Nonlinear aeroelastic stability analysis of three-phase nano-composite plates

被引：24
|
作者：
Yazdi, Ali A. [1 ]
机构：
[1] Quchan Univ Technol, Dept Mech Engn, Quchan, Iran
来源：
MECHANICS BASED DESIGN OF STRUCTURES AND MACHINES | 2019年 / 47卷 / 06期
关键词：
Carbon nano-tubes; flutter; homotopy perturbation method; large deflection; three-phase nano-composite; VIBRATION ANALYSIS; BUCKLING ANALYSIS; BEAMS; NANOCOMPOSITES; FLUTTER;
D O I：
10.1080/15397734.2019.1610436
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The main aim of this study is to investigate the geometrical nonlinear flutter of three-phase nano-composite plates reinforced with carbon nano-tubes (CNTs). The effective material properties are obtained using Halpin-Tsai relation and rule of mixture. The classical plate theory and von Karman geometrical nonlinearities assumptions are employed to obtain the governing equation of the system. The homotopy perturbation method (HPM) is utilized to conduct a numerical investigation to study the aeroelastic behavior of multiscale composite plates. The effects of different parameters such as CNTs weight percentage, aspect ratio, and elastic modulus ratio on flutter pressure of nano-composite plates are considered. Communicated by S. Velinsky.
引用
收藏
页码：753 / 768
页数：16
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