Dynamic Stability Behavior of 3D Braided Composite Plates Integrated with Piezoelectric Layers

被引:13
作者
Yang, Jie [1 ]
Huang, Xiaolin [2 ]
机构
[1] RMIT Univ, Sch Aerosp Mech & Mfg Engn, Bundoora, Vic 3083, Australia
[2] City Univ Hong Kong, Dept Bldg & Construct, Kowloon, Hong Kong, Peoples R China
关键词
dynamic stability; piezoelectric materials; braided composites; laminated plate; DEFORMABLE LAMINATED PLATES; PERIODIC INPLANE LOAD; HIGHER-ORDER THEORY; ELASTIC FOUNDATIONS; PARAMETRIC RESONANCE; ELEMENT METHOD; INSTABILITY; VIBRATION; ACTUATORS; MODEL;
D O I
10.1177/0021998309339219
中图分类号
TB33 [复合材料];
学科分类号
摘要
This article presents a dynamic stability analysis of a simply supported 3D braided composite laminated plate with surface-bonded piezoelectric layers, subjected to electrical and periodic in-plane mechanical loads. The braided composite plate is produced by the four-step 1 x 1 technique. It is assumed that the yarn is transversely isotropic, and the matrix is isotropic. A fiber inclination model is used to predict the effective stiffness matrices of the braided composite laminates. Theoretical formulations are based on Reddy's higher order shear deformation plate theory and include piezoelectric effects. Double Fourier series is employed to convert the dynamic governing equations into a linear system of Mathieu-Hill equations from which the boundary points on the unstable regions are determined by Bolotin's method. Numerical illustrations show the influence of fiber volume fraction, braiding angle, inclination angle, static load level, applied voltage, and aspect ratio on the dynamic stability, buckling and free vibration of the braided composite plate.
引用
收藏
页码:2223 / 2238
页数:16
相关论文
共 29 条
[11]   Non-linear dynamic stability characteristics of elastic plates subjected to periodic in-plane load [J].
Ganapathi, M ;
Patel, BP ;
Boisse, P ;
Touratier, M .
INTERNATIONAL JOURNAL OF NON-LINEAR MECHANICS, 2000, 35 (03) :467-480
[12]   Nonlinear free and forced vibration of simply supported shear deformable laminated plates with piezoelectric actuators [J].
Huang, XL ;
Shen, HS .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2005, 47 (02) :187-208
[13]   Nonlinear vibration and dynamic response of simply supported shear deformable laminated plates on elastic foundations [J].
Huang, XL ;
Zheng, JJ .
ENGINEERING STRUCTURES, 2003, 25 (08) :1107-1119
[14]   A failure model for the analysis of thin woven glass composite structures under impact loadings [J].
Iannucci, L ;
Dechaene, R ;
Willows, M ;
Degrieck, J .
COMPUTERS & STRUCTURES, 2001, 79 (08) :785-799
[15]   Effect of piezoelectric damping layers on the dynamic stability of plate under a thrust [J].
Kim, HW ;
Kim, JH .
JOURNAL OF SOUND AND VIBRATION, 2005, 284 (3-5) :597-612
[16]   Effects of fibre surface treatment on dynamic tensile properties of glass woven fabric reinforced vinylester composites [J].
Kim, JK ;
Sham, ML ;
Sohn, MS ;
Hu, SS .
POLYMERS & POLYMER COMPOSITES, 2005, 13 (05) :453-466
[17]   FINITE-ELEMENT ANALYSIS OF DYNAMIC INSTABILITY OF LAYERED COMPOSITE PLATES USING A HIGH-ORDER BENDING THEORY [J].
KWON, YW .
COMPUTERS & STRUCTURES, 1991, 38 (01) :57-62
[18]   Dynamic instability of layered anisotropic composite plates on elastic foundations [J].
Patel, BP ;
Ganapathi, M ;
Prasad, KR ;
Balamurugan, V .
ENGINEERING STRUCTURES, 1999, 21 (11) :988-995
[19]   Dynamic stability analysis of composite plates including delaminations using a higher order theory and transformation matrix approach [J].
Radu, AG ;
Chattopadhyay, A .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2002, 39 (07) :1949-1965
[20]  
Reddy J.N., 1984, INT J SOLIDS STRUCT, V20, P818