Flutter and Thermal Buckling Analysis for Composite Laminated Panel Embedded with Shape Memory Alloy Wires in Supersonic Flow
Joint Authors
Shao, Chonghui
Cao, Dengqing
Xu, Yuqian
Zhao, Hai
Source
International Journal of Aerospace Engineering
Issue
Vol. 2016, Issue 2016 (31 Dec. 2016), pp.1-12, 12 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2016-10-17
Country of Publication
Egypt
No. of Pages
12
Abstract EN
The flutter and thermal buckling behavior of laminated composite panels embedded with shape memory alloy (SMA) wires are studied in this research.
The classical plate theory and nonlinear von-Karman strain-displacement relation are employed to investigate the aeroelastic behavior of the smart laminated panel.
The thermodynamic behaviors of SMA wires are simulated based on one-dimensional Brinson SMA model.
The aerodynamic pressure on the panel is described by the nonlinear piston theory.
Nonlinear governing partial differential equations of motion are derived for the panel via the Hamilton principle.
The effects of ply angle of the composite panel, SMA layer location and orientation, SMA wires temperature, volume fraction and prestrain on the buckling, flutter boundary, and amplitude of limit cycle oscillation of the panel are analyzed in detail.
American Psychological Association (APA)
Shao, Chonghui& Cao, Dengqing& Xu, Yuqian& Zhao, Hai. 2016. Flutter and Thermal Buckling Analysis for Composite Laminated Panel Embedded with Shape Memory Alloy Wires in Supersonic Flow. International Journal of Aerospace Engineering،Vol. 2016, no. 2016, pp.1-12.
https://search.emarefa.net/detail/BIM-1105045
Modern Language Association (MLA)
Shao, Chonghui…[et al.]. Flutter and Thermal Buckling Analysis for Composite Laminated Panel Embedded with Shape Memory Alloy Wires in Supersonic Flow. International Journal of Aerospace Engineering No. 2016 (2016), pp.1-12.
https://search.emarefa.net/detail/BIM-1105045
American Medical Association (AMA)
Shao, Chonghui& Cao, Dengqing& Xu, Yuqian& Zhao, Hai. Flutter and Thermal Buckling Analysis for Composite Laminated Panel Embedded with Shape Memory Alloy Wires in Supersonic Flow. International Journal of Aerospace Engineering. 2016. Vol. 2016, no. 2016, pp.1-12.
https://search.emarefa.net/detail/BIM-1105045
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1105045