Page 387 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 387

374                                       Classical Methods   Chap. 12

                              potential  energies,  an  alternative  equation  for  the  fundamental  frequency  of  the
                              beam is
                                                                   , 2
                                                                     dx
                                                           ' - '1 0
                                                                    ----                ( 12.1-12)
                                                              ¡y^  dm
                              Example  12.1-1
                                  In  applying  this  procedure  to  a  simply  supported  beam  of  uniform  cross  section,
                                  shown  in  Fig.  12.1-2,  we  assume  the  deflection  to  be  represented  by  a  sine  wave  as
                                  follows:
                                                               .  1TX\  .
                                                            /
                                                        y  =  I Vqsm -j- I sm o)t

                                  where  yo  is the maximum deflection at midspan. The second derivative then becomes
                                                      d^y    /   77   .  7TX .

                                                             ( j j   >^oSin —  sm (Ot
                                                      dx^
                                  Substituting into Eq.  (12.1-12), we obtain
                                                       El n -r   /  sm^—r   --  dx
                                                         w ;  -/q   /      ,  El
                                                          m j  sm  -j- dx

                                  The  fundamental  frequency,  therefore,  is



                                       In this case, the assumed curve happened to be the natural vibration eurve, and
                                  the  exact  frequency  is  obtained  by  Rayleigh’s  method.  Any  other  eurve  assumed  for
                                  the  case  can  be  considered  to  be  the  result  of  additional  eonstraints,  or  stiffness,
                                  which result  in  a constant greater than   in the  frequency equation.




                                                                     Figure  12.1-2.

                              Example  12.1-2
                                  If the  distance  between  the  ends  of the  beam  of Fig.  12.1-2  is  rigidly fixed,  a  tensile
                                  stress  a  will be developed by the lateral deflection. Account for this additional strain
                                  energy in  the  frequency equation.
                              Solution:  Due  to  the  lateral  deflection,  the  length  dx  of  the  beam  is  increased  by  an
                                  amount

                                                  [V’l  +  {dy/dxf  -   l]  ii»:  s   f  ( ^ )   dx
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