Page 285 - Dynamics of Mechanical Systems
P. 285

0593_C08_fm  Page 266  Monday, May 6, 2002  2:45 PM





                       266                                                 Dynamics of Mechanical Systems


                                                                                   *
                       where a  is the n  component of a and T  is the n  component of T ; a  may be obtained
                                                                                     2
                                      2
                              2
                                                                   3
                                                           3
                       directly from Eq. (8.12.8), and, because  n ,  n , and  n  are parallel to principal inertia
                                                                        3
                                                             1
                                                                2
                       directions of B for G, T  is given by Eq. (8.6.12) as:
                                           3
                                                               1 (
                                                   T =−α  I + ω ω  I − )                      (8.12.13)
                                                                       I
                                                    3    3 33    2  11  22
                       where α , ω , and ω  can be obtained directly from Eqs. (8.12.5) and (8.12.6) and where
                                         2
                                 1
                              3
                       from the inertia properties of a slender rod, I , I , and I  are:
                                                                  22
                                                               11
                                                                         33
                                                    I =  0,  I =  I =  ml 2  12               (8.12.14)
                                                    11     22  33
                        Finally, by substituting from Eqs. (8.12.5), (8.12.6), (8.12.10), (8.12.13), and (8.12.14) into
                       (8.12.12), we obtain:
                                                       [
                                                                                      )
                                                            ˙˙
                                                                                       ˙˙
                                                                        θ
                                    − ( ) 2 sinθ − ( ) ( ) −( ) 2 Ω 2 sin cosθ ] (ml 12 θ
                                                         l 2 θ
                                                                              −
                                                                                   2
                                      mg l
                                                               l
                                                  m l 2
                                            )
                                    +(ml 12 Ω 2 sin cosθ  = 0
                                                  θ
                                         2
                       or
                                                                    θ
                                                ˙˙    2l ) sinθ − Ω 2  sin cosθ = 0           (8.12.15)
                                                θ +(3g
                                     ˙
                        Observe that  Ω  does not appear in this governing equation. This means that the angular
                       speed change of S does not affect the movement of B, except indirectly through Ω. Observe
                       further that, if Ω is constant, B has two equilibrium positions, that is, positions of constant θ:
                                                θ = 0   and    θ =  cos  −1 (3g  2lΩ  2 )     (8.12.16)
                       This last result shows that the inertia torque is important even when a body is moving at
                       a uniform rate. Indeed, if the body is not moving with uniform planar motion, its inertia
                       torque is not generally zero. Consider again the expression for T  of Eq. (8.12.13):
                                                                                3
                                                               1 (
                                                   T =−α  I + ω ω  I − )                      (8.12.17)
                                                                       I
                                                    3    3 33    2  11  22
                       Observe that even if α  is zero, T  is not zero unless the second term is also zero.
                                                    3
                                           3
                        The erroneous neglect of the inertia torque can of course produce incorrect results. For
                       example, suppose that in the current problem, where we are seeking the equilibrium
                       position with Ω constant, we construct an incorrect free-body diagram, as in Figure 8.12.4.
                       By setting moments about O equal to zero, we would obtain:
                                               (
                                                   2
                                              m l 2) Ω sin cosθ − (         =  0              (8.12.18)
                                                          θ
                                                                 mg l 2)sinθ
                                                      2
                       or
                                             cosθ = 2g lΩ 2     or    θ = cos (2g lΩ 2 )      (8.12.19)
                                                                      −1
                       The incorrectness of this result is seen by comparison with Eq. (8.12.16).
   280   281   282   283   284   285   286   287   288   289   290