Dynamic response of adaptive cross-ply cantilevers featuring interlaminar bonding imperfections

被引:31
作者
Icardi, U
Di Sciuva, M
Librescu, L
机构
[1] Politecn Torino, Dept Aerosp Engn, I-10129 Turin, Italy
[2] Virginia Polytech Inst & State Univ, Dept Engn Sci & Mech, Blacksburg, VA 24061 USA
关键词
D O I
10.2514/2.988
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The implications of slip-type interfacial bonding imperfections on the dynamic behavior of adaptive laminated beams with surface-bonded piezoactuator layers are investigated, Numerical results are supplied, and pertinent conclusions on the free and forced flexural motions under transient distributed loadings, as a function of the measure of bonding imperfections, are outlined. Near the end of this problem approach, a recently developed theory of anisotropic laminated plates that incorporates the effect of imperfect interlaminae bondings and fulfils the shear traction continuity requirements is used. The control is achieved via the action of a piezoelectrically induced bending moment at the tip of the beam, and in this context four different feedback control laws are employed. The obtained results reveal the powerful role played by the proposed control methodology toward suppressing vibrations and attenuating the detrimental effect induced by the interlaminae bonding flaws.
引用
收藏
页码:499 / 506
页数:8
相关论文
共 29 条
[1]   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
[2]   Boundary control of beams using active constrained layer damping [J].
Baz, A .
JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 1997, 119 (02) :166-172
[3]   Theory of multilayered anisotropic plates with weakened interfaces [J].
Cheng, ZQ ;
Jemah, AK ;
Williams, FW .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1996, 63 (04) :1019-1026
[4]   Effect of interfacial imperfection on buckling and bending behavior of composite laminates [J].
Cheng, ZQ ;
Kennedy, D ;
Williams, FW .
AIAA JOURNAL, 1996, 34 (12) :2590-2595
[5]   INTELLIGENT STRUCTURES FOR AEROSPACE - A TECHNOLOGY OVERVIEW AND ASSESSMENT [J].
CRAWLEY, EF .
AIAA JOURNAL, 1994, 32 (08) :1689-1699
[7]   AN IMPROVED SHEAR-DEFORMATION THEORY FOR MODERATELY THICK MULTILAYERED ANISOTROPIC SHELLS AND PLATES [J].
DISCIUVA, M .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1987, 54 (03) :589-596
[8]  
DISCIUVA M, 1992, COMPOS STRUCT, V22, P149, DOI 10.1016/0263-8223(92)90003-U
[9]  
DiSciuva M, 1997, STUD APPL MECH, V45, P395
[10]   Geometrically nonlinear theory of multilayered plates with interlayer slips [J].
DiSciuva, M .
AIAA JOURNAL, 1997, 35 (11) :1753-1759