S J Lee and J N Reddy 2004 Smart Mater. Struct. 13 1176 doi:10.1088/0964-1726/13/5/022
S J Lee1 and J N Reddy2
Show affiliationsThird-order shear deformation theories of laminated composite shells are developed using the strain–displacement relations of Donnell and Sanders theories. These theories also account for geometric nonlinearity in the von Kármán sense. Analytical (Navier) solutions for vibration suppression in cross-ply laminated composite shells with surface mounted smart material layers are developed using the linear versions of the two shell theories and for simply supported boundary conditions. Numerical results are presented to bring out the parametric effects of shell types (cylindrical, spherical, and doubly curved shells) and material properties on vibration suppression. A simple negative velocity feedback control in a closed loop is used.
46.40.-f Vibrations and mechanical waves
46.70.De Beams, plates and shells
46.35.+z Viscoelasticity, plasticity, viscoplasticity
Issue 5 (October 2004)
Received 26 November 2003, in final form 4 June 2004
Published 23 August 2004
S J Lee and J N Reddy 2004 Smart Mater. Struct. 13 1176
Meelis Sildoja et al 2008 Metrologia 45 11
Ch Rothleitner et al 2009 Metrologia 46 283
Craig Warner et al. 2003 ApJ 596 72
O Novotný et al 2009 J. Phys.: Conf. Ser. 192 012021
Lea F Santos and Lorenza Viola 2008 New J. Phys. 10 083009
Marco Valerio Battisti 2009 J. Phys.: Conf. Ser. 189 012005
, and neighbours: rotation-alignment for the half-filled
subshell?
J K Hwang et al 1998 J. Phys. G: Nucl. Part. Phys. 24 L9
Richard Seto (for the PHENIX Collaboration) 2004 J. Phys. G: Nucl. Part. Phys. 30 S1017
J Allday 1997 Phys. Educ. 32 327