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238                                                         Chapter 4
         and the  underlying  mechanism  can be  utilized in  micro-scale sensing  for
         instance.

         Example 4.13
             A circular,  circumferentially-clamped  SMA  membrane in  martensitic
         state is  deformed  through an external  pressure such  that a  maximum  central
         deflection   is  reached. A  temperature  increase  of   is  applied to the
         membrane and the  martensite transforms  completely in  austenite.  Find the
         maximum force  that can be generated through  this  reversed  transformation.
         Consider that the membrane is defined by a radius       and thickness
                 The elastic properties of the austenite and martensite  are:
                                                              (after  Otsuka and
         Wayman [10]). Also consider that

          Solution:
             The maximum force  that can be  generated  during the  membrane’s
          martensitic-austenitic  transformation equals the force  that is  needed to
          prevent any resulting  deformation,  and the  stiffness of a  clamped  circular
          plate that is  acted  upon by a  force placed  at the  symmetry  center
          perpendicularly to the membrane plane is given in Eq. (1.231), Chapter 1. As
          a consequence, the maximum (bloc) force becomes:





          The flexural rigidities in austenitic and martensitic phase are:








          By using the numerical values of this problem, the maximum force is found
          to be of 0.206 mN.

          8      BIMORPH TRANSDUCTION

          8.1    Generic Formulation


              Bimorphs are  composed of two  layers  of different materials  laid upon
          each other as sketched in Fig. 4.51  (a). In general, one layer is active,  in the
          sense that it can deform axially upon application of a specific type of energy.
          Because the two  layers are sandwiched together, the  free  axial  deformation
          of  the top  layer is constrained  by  the  bottom layer  and, as  a result,  the
          composite beam  will  bend.  When the  top  layer  shrinks, the resulting
          deformed shape of the beam is the one shown in Fig. 4.51  (b). When the free
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