3-DIMENSIONAL SOLUTIONS FOR COUPLED THERMOELECTROELASTIC RESPONSE OF MULTILAYERED PLATES

被引:138
作者
XU, KM
NOOR, AK
TANG, YY
机构
[1] UNIV VIRGINIA,CTR COMPUTAT STRUCT TECHNOL,NASA,LANGLEY RES CTR,HAMPTON,VA 23681
[2] NATL RES COUNCIL,STRUCT ACOUST BRANCH,NASA,LANGLEY RES CTR,HAMPTON,VA 23681
基金
美国国家航空航天局;
关键词
D O I
10.1016/0045-7825(95)00825-L
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Analytic three-dimensional solutions are presented for the coupled thermoelectroelastic response of multilayered hybrid composite plates. The plates consist of a combination of fiber-reinforced cross-ply and piezothermoelastic layers. Both the thermoelectroelastic static response and its sensitivity coefficients are computed. The sensitivity coefficients measure the sensitivity of the response to variations in different mechanical, thermal and piezoelectric material properties of the plate. A linear constitutive model is used, and the material properties are assumed to be independent of the temperature and the electric field. The plates are assumed to have rectangular geometry and special material symmetries. A mixed formulation is used with the fundamental unknowns consisting of the three transverse stress components, three displacement components, transverse component of the electric displacement field, electric potential, transverse heat flux component and temperature change. Each of the fundamental unknowns is expressed in terms of a double Fourier series in the Cartesian surface coordinates. A state space approach is used to generate the static response and to evaluate the sensitivity coefficients. Extensive numerical results are presented showing the effects of variation in the geometric parameters of the plate on the different response quantities and their sensitivity coefficients.
引用
收藏
页码:355 / 371
页数:17
相关论文
共 23 条
[1]  
ALIKE H, 1984, J ACOUST SOC AM, V56, P1782
[2]   DISTRIBUTED PIEZOELECTRIC POLYMER ACTIVE VIBRATION CONTROL OF A CANTILEVER BEAM [J].
BAILEY, T ;
HUBBARD, JE .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1985, 8 (05) :605-611
[3]   USE OF PIEZOELECTRIC ACTUATORS AS ELEMENTS OF INTELLIGENT STRUCTURES [J].
CRAWLEY, EF ;
DELUIS, J .
AIAA JOURNAL, 1987, 25 (10) :1373-1385
[4]  
CULLEN CJ, 1979, LINEAR ALGEBRA DIFFE
[5]  
DIMITRIADIS EK, 1991, J VIB ACOUST ASME, V117, P100
[6]  
ERINGEN AC, 1989, ELECTRODYNAMICS CONT
[7]   AN EXACT SOLUTION FOR THE STATICS AND DYNAMICS OF LAMINATED THICK PLATES WITH ORTHOTROPIC LAYERS [J].
FAN, JR ;
YE, JQ .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1990, 26 (5-6) :655-662
[8]   EFFECTS OF A PIEZO-ACTUATOR ON A FINITELY DEFORMED BEAM SUBJECTED TO GENERAL LOADING [J].
IM, SY ;
ATLURI, SN .
AIAA JOURNAL, 1989, 27 (12) :1801-1807
[9]  
JONNALAGADDA KD, IN PRESS COMPUT STRU
[10]   LAMINATED PIEZOPOLYMER PLATES FOR TORSION AND BENDING SENSORS AND ACTUATORS [J].
LEE, CK ;
MOON, FC .
JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1989, 85 (06) :2432-2439