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

                              74   Chapter Two
                                                        C (x) — xC (x)
                                                         l
                                                                 c
                                                 f (x) =     C l                         (2.94)
                                                 b
                              where the newly introduced compliances in the numerator are calcu-
                              lated as
                                                   l  2                  l
                                              12    x dx            12    xdx
                                       C (x) =              C (x) =                      (2.95)
                                                              c
                                        l
                                              Et 3ฒ w(x)            Et 3ฒ w(x)
                                                  x
                                                                        x
                              It can easily be demonstrated that for a constant rectangular cross-sec-
                              tion microcantilever, the bending-related distribution function defined
                              in Eqs. (2.94) and (2.95) reduces to Eq. (2.63).
                                In the case of short microcantilevers, where shearing effects and the
                              corresponding  deformations  have to be accounted for, the bending-
                              related distribution function is calculated as
                                                         sh
                                                        C (x) — xC (x)
                                                         l
                                                                  c
                                                f b sh (x) =                             (2.96)
                                                             C sh
                                                              l
                                                sh             E
                              where            C (x) = C (x) + ț  G  C (x)               (2.97)
                                                l
                                                        l
                                                                  a
                              For a constant cross-section microcantilever, Eqs. (2.96) and (2.97) re-
                              sult in Eq. (2.77), which gives the bending-related distribution function
                              in a separate (and independent) derivation.
                                Several variable-cross-section microcantilever configurations such as
                              trapezoid or corner-filleted are analyzed next by providing lumped-
                              parameter stiffness and inertia fractions together with the resonant
                              frequencies corresponding to axial, torsional, and bending vibrations.


                              Trapezoid microcantilevers. A  trapezoid configuration is shown in
                              Fig. 2.25 together with the defining geometry. It is assumed that the
                              microcantilever is fixed at its root and free at the opposite end, and that
                              its constant thickness t is small (thin configuration). The variable width
                              w, which is measured at a distance x from the free end, can be expressed
                              as

                                                           (w — w )x
                                                              2
                                                                  1
                                                w(x) = w +                               (2.98)
                                                        1       l
                                As previously mentioned, the  bending stiffness corresponding to
                              point 1 in Fig. 2.25 and to deformation (rotation) about the y axis is
                              calculated with the aid of the generic Eq. (2.84) and the width definition
                              of Eq. (2.98). Thus, the bending stiffness is




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