Active vibration control of composite shallow shells: An integrated approach

被引:9
|
作者
Rahman, N. [1 ]
Alam, M. N. [1 ]
Junaid, M. [1 ]
机构
[1] Aligarh Muslim Univ, Zakir Husain Coll Engn & Technol, Dept Mech Engn, Aligarh 202002, UP, India
关键词
Shell; composite; finite element modeling; ABAQUS; constant gain velocity feedback; linear quadratic regulator;
D O I
10.15282/jmes.12.1.2018.6.0300
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Active vibration control of smart composite shallow shells with distributed piezoelectric sensors and actuators is presented in this work. An integrated approach is used for recording the uncontrolled and controlled vibration response under pressure impulse load. The FE model developed in ABAQUS is utilized to generate the global mass, stiffness and load matrices of the system. The system matrices are arranged in state space format and the dynamic equations of the system are obtained. The controlled responses are achieved using the inputs from FE model in ABAQUS in conjunction with the developed MATLAB codes for Constant Gain Velocity Feedback (CGVF) and Linear Quadratic Regulator (LQR) control strategies. The method is first validated by comparing the natural frequencies obtained using the ABAQUS generated matrices with that obtained using an FE model with four noded quadrilateral shallow shell element based on efficient zigzag theory. The shell element uses the concept of electric nodes to satisfy the equipotential condition of electrode surface. An 8-noded linear piezoelectric brick element is used for piezoelectric layers and an 8-noded quadrilateral continuum shell element is used for the elastic layers of hybrid shells for making the finite element mesh in ABAQUS. The non-dimensional natural frequencies and active vibration control responses for hybrid composite cylindrical and spherical shells are presented for clamped-clamped and cantilever boundary conditions. Boundary conditions have significant effect on vibration amplitude, control voltage and settling time. In comparison to CGVF controller, a better control in lesser time is achieved with LQR controller for a shell with similar boundary conditions. Larger gain values (G) are required for vibration control of thick shells.
引用
收藏
页码:3354 / 3369
页数:16
相关论文
共 50 条
  • [1] Coupled efficient layerwise finite element modeling for active vibration control of smart composite and sandwich shallow shells
    Kapuria, S.
    Yasin, M. Yaqoob
    [J]. JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2014, 25 (16) : 2013 - 2036
  • [2] Active Vibration Control of Truncated Conical Porous Smart Composite Shells
    Ebrahimi, Farzad
    Mollazeinal, Ali
    Ahari, Mehrdad Farajzadeh
    [J]. INTERNATIONAL JOURNAL OF STRUCTURAL STABILITY AND DYNAMICS, 2024, 24 (12)
  • [3] Active vibration control of double wall composite shells to random inputs
    Wang, CY
    Vaicaitis, R
    [J]. PROBABILISTIC MECHANICS & STRUCTURAL RELIABILITY: PROCEEDINGS OF THE SEVENTH SPECIALTY CONFERENCE, 1996, : 842 - 845
  • [4] Vibration of cantilevered laminated composite shallow conical shells
    Lim, CW
    Liew, KM
    Kitipornchai, S
    [J]. INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1998, 35 (15) : 1695 - 1707
  • [5] Thermally induced vibration control of composite plates and shells with piezoelectric active damping
    Raja, S
    Sinha, PK
    Prathap, G
    Dwarakanathan, D
    [J]. SMART MATERIALS & STRUCTURES, 2004, 13 (04): : 939 - 950
  • [6] On Nonlinear Vibration Analysis of Shallow Shells - A New Approach
    Banerjee, M. M.
    Mazumdar, J.
    [J]. VIBRATION PROBLEMS ICOVP 2011, 2011, 139 : 51 - 58
  • [7] Free vibration of pretwisted, cantilevered composite shallow conical shells
    Lim, CW
    Liew, KM
    Kitipornchai, S
    [J]. AIAA JOURNAL, 1997, 35 (02) : 327 - 333
  • [8] Free vibration analysis of pretwisted delaminated composite stiffened shallow shells: A finite element approach
    Rout, Mrutyunjay
    Bandyopadhyay, Tanmoy
    Karmakar, Amit
    [J]. JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2017, 36 (08) : 619 - 636
  • [9] Stochastic free vibration analyses of composite shallow doubly curved shells - A Kriging model approach
    Dey, Sudip
    Mukhopadhyay, Tanmoy
    Adhikari, Sondipon
    [J]. COMPOSITES PART B-ENGINEERING, 2015, 70 : 99 - 112
  • [10] Modeling of piezolaminated composite shells for vibration control
    Piéfort, V
    Loix, N
    Preumont, A
    [J]. EUROPEAN CONFERENCE ON SPACECRAFT STRUCTURES, MATERIALS AND MECHANICAL TESTING, PROCEEDINGS, 1999, 428 : 525 - 530