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

                                 Basic Members: Lumped- and Distributed-Parameter Modeling and Design  49

                                                     M y


                                                            eccentric
                                   fixed shaft

                                                             u z

                                               k c,y



                              Figure 2.6 Lumped-parameter cross-bending stiffness for a microcantilever.

                              theorem, which expresses the load L i  that is applied at a point on an
                              elastic body as the partial derivative of the strain energy U evaluated
                              with respect to the corresponding elastic deformation d i  about the load
                              direction at the point of interest, or
                                                           ˜U
                                                       L =                                (2.3)
                                                        i
                                                           ˜d
                                                             i
                              This approach is implemented with ease when the cross section is con-
                              stant, but is more difficult to utilize for variable-cross-section members.
                                The strain energy corresponding to axial loading can be expressed as
                                                    2
                                                 l  F (x)     l    du (x) 2
                                             1
                                                                      x
                                                   a
                                                          2ฒ
                                       U =  2Eฒ    A(x)  =  E  A(x)  dx     dx            (2.4)
                                         a
                                                0            0
                              where F a (x) is  the axial load,  A(x) is the  cross-sectional area,  u x (x)
                              is the axial deformation,  and  E is Young’s  modulus of  elasticity.
                              The differential equation expressing the  static equilibrium in axial
                              loading is
                                                    2
                                                   d u (x)A(x)
                                                       x
                                                                =0                        (2.5)
                                                       dx 2
                              The axial deformation at a generic point on the micromember can be
                              expressed as a function of the axial deformation at the free end and a
                              distribution function f (x) as
                                                  a
                                                    u (x) = f (x)u                        (2.6)
                                                     x      a    x






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