Page 388 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 388

Sec. 12.1  Rayleigh Method                                     375


                                  The  additional  strain  energy in  element  dx  is
                                                       dU =  {aAedx =  {EAe^ dx
                                  where  A  is the cross-sectional area, a  is the stress due to tension, and  e  =  \idy/dxY
                                  is the unit strain.
                                      Equating  the  kinetic  energy  to  the  total  strain  energy  of bending  and  tension,
                                  we obtain
                                                       =              +            dx

                                  The preceding equation  then  leads  to the frequency equation:

                                                           d^y
                                                      fEI       dx -y
                                                           dx^
                                                                jy^ dm

                                  which contains an  additional  term due  to tension.

                                  Accuracy  of  the  integral  method  over  differentiation.  In  using
                              Rayleigh’s method  of determining the  fundamental frequency, we must choose  an
                              assumed curve. Although the deviation of this assumed deflection curve compared
                              to the  exact curve may be slight,  its derivative could be in error by a large amount
                              and hence the strain energy computed  from  the equation


                                                      u - I / e ;     dx
                                                                dx^
                              may  be  inaccurate.  To  avoid  this  difficulty,  the  following  integral  method  for
                              evaluating  U  is recommended  for some  beam  problems.
                                  We  first  recognize  that  the  shear  V  is  the  integral  of  the  inertia  loading
                              ma)^y  from the free end of the beam,  as indicated by both Figs.  12.1-3 and  12.1-4.

                                                    V{^)  = c o ^fm ie )y(^)d ^         (12.1-13)

                              Because bending moment  is related to the  shear by the  equation
                                                           dM
                                                            dx  =  E                    (12.1-14)







                                                                     Figure  12.1-3.
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