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    Stability analysis of carbon nanotubes using a hybrid atomistic-structural element

    , Article International Journal of Nanomanufacturing ; Volume 5, Issue 3-4 , 2010 , Pages 366-375 ; 17469392 (ISSN) Sadeghi, M ; Naghdabadi, R ; Sharif University of Technology
    2010
    Abstract
    In this paper, a hybrid atomistic-structural element for studying the mechanical behaviour of carbon nanotubes is introduced. Non-linear formulation for this element is derived based on empirical inter-atomic potentials. This hybrid element is capable of taking into account the non-linear nature of inter-atomic forces as well as the non-linearity arising from large deformations. Using these capabilities, the stability analysis of carbon nanotubes under axial compressive loading is performed and the post-buckling behaviour is predicted. Also, the dependence of axial buckling force on nanotube radius is shown  

    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... 

    Stability of single-walled carbon nanopeapods under combined axial compressive load and external pressure

    , Article Physica E: Low-Dimensional Systems and Nanostructures ; Volume 41, Issue 3 , 2009 , Pages 513-517 ; 13869477 (ISSN) Najafi Sohi, A ; Naghdabadi, R ; Sharif University of Technology
    Elsevier  2009
    Abstract
    In this paper, the axial stability of single-walled carbon nanopeapods is studied based on an elastic continuum shell model. In order to model the non-bonded van der Waals interactions between host carbon nanotube and guest fullerenes, an equivalent pressure distribution is proposed and incorporated in the model. Deriving an explicit equation for the determination of critical axial load, it is concluded that the axial stability of a single-walled carbon nanopeapod is less than that of a carbon nanotube under otherwise identical conditions. In addition, it is shown that applying external pressure to the carbon nanopeapod decreases the axial compressive stability through reducing the critical... 

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

    , Article International Journal for Numerical Methods in Engineering ; Volume 117, Issue 8 , 2019 , Pages 901-925 ; 00295981 (ISSN) Zarifian, P ; Ovesy, H. R ; Firouz Abadi, R. D ; Sharif University of Technology
    John Wiley and Sons Ltd  2019
    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... 

    Vibration control and manufacturing of intelligibly designed axially functionally graded cantilevered macro/micro-tubes

    , Article 13th IFAC Workshop on Intelligent Manufacturing Systems, IMS 2019, 12 August 2019 through 14 August 2019 ; Volume 52, Issue 10 , 2019 , Pages 382-387 ; 24058963 (ISSN) Mirtalebi, H ; Ebrahimi Mamaghani, A ; Ahmadian, M. T ; Barari A ; Sharif University of Technology
    Elsevier B.V  2019
    Abstract
    In the last decade, extensive attention is devoted to intelligibly designed materials of macro/micro-structures containing the fluid flow. In this study, intelligent control and vibrational stability of cantilevered fluid conveying macro/micro-tubes utilizing axially functionally graded (AFG) materials are considered. The governing equation of motion of the system is derived based on modified couple stress theory and then is discretized using Galerkin method. A detailed investigation is carried out to elaborate the influence of various parameters such as material properties, axial compressive load, and Pasternak foundation on the dynamical behavior of the system, all of which are influential... 

    Vibration control and manufacturing of intelligibly designed axially functionally graded cantilevered macro/micro-tubes

    , Article 13th IFAC Workshop on Intelligent Manufacturing Systems, IMS 2019, 12 August 2019 through 14 August 2019 ; Volume 52, Issue 10 , 2019 , Pages 382-387 ; 24058963 (ISSN) Mirtalebi, H ; Ebrahimi Mamaghani, A ; Ahmadian, M. T ; Sharif University of Technology
    Elsevier B.V  2019
    Abstract
    In the last decade, extensive attention is devoted to intelligibly designed materials of macro/micro-structures containing the fluid flow. In this study, intelligent control and vibrational stability of cantilevered fluid conveying macro/micro-tubes utilizing axially functionally graded (AFG) materials are considered. The governing equation of motion of the system is derived based on modified couple stress theory and then is discretized using Galerkin method. A detailed investigation is carried out to elaborate the influence of various parameters such as material properties, axial compressive load, and Pasternak foundation on the dynamical behavior of the system, all of which are influential...