Page 300 - Semiconductor For Micro- and Nanotechnology An Introduction For Engineers
P. 300

Inhomogeneities
                             if we assume that the plate lies symmetrically about its neutral axis and
                             placed at  z =  0  . In order to preserve a simple algebraic structure later
                             on, we define the averaged plate strains by
                                                        t ---
                                                       2
                                     { ε ,  ε ,  ε } =    12 3∫  { ε ,  ε ,  ε }zz  (7.134a)
                                                                      d
                                                    ------
                                                            xx
                                       xx
                                          yy
                                                                   xy
                                              xy
                                                               yy
                                                    h   – --- t
                                                         2
                                                        t ---
                                                     2
                                                     h ∫
                                         { ε ,  ε } =   2 t  { ε ,  ε } z     (7.134b)
                                                                  d
                                                     ---
                                              yz
                                                            xz
                                                               yz
                                           xz
                                                        –
                                                         2 ---
                             We now join the above relations to obtain the plate-specific constitutive
                             relation for an isotropic material, namely
                                                      (
                                              M   =  D ε +  νε )                (7.135a)
                                               xx      xx    yy
                                                     (
                                              M  yy  =  D ε +  νε )             (7.135b)
                                                       yy
                                                             xx
                                              M    =  ( 1 –  ν)Dε               (7.135c)
                                                xy           xy
                             and
                                                 Q xz  =  µ′hR xz               (7.136a)
                                                Q yz  =  µ′hR  yz               (7.136b)
                                                                     2
                                                           3
                                                                (
                             where the plate stiffness is  D =  Eh ⁄  ( 12 1 –  ν ))   and the modified
                             shear stiffness is µ′ =  k µ  .
                                                M
                             The first z moment of the first two mechanical equations of motion, rep-
                             resented by (7.110), with the third equation of motion combine to give
                             the plate equations of motion
                                                              t
                                         ∂M  xx  ∂M  xy       --- 2
                                                                  d
                                         ------------ +  ------------ –  Q xz  =  ρ  t ∫  u˙˙ zz  (7.137a)
                                                                 x
                                          ∂x    ∂y            – ---
                                                              2
                                                              t
                                         ∂M  xy  ∂M  yy       --- 2
                                                                  d
                                         ------------ +  ------------ –  Q yz  =  ρ  t ∫  u˙˙ zz  (7.137b)
                                                                 y
                                          ∂x    ∂y            – ---
                                                              2
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