Page 65 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 65

52                                 Harmonically Excited Vibration   Chap. 3













                                                   Fn  sin  cot

                                    Figure   3.1-1   Viscously   Figure  3.1-2.  Vector  relationship
                                    damped  system  with  har­  for forced vibration with  damping.
                                    monic excitation.

                             integral.  The complementary function,  in this case,  is a damped free vibration  that
                             was discussed  in Chapter 2.
                                  The particular solution to the preceding equation  is a steady-state oscillation
                             of the  same  frequency  co  as  that  of the  excitation.  We  can  assume  the  particular
                             solution  to be of the form
                                                      X   = X     -   (¡))               (3.1-2)
                             where  X   is  the  amplitude  of oscillation  and  cf)  is  the  phase  of  the  displacement
                             with  respect to the  exciting force.
                                  The  amplitude  and phase  in  the previous equation  are  found by substituting
                             Eq.  (3.1-2)  into  the  differential  equation  (3.1-1).  Remembering  that  in  harmonic
                             motion  the  phases  of the velocity  and  acceleration  are  ahead  of the  displacement
                             by  90°  and  180°,  respectively,  the  terms  of  the  differential  equation  can  also  be
                             displayed graphically,  as in  Fig.  3.1-2.  It  is easily seen from this diagram that

                                                    =                                    (3.1-3)

                                                        {k  —mco^)  +  {ciüŸ
                              and
                                                              CO)

                                                  <>=  tan  '  ---------- j              (3.1-4)
                                                   f
                                                           k  —mco

                                  We now express Eqs. (3.1-3) and (3.1-4) in nondimensional form that enables
                              a  concise  graphical  presentation  of  these  results.  Dividing  the  numerator  and
                              denominator of Eqs.  (3.1-3) and (3.1-4) by  /c, we obtain
                                                     =                                    (3.1-5)
                                                              mo)^
                                                                      { coj Ÿ
                                                          [^
                                                        V(>-— )     Mt )
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