baffle

    , Article Ocean Engineering ; Volume 262 , 2022 ; 00298018 (ISSN) Jamshidi, S ; Firouz Abadi, R. D ; Amirzadegan, S ; Sharif University of Technology
    Elsevier Ltd  2022
    Abstract
    This work studies the natural frequencies and modes of liquid sloshing in a rectangular 3D tank with the slotted baffles in middle. A new vibrational model incorporating the pressure difference between the two sides of the baffle, using a transmission function in Laplace space is presented. To this end, a part of the baffle that includes the wall and the slot is modeled in Fluent software, to express this pressure difference as a function of the fluid velocity passing through the baffle. Then, using the boundary element method, and boundary conditions, the equations of the fluid domain are developed. In this research, the rigid baffle is surrounded by a three-dimensional irrotational... 

    On the Flutter of Swept Taper Wing in Subsonic Compressible Flow Considering Effect of Fuel Sloshing in External Stores

    , M.Sc. Thesis Sharif University of Technology Beheshtinia, Farshad (Author) ; Dehghani Firoozabadi, R (Supervisor)
    Abstract
    In the present work, the aeroelastic stability analysis for the swept taper wing and external fuel tank combination system in subsonic compressible flow are represented. The wing structure is modeled by using the Euler-Bernoulli beam theory. Fuel sloshing is modeled by using an equivalent mechanical mass-spring-damper model. Modal analysis technique is used to drive the structural equations of motion of the system. Aeorodynamic of wing is modeled by using index aerodynamic that has been dived by Marzocca and a slender body aerodynamic theory for the external fuel tank are used. For stability analysis, k-method redrived for a case that structural damping there is. The effects of the external... 

    Multidisciplinary Design Optimization of an Air Launch Satellite Launch Vehicle by Considering the Coupled Slosh–vehicle Dynamics

    , M.Sc. Thesis Sharif University of Technology Keshavarz Mohammadian, Moein (Author) ; Fathi, Mohsen (Supervisor)
    Abstract
    In this thesis, the multidisciplinary design of liquid propellant satellite launch vehicle has been done by taking into consideration the effects of fuel sloshing. At first, the theory of multidisciplinary design and one-level architecture with the label of multidisciplinary feasibility have been used. In the following, Gravitational Search Algorithm (GSA) and Particle swarm optimization (PSO) have been developed. Then, the multidisciplinary design cycle began with the design of the liquid propellant system. In the propulsion section, the selection of the optimal fuel, the design of the nozzle, motor and the selection of the optimal engine cycle considering the geometric and mass... 

    Rayleigh Waves Propagation in a Piezoelectric Layered Half-space with Imperfect Interface

    , M.Sc. Thesis Sharif University of Technology Sheikh Bagher Mohajer, Mohammad Mahdi (Author) ; Eskandari, Morteza (Supervisor)
    Abstract
    The problem of the Rayleigh wave propagation in a piezoelectric layer overlying a piezoelectric half space by an imperfect interface is investigated. These days because of widespread use of the piezoelectric materials in sensors and transducers based on surface waves, the study of wave propagation in these medias is paid attention by many researchers. In this study, imperfection between layer and half-space idealized by springs which have determine values. If the stiffness of springs approaches to infinity, the interface will be perfect. Also, zero stiffness of springs indicates that there is no continuity between layer and half space. With the use of potential functions for displacement... 

    Theoretical and Experimental Analysis of Fluid Sloshing on a Flying Object

    , M.Sc. Thesis Sharif University of Technology Abbasi, Mohammad Hossein (Author) ; Durali, Mohammad (Supervisor)
    Abstract
    Slosh phenomenon is described as the motion of the fluid’s free surface in a tank or partially-filled container. This motion can induce undesired forces that can change the path of a vehicle. In some liquid carrying vehicles these undesired changes is sensed by the driver or control system and can lead to instability. Some examples of this phenomenon are aircrafts, rockets, ships and fuel carrier trucks.
    In this project, a coupling between the dynamics of the vehicle and the contained fluid is implemented for in depth understanding of the interactions. This is done by Co-Simulation. With the help of Co-Simulation, corrective control actions can be taken and the design of more powerful... 

    Sloshing Analysis of Rectangular Container with Perforated Baffle

    , M.Sc. Thesis Sharif University of Technology Merikhnezhad, Atieh (Author) ; Dehghani Firouzabadi, Rooholah (Supervisor)
    Abstract
    In this thesis, sloshing of a rectangular container with perforated baffle is being analysed. Employing the linear sloshing theorem, we construct an accurate numerical and analytical approximation of natural sloshing mode in rectangular container with perforated baffle. Two dimensional irrotational flow of an ideal incompressible liquid is assumed. Finally the dissipated energy is being measured and equal viscous damping was calculated. So the perforation in which the damping is being maximized is determined and finally the results being compared with some experimental and analytical results from journal paper  

    Stability analysis of elastic launch vehicles with fuel sloshing in planar flight using a BEM-FEM model

    , Article Aerospace Science and Technology ; Volume 53 , 2016 , Pages 74-84 ; 12709638 (ISSN) Noorian, M. A ; Haddadpour, H ; Ebrahimian, M ; Sharif University of Technology
    Elsevier Masson SAS  2016
    Abstract
    A numerical model is developed for investigation of coupled dynamics of fuel contained elastic launch vehicles in planar atmospheric flight. Finite element method along with the linear quasi-steady piston aerodynamic theory is used for developing an aeroelastic model. A reduced order boundary element model is used for modeling the liquid sloshing in tanks. The interaction of sloshing and aeroelasticity is studied using stability analysis of the coupled system. Results show that the slosh-aeroelastic coupling in an elastic launch vehicle occurs for low tank filling ratios and may lead to decreasing the system damping. Due to more interactions between the slosh and rigid body modes, larger... 

    Reduced order modeling of liquid sloshing in 3D tanks using boundary element method

    , Article Engineering Analysis with Boundary Elements ; Volume 33, Issue 6 , 2009 , Pages 750-761 ; 09557997 (ISSN) Dehghani Firouzabadi, R ; Haddadpour, H ; Ghasemi, M ; Sharif University of Technology
    2009
    Abstract
    This paper presents the application of reduced order modeling technique for investigation of liquid sloshing in three-dimensional tanks. The governing equations of sloshing are written using a boundary element formulation for incompressible potential flow. Then, the governing equations are reduced to a more efficient form that is represented only in terms of the velocity potential on the liquid free surface. This particular form is employed for eigen-analysis of fluid motion and the sloshing frequencies and mode shapes are determined. Then, the sloshing frequencies and the corresponding right- and left-eigenvectors are used along the modal analysis technique to find a reduced order model... 

    Satellite attitude PDE-based controller design considering fluid fuel sloshing in planar maneuver

    , Article Aerospace Science and Technology ; Volume 122 , 2022 ; 12709638 (ISSN) Jokar, M ; Salarieh, H ; Nejat Pishkenari, H ; Sharif University of Technology
    Elsevier Masson s.r.l  2022
    Abstract
    Due to significance of high-accuracy attitude control, the fuel sloshing effects on the satellite attitude should be considered, more precisely. This work deals with the attitude control of a liquid propellant-filled satellite considering the incompressible fuel sloshing in the planar maneuver. The satellite consists of a rigid body, a partially-filled tank and a flexible diaphragm. Hamilton's principle is employed to derive nonlinear coupled PDEs-ODEs governing the coupled satellite-diaphragm propellant tank system. Afterwards, to dispense with the spillover instability, a PDE-based controller is designed to realize the satellite attitude control while tracking a desired pitch angle and... 

    Two phase modal analysis of nonlinear sloshing in a rectangular container

    , Article Ocean Engineering ; Volume 38, Issue 11-12 , August , 2011 , Pages 1277-1282 ; 00298018 (ISSN) Ansari, M. R ; Firouz Abadi, R. D ; Ghasemi, M ; Sharif University of Technology
    2011
    Abstract
    Sloshing, or liquid free surface oscillation, in containers has many important applications in a variety of engineering fields. The modal method can be used to solve linear sloshing problems and is the most efficient reduced order method that has been used during the previous decade. In the present article, the modal method is used to solve a nonlinear sloshing problem. The method is based on a potential flow solution that implements a two-phase analysis on sloshing in a rectangular container. According to this method, the solution to the mass conservation equation, with a nonpenetration condition at the tank walls, results in velocity potential expansion; this is similar to the mode shapes... 

    Love Wave Propagation in a Functionally Graded Magneto-Electro-Elastic Half-Space with Quadratic Variations

    , M.Sc. Thesis Sharif University of Technology Nobahar, Masoud (Author) ; Eskandari, Morteza (Supervisor)
    Abstract
    The propagation behavior of Love wave in functionally graded magneto-electro-elastic half-spaces with a quadratic variation is addressed. The magneto-electromechanical coupling factor, the dispersion relations, electric potential, magnetic potential and displacement are obtained analytically for both magneto-electrically open and short conditions. The effect of gradient coefficient on phase velocity, group velocity and magneto-electromechanical coupling factor are plotted and discussed. Research on the wave propagation in magneto-electro-elastic materials is still very limited. This work provides us with a theoretical foundation to design and practically apply SAW devices with high... 

    A FEM-BEM Model for Investigation of Fuel SlushingEffect on the Supersonic Wing Aeroelasticity

    , M.Sc. Thesis Sharif University of Technology Zanjanizadeh Esfahani, Mohammad Javad (Author) ; Haddadpour, Hassan (Supervisor)
    Abstract
    In the present work the stability analysis for the coupled aeroelasticity and fuel sloshing in supersonic wings is represented. The wing and store structure is modeled using the finite element method. The supersonic wing aerodynamic is modeled by the linear piston theory and store aerodynamic is modeled by the semi-stable slender body piston theory. Fuel sloshing in the store with desired geometry is modeled by the boundary element method. The coupled structure, aerodynamic and sloshing governing equations are drawn by using the Galerkin method and reduce order modeling teqnique for them and an effective numerical model was developed that is capable to analyze the stability for... 

    Computational Simulation of a 2D Sloshing Flow in a Rectangular Tank with Baffle, Using LBM

    , M.Sc. Thesis Sharif University of Technology Goudarzi, Saman (Author) ; Tayyebi Rahni, Mohammad (Supervisor)
    Abstract
    In the this study, a numerical simulation of two-dimensional incompressible sloshing flow in a rectangular tank with baffle(s), using Lattice Boltzmann Method (LBM) is presented. Finite difference LBM and two-phase "Lee" model were used. The potential form of intermolecular forces is utilized to guarantee the stability of the numerical scheme and the discretization of the solution domain is performed by a two dimensional structured grid. Two different distribution functions are applied to obtain pressure, momentum, and composition of the particles. Furthermore, the Boltzmann transport equation is discretized, by using standard D2Q9 method. The "dropl" test case is simulated by the present...