Ganesh, Shankar and Kumar, Keshava S and Mahato, PK (2016) Free Vibration Analysis of Delaminated Composite Plates using Finite Element Method. In: 12th International Conference on Vibration Problems (ICOVP), DEC 14-17, 2015, Guwahati, INDIA, pp. 1067-1075.
Int_Con_Vib_Pro_144_1067_2016.pdf - Published Version
Restricted to Registered users only
Download (231Kb) | Request a copy
In the present paper equivalent single layer (ESL) theory has employed with finite element method to describe the free vibration analysis of delaminated composite plates. Based on the first order shear deformation theory (FSDT) and finite element formulation, the work is fully concentrated on the free vibration analysis of delaminated composite plates. Two types of boundary conditions which are simply supported (S-S-S-S) and cantilever type (C-F-F-F) have taken for the analysis. The present work has also calculated the deformation at different places in composite plate; this is fully analytical and computational approach. Result is validated with the various references presented on the literature survey (C) 2016 The Authors. Published by Elsevier Ltd.
|Item Type:||Conference Proceedings|
|Additional Information:||Copy right for this article belongs to the ELSEVIER SCIENCE BV, SARA BURGERHARTSTRAAT 25, PO BOX 211, 1000 AE AMSTERDAM, NETHERLANDS|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||07 Dec 2016 06:06|
|Last Modified:||07 Dec 2016 06:06|
Actions (login required)