Page 299 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 299

286                             Vibration of Continuous Systems   Chap. 9

                                  From Table  9.5-1,  the  first natural  frequency becomes
                                                        [   15.03  X  10^
                                                a>, =3.52, /   ---------------  =  28.12 rad/s
                                                         ^ ( 2 0 X 1 2 /
                                                                       =  4.48 c.p.s.


                       9.6  EFFECT OF ROTARY INERTIA
                           AND SHEAR DEFORMATION

                              The Timoshenko theory accounts for both the rotary inertia and shear deformation
                              of the  beam.  The  free-body  diagram  and  the  geometry for  the  beam  element  are
                              shown  in  Fig.  9.6-1.  If the  shear deformation  is  zero,  the  center  line of the  beam
                              element will coincide with the perpendicular to the face of the cross section.  Due
                              to  shear,  the  rectangular  element  tends  to  go  into  a  diamond  shape  without
                              rotation  of  the  face,  and  the  slope  of  the  center  line  is  diminished  by  the  shear
                              angle (if/  -  dy/dx). The following quantities can then be defined:
                                               y  =  deflection of the center line of the beam
                                              dy
                                                 =  slope of the center line of the beam
                                               il/  =  slope due to bending
                                              dy
                                            -   ^   =  loss of slope, equal to the shear angle

                                  There  are two elastic equations for the beam, which  are
                                                                                          (9.6-1)
                                                            dx   kAG
                                                           difj  _  M                     (9.6-2)
                                                            dx   El
                                                                                     :
                              where  A  is  the  cross-sectional  area,  G  is  the  shear  modulus,  A  is  a  factor
                              depending on  the  shape  of the  cross  section,  and  El  is  the bending stiffness.  For













                                               Figure 9.6-1.   E ffect  o f shear  deform ation.
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