Parametric instability of thick doubly curved CNT reinforced composite sandwich panels under in-plane periodic loads using higher-order shear deformation theory-Reference-Cited by-同舟云学术

Parametric instability of thick doubly curved CNT reinforced composite sandwich panels under in-plane periodic loads using higher-order shear deformation theory

Published:2016-09-28 Issue:10 Volume:24 Page:1927-1950
ISSN:1077-5463
Container-title:Journal of Vibration and Control
language:en
Short-container-title:Journal of Vibration and Control

Author:

Sankar A¹²,El-Borgi S³⁴,Ganapathi M¹,Ramajeyathilagam K²

Affiliation:

1. Tech Mahindra Ltd., Electronic City, Bangalore, India

2. School of Aeronautical Sciences, Hindustan University, Keelambakkam, Chennai, India

3. Texas A&M University at Qatar, Mechanical Engineering Program, Engineering Building, Education City, Doha, Qatar

4. Applied Mechanics and Systems Research Laboratory, Tunisia Polytechnic School, University of Carthage, La Marsa, Tunisia

Publisher

SAGE Publications

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering,Automotive Engineering,General Materials Science

Link

http://journals.sagepub.com/doi/pdf/10.1177/1077546316672973

Reference40 articles.

1. Eshelby–Mori–Tanaka approach for vibrational behavior of continuously graded carbon nanotube-reinforced cylindrical panels

2. Buckling analysis of laminated composite rectangular plates reinforced by SWCNTs using analytical and finite element methods

3. Parametric instability of thick, orthotropic, circular cylindrical shells

4. A higher-order theory for bending analysis of laminated shells of revolution

5. Finite element method applied to the supersonic flutter of circular cylindrical shells

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