Page 153 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 153

140                   Systems with Two or More Degrees of Freedom   Chap. 5

                                        M  l Z Î

                                                      n-fin    k:(Xc~l^e)


                                          Figure 5.3-3.  Coordinates leading to dynamic coupling.


                                         h     I-
                                                    = l
                                                     il'                       U2(^1

                                      Figure 5.3-4.  Coordinates leading to static and dynamic coupling.

                             If  /cj/,  =  ^ 2^2’   coupling  disappears,  and  we  obtain  uncoupled  x  and  6
                             vibrations.

                                  Dynamic  coupling.  There  is  some  point  C  along  the  bar  where  a  force
                             applied  normal  to  the  bar  produces  pure  translation;  i.e.,   ^ 2^4*
                             5.3-3.) The  equations of motion  in terms of   and  6  can be  shown to be

                                      m   me  ("•)+ [ ( /c j  + /C2 )   0
                                      me      1 «)  [     0      { k j j   + k ,li)  e

                             which  shows  that  the  coordinates  chosen  eliminated  the  static  coupling  and
                             introduced  dynamic coupling.

                                  Static and dynamic coupling.  If we choose  x  =   at the end of the bar,
                             as shown  in  Fig.  5.3-4,  the equations of motion become

                                          m   ml^         (^1  +  ^ 2)  k^l  ■
                                                  P . : U
                                         mi^   y,            k^l           e
                              and both  static and  dynamic coupling are  now present.
                              Example 5.3-2
                                  Determine  the  normal  modes  of vibration  of an  automobile  simulated by  the  simpli-
                                  hed  2-DOF system with  the  following numerical values (see  Fig. 5.3-5):

                                            IT =  3220 lb   L  =  4.5 ft  k^  =  2400 Ib/ft
                                               ^   2
                                            ,
                                            T. =  —r                  ^2  =  2600 Ib/ft
                                            ^    g
                                             r =  4Ü      / =  10 ft
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