Buckling and Free Vibration Behavior of a Temperature Dependent FG-CNTRC Cylindrical Panel Under Thermal Load. (2018)

• Record Type: Journal Article
• Authors: Bhagat, Vinod; Jeyaraj, P.; Murigendrappa, S.M.
• Is Part Of: Materials today. Volume 5:Number 11(2018)Part 3
• Page Start: 23682
• Page End: 23691
• Publication Date: 2018
• Subjects: Cylindrical panel -- Carbon-nanotubes -- Finite element method -- Thermal buckling -- Free vibration; Materials science -- Congresses -- Periodicals; 620.1
• DOI: 10.1016/j.matpr.2018.10.158
• Languages: English
• ISSNs: 2214-7853

Abstract

Abstract: Present study deals with the buckling and free vibration behavior of functionally graded carbon-nanotubes reinforced composite (FG-CNTRC) cylindrical panel exposed to uniform thermal load. Stresses setup due to thermal load and temperature dependent properties influences the buckling and free vibration behavior of the heated structures. Approach employed in the present study consists of static analysis to compute thermal stresses, eigen-value buckling analysis to compute critical buckling temperature and finally modal analysis, taking thermal stresses into account. Influence of different CNTs grading pattern, CNTs volume fraction, geometric parameters, boundary constraints and temperature dependent properties on the buckling strength are investigated. It is observed that hybrid CNTs distribution pattern gives comparatively higher buckling strength and free vibration frequencies. Investigation on free vibration characteristics of the FG-CNTRC panel at elevated temperature signifies that the decline in free vibration frequencies is very drastic at a temperature close to buckling temperature along with temperature dependent properties. c 2017 Elsevier Ltd. All rights reserved