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Shock and Vibration
Volume 2018, Article ID 6980536, 16 pages
https://doi.org/10.1155/2018/6980536
Research Article

New Frequency-Dependent Trigonometric Interpolation Functions for the Dynamic Finite Element Analysis of Thin Rectangular Plates

Department of Aerospace Engineering, Ryerson University, Toronto, ON, Canada

Correspondence should be addressed to Supun Jayasinghe; ac.nosreyr@nisayajh

Received 1 October 2017; Revised 8 November 2017; Accepted 13 November 2017; Published 15 January 2018

Academic Editor: Nerio Tullini

Copyright © 2018 Supun Jayasinghe and Seyed M. Hashemi. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

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