Active control of free and forced vibration of rotating laminated composite cylindrical shells embedded with magnetostrictive layers based on classical shell theory

In this study, active control of free and forced vibration of rotating thin laminated composite cylindrical shells embedded with two magnetostrictive layers is investigated by means of classical shell theory. The shell is subjected to harmonic load which is exerted to inner surface of the shell in t...

Full description

Saved in:
Bibliographic Details
Main Authors: Shahin Mohammadrezazadeh, Ali Asghar Jafari
Format: Article
Language:English
Published: Semnan University 2020-11-01
Series:Mechanics of Advanced Composite Structures
Subjects:
Online Access:https://macs.semnan.ac.ir/article_4462_ebead7618fd19867d7460a29ecac3e38.pdf
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1850116591841181696
author Shahin Mohammadrezazadeh
Ali Asghar Jafari
author_facet Shahin Mohammadrezazadeh
Ali Asghar Jafari
author_sort Shahin Mohammadrezazadeh
collection DOAJ
description In this study, active control of free and forced vibration of rotating thin laminated composite cylindrical shells embedded with two magnetostrictive layers is investigated by means of classical shell theory. The shell is subjected to harmonic load which is exerted to inner surface of the shell in thickness direction.  The velocity feedback control method is used in order to obtain the control law. The vibration equations of the rotating cylindrical shell are extracted by means of Hamilton principle while the effects of initial hoop tension, centrifugal and Coriolis accelerations are considered in the vibration equations. The differential equations of the rotating cylindrical shell are converted to ordinary differential equations by means of modified Galerkin method.  The displacement of the shell is obtained using modal analysis. The free vibration results of this study are validated by comparison with the results of open literature. Also, the validity of the forced vibration results is proved by comparison with the fourth order Runge-Kutta method's result. Finally, the effects of several parameters including circumferential wave number, rotational velocity, the whole orthotropic layers thickness, magnetostrictive layers thickness, length, the amplitude and exciting frequency of the load on the vibration characteristics of the rotating cylindrical shell are investigated.
format Article
id doaj-art-2946b7471b9f49ffab322ca07929d9a0
institution OA Journals
issn 2423-4826
2423-7043
language English
publishDate 2020-11-01
publisher Semnan University
record_format Article
series Mechanics of Advanced Composite Structures
spelling doaj-art-2946b7471b9f49ffab322ca07929d9a02025-08-20T02:36:16ZengSemnan UniversityMechanics of Advanced Composite Structures2423-48262423-70432020-11-017235536910.22075/macs.2020.16921.11914462Active control of free and forced vibration of rotating laminated composite cylindrical shells embedded with magnetostrictive layers based on classical shell theoryShahin Mohammadrezazadeh0Ali Asghar Jafari1Faculty of Mechanical Engineering, K. N. Toosi University of Technology, Tehran 1991943344, IranFaculty of Mechanical Engineering, K. N. Toosi University of Technology, Tehran 1991943344, IranIn this study, active control of free and forced vibration of rotating thin laminated composite cylindrical shells embedded with two magnetostrictive layers is investigated by means of classical shell theory. The shell is subjected to harmonic load which is exerted to inner surface of the shell in thickness direction.  The velocity feedback control method is used in order to obtain the control law. The vibration equations of the rotating cylindrical shell are extracted by means of Hamilton principle while the effects of initial hoop tension, centrifugal and Coriolis accelerations are considered in the vibration equations. The differential equations of the rotating cylindrical shell are converted to ordinary differential equations by means of modified Galerkin method.  The displacement of the shell is obtained using modal analysis. The free vibration results of this study are validated by comparison with the results of open literature. Also, the validity of the forced vibration results is proved by comparison with the fourth order Runge-Kutta method's result. Finally, the effects of several parameters including circumferential wave number, rotational velocity, the whole orthotropic layers thickness, magnetostrictive layers thickness, length, the amplitude and exciting frequency of the load on the vibration characteristics of the rotating cylindrical shell are investigated.https://macs.semnan.ac.ir/article_4462_ebead7618fd19867d7460a29ecac3e38.pdfactive vibration controlclassical shell theorymodified galerkin methodmagnetostrictive layersrotating laminated composite cylindrical shell
spellingShingle Shahin Mohammadrezazadeh
Ali Asghar Jafari
Active control of free and forced vibration of rotating laminated composite cylindrical shells embedded with magnetostrictive layers based on classical shell theory
Mechanics of Advanced Composite Structures
active vibration control
classical shell theory
modified galerkin method
magnetostrictive layers
rotating laminated composite cylindrical shell
title Active control of free and forced vibration of rotating laminated composite cylindrical shells embedded with magnetostrictive layers based on classical shell theory
title_full Active control of free and forced vibration of rotating laminated composite cylindrical shells embedded with magnetostrictive layers based on classical shell theory
title_fullStr Active control of free and forced vibration of rotating laminated composite cylindrical shells embedded with magnetostrictive layers based on classical shell theory
title_full_unstemmed Active control of free and forced vibration of rotating laminated composite cylindrical shells embedded with magnetostrictive layers based on classical shell theory
title_short Active control of free and forced vibration of rotating laminated composite cylindrical shells embedded with magnetostrictive layers based on classical shell theory
title_sort active control of free and forced vibration of rotating laminated composite cylindrical shells embedded with magnetostrictive layers based on classical shell theory
topic active vibration control
classical shell theory
modified galerkin method
magnetostrictive layers
rotating laminated composite cylindrical shell
url https://macs.semnan.ac.ir/article_4462_ebead7618fd19867d7460a29ecac3e38.pdf
work_keys_str_mv AT shahinmohammadrezazadeh activecontroloffreeandforcedvibrationofrotatinglaminatedcompositecylindricalshellsembeddedwithmagnetostrictivelayersbasedonclassicalshelltheory
AT aliasgharjafari activecontroloffreeandforcedvibrationofrotatinglaminatedcompositecylindricalshellsembeddedwithmagnetostrictivelayersbasedonclassicalshelltheory