Stiffening effects on the free vibration behavior of composite plates with PZT actuators

Composite Structures

Volumn 49, Issue 1, 2000, Pages 55-63

  Hernandes, José Antônio ^a   Almeida, S F M ^a   Nabarrete, A ^a  

^a INSTITUTO TECNOLÓGICO DE AERONÁUTICA   (Brazil)

Author keywords

Piezoelectric; Plate finite element; Stress stiffening

Indexed keywords

ACTUATORS; EIGENVALUES AND EIGENFUNCTIONS; FINITE ELEMENT METHOD; PIEZOELECTRIC MATERIALS; PLATES (STRUCTURAL COMPONENTS); STIFFNESS; STIFFNESS MATRIX; STRESS ANALYSIS; STRUCTURAL ANALYSIS; VIBRATIONS (MECHANICAL);

FREE VIBRATIONS; REISSNER-MINDLIN THEORY; STRESS RESULTANTS;

COMPOSITE STRUCTURES;

EID: 0033888430     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(99)00125-7     Document Type: Article

References (14)

1. Crawley E.F., Anderson E.H. Detailed models of piezoceramic actuation of beams. J Intell Mater Syst Struct. 1(1):1990;4-25.
2. Crawley E.F., de Luis J. Use of the piezoelectric actuators as elements of intelligent structures. AIAA J. 25(10):1987;1373-1385.
3. Ha S.K., Keilers C., Chang F.K. Finite element analysis of composite structures containing distributed piezoceramic sensors and actuators. AIAA J. 30(3):1992;772-780.
4. Batra R.C., Liang X.Q., Yang J.S. Shape control of vibrating simply supported rectangular plates. AIAA J. 34(1):1996;116-122.
5. Ghosh K., Batra R.C. Shape control of plates using piezoceramic elements. AIAA J. 33(7):1995;1354-1357.
6. Sonti V.R., Jones J. Dynamic effects of piezoactuators on the cylindrical shell response. AIAA J. 34(4):1996;795-801.
7. Tzou H.S., Ye R. Analysis of piezoelastic structures with laminated piezoelectric triangle shell elements. AIAA J. 34(1):1996;110-115.
8. Chandra R., Chopra I. Structural modeling of composite beams with induced-strain actuators. AIAA J. 31(9):1993;1692-1701.
9. Brunelle E.J., Robertson S.R. Initially stressed mindlin plates. AIAA J. 12(8):1974;1036-1045.
10. Yang I.H., Shieh J.A. Vibrations of initially stressed thick rectangular orthotropic plates. J Sound and Vibration. 119(3):1987;545-558.
11. Rammerstorfer F.G. Increase of the first natural frequency and buckling load of plates by optimal fields of initial stresses. Acta Mech. 27(1-4):1977;217-238.
12. Almeida S.F.M., Hansen J.S. Enhanced elastic buckling loads of composite plates with tailored thermal residual stresses. J Appl Mech. 64(4):1997;772-780.
13. Dawe DJ, Roufaeil OL. Buckling of rectangular mindlin plates. Comput Struct 15(4):461-71.
14. Heppler G.R., Hansen J.S. A mindlin element for thick and deep shells. Comput Meth Appl Mech Eng. 54(1):1986;21-47.