Fig. 6.7
Outward and inward displacements of the spherical shell . . . . . . 107
Fig. 6.8
Cylindrical panel with layered orthotropic materials . . . . . . . . . . 108
Fig. 6.9
Static response of cross-ply laminated panel with thickness
of 12.6 mm and stacking sequence ½0
=90
=0
. . . . . . . . . . . . . 108
Fig. 6.10 Static response of cross-ply laminated panel with thickness
of 12.6 mm and stacking sequence ½90
=0
=90
. . . . . . . . . . . . 109
Fig. 6.11 Static response of cross-ply laminated panel with thickness
of 6.3 mm and stacking sequence ½0
=90
=0
. . . . . . . . . . . . . . 109
Fig. 6.12 Static response of cross-ply laminated panel with thickness
of 6.3 mm and stacking sequence ½90
=0
=90
. . . . . . . . . . . . . 110
Fig. 6.13 Static response of angle-ply laminated panel with thickness
of 12.6 mm and stacking sequences ½45
= À 45
and
½À45
=45
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 110
Fig. 6.14 Static response of angle-ply laminated panel with thickness
of 6.3 mm and stacking sequences ½45
= À 45
and
½À45
=45
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 111
Fig. 6.15 Cantilevered beam with one piezoelectric patch bonded . . . . . . . 111
Fig. 6.16 Static response of the cantilevered smart beam: a tip
displacement, b sensor output voltage, reprinted from Ref. [5],
copyright 2014, with permission from ELSEVIER . . . . . . . . . . . 112
Fig. 6.17 Maximum rotations at centerline nodes of cantilevered smart
beam: a rotation u 1 , b rotation u 2 , reprinted from Ref. [5],
copyright 2014, with permission from ELSEVIER . . . . . . . . . . . 113
Fig. 6.18 Dynamic response of cantilevered beam using various shell
theories: a tip displacement, b sensor output voltage, reprinted
from Ref. [19], copyright 2013, with permission from IOP . . . . 114
Fig. 6.19 Dynamic response of cantilevered beam using various meshes
and integration schemes: a tip displacement, b sensor output
voltage, reprinted from Ref. [19], copyright 2013, with
permission from IOP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 115
Fig. 6.20 Fully clamped plate with one piezoelectric patch centrally
bonded . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 116
Fig. 6.21 Static response of the fully clamped plate: a mid-point
displacement, b sensor output voltage, reprinted from Ref. [5],
copyright 2014, with permission from ELSEVIER . . . . . . . . . . . 118
Fig. 6.22 Rotations of the plate under a pressure of 2 Â 10
7 Pa: a
rotation u 1 , b rotation u 2 , reprinted from Ref. [5], copyright
2014, with permission from ELSEVIER . . . . . . . . . . . . . . . . . . . 119
Fig. 6.23 Dynamic response of the fully clamped plate under a step
pressure of 2 Â 10
4 Pa: a mid-point displacement, b sensor
xviii
List of Figures
Outward and inward displacements of the spherical shell . . . . . . 107
Fig. 6.8
Cylindrical panel with layered orthotropic materials . . . . . . . . . . 108
Fig. 6.9
Static response of cross-ply laminated panel with thickness
of 12.6 mm and stacking sequence ½0
=90
=0
. . . . . . . . . . . . . 108
Fig. 6.10 Static response of cross-ply laminated panel with thickness
of 12.6 mm and stacking sequence ½90
=0
=90
. . . . . . . . . . . . 109
Fig. 6.11 Static response of cross-ply laminated panel with thickness
of 6.3 mm and stacking sequence ½0
=90
=0
. . . . . . . . . . . . . . 109
Fig. 6.12 Static response of cross-ply laminated panel with thickness
of 6.3 mm and stacking sequence ½90
=0
=90
. . . . . . . . . . . . . 110
Fig. 6.13 Static response of angle-ply laminated panel with thickness
of 12.6 mm and stacking sequences ½45
= À 45
and
½À45
=45
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 110
Fig. 6.14 Static response of angle-ply laminated panel with thickness
of 6.3 mm and stacking sequences ½45
= À 45
and
½À45
=45
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 111
Fig. 6.15 Cantilevered beam with one piezoelectric patch bonded . . . . . . . 111
Fig. 6.16 Static response of the cantilevered smart beam: a tip
displacement, b sensor output voltage, reprinted from Ref. [5],
copyright 2014, with permission from ELSEVIER . . . . . . . . . . . 112
Fig. 6.17 Maximum rotations at centerline nodes of cantilevered smart
beam: a rotation u 1 , b rotation u 2 , reprinted from Ref. [5],
copyright 2014, with permission from ELSEVIER . . . . . . . . . . . 113
Fig. 6.18 Dynamic response of cantilevered beam using various shell
theories: a tip displacement, b sensor output voltage, reprinted
from Ref. [19], copyright 2013, with permission from IOP . . . . 114
Fig. 6.19 Dynamic response of cantilevered beam using various meshes
and integration schemes: a tip displacement, b sensor output
voltage, reprinted from Ref. [19], copyright 2013, with
permission from IOP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 115
Fig. 6.20 Fully clamped plate with one piezoelectric patch centrally
bonded . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 116
Fig. 6.21 Static response of the fully clamped plate: a mid-point
displacement, b sensor output voltage, reprinted from Ref. [5],
copyright 2014, with permission from ELSEVIER . . . . . . . . . . . 118
Fig. 6.22 Rotations of the plate under a pressure of 2 Â 10
7 Pa: a
rotation u 1 , b rotation u 2 , reprinted from Ref. [5], copyright
2014, with permission from ELSEVIER . . . . . . . . . . . . . . . . . . . 119
Fig. 6.23 Dynamic response of the fully clamped plate under a step
pressure of 2 Â 10
4 Pa: a mid-point displacement, b sensor
xviii
List of Figures