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0593_C11_fm  Page 371  Monday, May 6, 2002  2:59 PM





                       Generalized Dynamics: Kinematics and Kinetics                               371



                             O  y

                           O
                                    O  x
                                                         kx
                                                           1              k(x  - x  )   k(x  - x  )
                                                                                         3
                                                                             2   1  1       2
                                    G                                                             C
                                                                     C              C               3
                                                                      1               2
                          C                               P                P
                           1                               1                2             P  3
                            C   Mg
                              2
                                C                             mg   k(x  - x  )   mg  k(x  - x  )   mg  kx
                                                                                     3
                                                                                       2
                                                                        1
                                                                     2
                                  3                                                                  3
                       FIGURE 11.7.4                     FIGURE 11.7.5
                       Free-body diagram of the applied  Free-body diagrams of the applied forces on the particles.
                       forces on the tube T.
                       and
                                             v =  0  ,  v =  0  ,  v =  0  ,  v = ( L 2) n      (11.7.7)
                                               G
                                                              G
                                                                      G
                                                      G
                                               ˙ x 1   ˙ x 2  ˙ x 3   ˙ θ      2
                        Consider next the forces acting on the particles and on the tube T. Figures 11.7.4 and
                       11.7.5 contain free-body diagrams showing applied forces on T and the particles. In these
                       figures C , C , and C  represent contact forces between the particles and T applied at points
                                 2
                                        3
                              1
                       Q , Q , and Q  of T. O  and O  are components of the pin reaction forces at O on T.
                                   3
                                                 y
                        1
                           2
                                          x
                        With forces applied at O and at Q , Q , and Q , it is necessary to also determine the
                                                           2
                                                                   3
                                                        1
                       partial velocities of O, Q , Q , and Q . Because O is fixed in our inertial frame we have:
                                                       3
                                             1
                                                2
                                                             O
                                                            v = 0                               (11.7.8)
                       and then:
                                                     v =  v = v =  v =  0                       (11.7.9)
                                                               O
                                                                    O
                                                          O
                                                      O
                                                      ˙ x 1  ˙ x 2  ˙ x 3  ˙ θ
                        Points Q , Q , and Q  are points of T at the positions of P , P , and P . Their velocities are:
                                   2
                                          3
                                                                                   3
                                                                            2
                                1
                                                                          1
                                                       v Q 1  = (l + x )θ ˙  n                 (11.7.10)
                                                                1    2
                                                             l
                                                       v Q 2  = ( 2 + x )θ ˙  n                (11.7.11)
                                                                 2   2
                                                          = (      ˙
                                                             l
                                                        Q 3
                                                       v    3 + x )θ n                         (11.7.12)
                                                                 3   3
                       Hence, the partial velocities of Q , Q , and Q  are:
                                                    1
                                                               3
                                                       2
                                           v Q 1  =  0  ,  v Q 1  =  0  ,  v Q 1  =  0  ,  v Q 1  = (l +  x  n )
                                            ˙ x 1   ˙ x 2    ˙ x 3   ˙ θ    1  2
                                                                         2 +
                                           v Q 2  =  0  ,  v Q 2  =  0  ,  v  Q 2  =  0  ,  v Q 2  = ( l  x  n )  (11.7.13)
                                            ˙ x 1   ˙ x 2    ˙ x 3   ˙ θ      2  2
                                           v Q 3  =  0  ,  v Q 3  =  0  ,  v Q 3  =  0  ,  v Q 3  = ( 3l + )n
                                                                          l x
                                            ˙ x 1   ˙ x 2    ˙ x 3   ˙ θ      3  2
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