Non-linear vibration analysis of smart composite structures with discrete delamination using a refined layerwise theory

被引:59
作者
Chattopadhyay, A [1 ]
Kim, HS [1 ]
Ghoshal, A [1 ]
机构
[1] Arizona State Univ, Dept Mech & Aerosp Engn, Tempe, AZ 85287 USA
关键词
D O I
10.1016/S0022-460X(03)00561-3
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
A non-linear vibration analysis procedure has been developed to investigate the dynamic response of composite laminates with embedded and/or surface bonded piezoelectric sensors and multiple finite/discrete delaminations. The objective is to accurately predict the sensor output in the time domain. A recently developed refined layerwise composite theory is used to develop the piezoelectric-mechanical model. A two-way coupled electro-mechanical formulation is used to derive the equations of motion. An adaptive nonlinear transient implicit algorithm is used to generate the voltage time history, which is useful in characterizing the presence of delamination. The contact problem of delaminated interfacial surfaces is modelled in terms of fictitious linear springs to provide an accurate description of the transient behavior. The accuracy of the model is validated through comparison with experimental results. The validity of low frequency vibration analysis in detection of delamination(s) from in-situ sensor outputs is also established. It is anticipated that the developed framework will be a useful tool in structural health monitoring studies. (C) 2003 Elsevier Ltd. All rights reserved.
引用
收藏
页码:387 / 407
页数:21
相关论文
共 24 条
[1]  
ARGYRIS J, 1991, DYNAMICS STURCTURES
[2]  
Bathe K, 2007, Finite element procedures
[3]   THE EFFECT OF DELAMINATIONS IN GRAPHITE PEEK COMPOSITE PLATES ON MODAL DYNAMIC CHARACTERISTICS [J].
CAMPANELLI, RW ;
ENGBLOM, JJ .
COMPOSITE STRUCTURES, 1995, 31 (03) :195-202
[4]   Dynamics of delaminated smart composite cross-ply beams [J].
Chattopadhyay, A ;
Dragomir-Daescu, D ;
Gu, HZ .
SMART MATERIALS & STRUCTURES, 1999, 8 (01) :92-99
[5]   Dynamics of delaminated composite plates with piezoelectric actuators [J].
Chattopadhyay, A ;
Gu, HZ ;
Dragomir-Daescu, D .
AIAA JOURNAL, 1999, 37 (02) :248-254
[6]   NEW HIGHER-ORDER PLATE-THEORY IN MODELING DELAMINATION BUCKLING OF COMPOSITE LAMINATES [J].
CHATTOPADHYAY, A ;
GU, HZ .
AIAA JOURNAL, 1994, 32 (08) :1709-1716
[7]  
CHATTOPADHYAY A, 2002, IUTAM S DYNAMICS ADV
[8]   Higher-order zig-zag theory for laminated composites with multiple delaminations [J].
Cho, M ;
Kim, JS .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 2001, 68 (06) :869-877
[9]   Delamination suckling and postbuckling of composite cylindrical shells [J].
Gu, HZ ;
Chattopadhyay, A .
AIAA JOURNAL, 1996, 34 (06) :1279-1286
[10]   BUCKLING AND POSTBUCKLING OF DELAMINATED COMPOSITES UNDER COMPRESSIVE LOADS INCLUDING TRANSVERSE-SHEAR EFFECTS [J].
KARDOMATEAS, GA ;
SCHMUESER, DW .
AIAA JOURNAL, 1988, 26 (03) :337-343