Aero-hygro-thermal stability analysis of higher-order refined supersonic FGM panels with even and uneven porosity distributions

被引:59
作者
Barati, Mohammad Reza
Shahverdi, Hossein [1 ]
机构
[1] Amirkabir Univ Technol, Aerosp Engn Dept, Tehran 158754413, Iran
关键词
Hygro-thermal instability; Aerodynamic pressure; Functionally graded materials; Porosities; Piston theory; FUNCTIONALLY GRADED PLATES; SHEAR DEFORMATION-THEORY; VIBRATION ANALYSIS; SANDWICH PLATES; BEAMS; FLOW; LOADS;
D O I
10.1016/j.jfluidstructs.2017.06.007
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In this paper, porosity-dependent aero-hygro-thermal instability of functionally graded (FG) panels is investigated by developing a higher-order refined shear deformable theory for the first time. Porosities are randomly distributed around the cross section of FG panel. Hygro-thermo-elastic material properties of porous FG panel are described using a modified power-law function accounting for even and uneven porosity distributions. Based on the presented refined shear deformation theory, it is possible to examine instability regions of thicker FG panels without using a shear correction factor. Employing extended Hamilton's principle, the governing equations of FG panel under supersonic airflow simulated via first-order piston theory are obtained. It is concluded that porosity volume fraction, type of porosities, hygro-thermal environment, material gradation and slenderness ratio have major roles on the prediction of divergence and flutter boundaries of porous FG panels. (C) 2017 Elsevier Ltd. All rights reserved.
引用
收藏
页码:125 / 136
页数:12
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