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5. Static response of MEMS                                       315
         (5.144) and (5.145), the maximum stress according to the large displacement
         model is:





         As a consequence, the following stress ratio can be formulated, based on Eqs.
         (5.142) and (5.146):





         The stress ratio of Eq. (5.147) is plotted against the force F in Fig.  5.48. It
         can be  seen  that by using  the  small-displacement  theory,  the  stresses are
         always overevaluated,  as  compared  to the  large-displacement  theory, up  to
         factors of approximately 2.5  for  large values of F.  However, at  relatively
         smaller loads, the predictions given by the two methods are almost identical,
          as also shown in Fig. 5.48, where the stress ratio is very close to  1  for small
         values of the force F.




















                   Figure 5.48  Stress ratio as a function of the tip force – Eq. (5.147)



          7.     BUCKLING

          7.1    Introduction

              Buckling is  associated  with  structural  instability  occurring at
          statical/dynamical loads which  are called critical and which  can  produce
          either  failure or  large  deformations that are unacceptable.  The discussion
          here will be restricted to  statically-generated buckling. Figure  5.49 pictures
          three different situations that are stability-related.
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