Abstract
Analytical solutions of laminated composite shells with embedded actuating layersare presented in this study. The magnetostrictive actuating layers are used tocontrol natural vibration of laminated composite shell panels. The first-ordershear deformation shell theory (FSDT) is used to represent the shell kinematicsand equations of motion. The exact solution for symmetric laminated shells withembedded actuating layers under simply supported boundary conditions is obtainedusing the Navier solution procedure. Negative velocity feedback control is used.The parametric effects of the position of the magnetostrictive layers, materialproperties and control parameters on the vibration suppression are investigated indetail.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
