Page 103 - Mechanical design of microresonators _ modeling and applications
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0-07-145538-8_CH02_102_08/30/05



                                    Basic Members: Lumped- and Distributed-Parameter Modeling and Design

                              102   Chapter Two
                              (outlined previously in this distributed-parameter section) and can be
                              expressed as

                                                  2
                                                 Ȧ =  2     U max
                                                           2
                                                      ȡt  ฒ w (x, y) dA                 (2.211)
                                                        A  0
                              where U max  is the maximum potential energy and is formulated as

                                                              2
                                                     2
                                               ( ) ( ) ( )( )
                                                                    2
                                                 2
                                                         2
                                                                          2
                                                                         ˜ w
                                                                   ˜ w
                                                         ˜ w
                                                ˜ w
                                                   0
                                                                      0
                                                            0
                                                                            0
                                                      +
                                                               +2ȝ
                                          D      ˜x 2    ˜y 2       ˜x 2  ˜y 2
                                   U max  =  2ฒ           2   2                 dA      (2.212)
                                                         ˜ w
                                                            0
                                            A   +2(1 íȝ) ( ˜x ˜ y)
                              The flexural rigidity D is defined as
                                                           Et 3
                                                    D =                                 (2.213)
                                                               2
                                                        12(1 íȝ )
                                For a rectangular thin plate which is fixed (clamped on the contour),
                              as sketched in Fig. 2.39, a suitable w 0  function needs to be used, that
                              would satisfy the boundary conditions, namely, zero  deflections and
                              zero slopes (partial derivatives of deflection in terms of x or y) on the
                              contour.
                                Such a function could be the following one:
                                  y




                              l2





                                                              x
                                            l1
                              Figure 2.39 Top view of rectangular plate with dimensions and reference frame.





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