Stiffening effects on the free vibration behavior of composite plates with PZT actuators
Tài liệu tham khảo
Crawley, 1990, Detailed models of piezoceramic actuation of beams, J Intell Mater Syst Struct, 1, 4, 10.1177/1045389X9000100102
Crawley, 1987, Use of the piezoelectric actuators as elements of intelligent structures, AIAA J, 25, 1373, 10.2514/3.9792
Ha, 1992, Finite element analysis of composite structures containing distributed piezoceramic sensors and actuators, AIAA J, 30, 772, 10.2514/3.10984
Batra, 1996, Shape control of vibrating simply supported rectangular plates, AIAA J, 34, 116, 10.2514/3.13030
Ghosh, 1995, Shape control of plates using piezoceramic elements, AIAA J, 33, 1354, 10.2514/3.12427
Sonti, 1996, Dynamic effects of piezoactuators on the cylindrical shell response, AIAA J, 34, 795, 10.2514/3.13142
Tzou, 1996, Analysis of piezoelastic structures with laminated piezoelectric triangle shell elements, AIAA J, 34, 110, 10.2514/3.12907
Chandra, 1993, Structural modeling of composite beams with induced-strain actuators, AIAA J, 31, 1692, 10.2514/3.11832
Brunelle, 1974, Initially stressed mindlin plates, AIAA J, 12, 1036, 10.2514/3.49407
Yang, 1987, Vibrations of initially stressed thick rectangular orthotropic plates, J Sound and Vibration, 119, 545, 10.1016/0022-460X(87)90413-5
Rammerstorfer, 1977, Increase of the first natural frequency and buckling load of plates by optimal fields of initial stresses, Acta Mech, 27, 217, 10.1007/BF01180087
Almeida, 1997, Enhanced elastic buckling loads of composite plates with tailored thermal residual stresses, J Appl Mech, 64, 772, 10.1115/1.2788981
Dawe DJ, Roufaeil OL. Buckling of rectangular mindlin plates. Comput Struct 15(4):461–71
Heppler, 1986, A mindlin element for thick and deep shells, Comput Meth Appl Mech Eng, 54, 21, 10.1016/0045-7825(86)90033-2