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0593_C09_fm  Page 291  Monday, May 6, 2002  2:50 PM





                       Principles of Impulse and Momentum                                          291


                       By integrating over the time interval in which the forces are applied, we have:


                                            t 2     t 2
                                            ∫ M dt = ∫ ( d A SQ )  A () − A ()
                                                            dt dt =
                                                                       t
                                                                               t
                                                                            SQ
                                               Q
                                                                    SQ
                                                                       2
                                                                                1
                                            t 1     t 1
                       or
                                                          J =∆ A                               (9.6.16)
                                                           Q     S Q
                       where here J  represents the sum of the angular impulses of the applied forces about Q
                                  Q
                       during the time interval (t , t ). Hence, as with a single particle, the angular impulse about
                                                2
                                              1
                       a point Q fixed in an inertial reference frame is equal to the change in angular momentum
                       of the set of particles about Q.
                        Finally, consider a rigid body B moving in an inertial reference frame R as in Figure
                       9.6.5. Let G be the mass center of B, let Q be a reference point, and let O be the origin of
                       R. Then, from Eqs. (9.4.8), (9.4.12), and (9.4.13), the angular momenta of B about O, Q,
                       and G are:

                                              A   =  A  +  A  =  I BG ⋅ωω + P × m v G          (9.6.17)
                                                BO    B G  G O          G
                                                                          ×
                                             A    =  A  +  A  =  I BG ⋅ωω +  QG m v G          (9.6.18)
                                               BQ    B G   G Q

                                                         A   =  I  BG ⋅ωω                      (9.6.19)
                                                          BG
                       where P  and QG locate G relative to O and Q as in Figure 9.6.5, and where as before ωω ωω
                              G
                       is the angular velocity of B in R, I B/G  is the central inertia dyadic of B, and m is the mass
                       of B. Consider the derivatives of these momenta. For A B/O  we have:

                                                                       G (
                                                             ωω
                                           R dA BO  dt = (  B G ⋅ )  dt +  R d P × mv )  dt
                                                                             G
                                                      R
                                                       d I
                                                                           ωω
                                                    =  B d I (  B G ⋅ )  dt + ωω ×  I (  B G ⋅ )  (9.6.20)
                                                             ωω
                                                      + v × mv + P ×  ma G
                                                         G    G   G











                       FIGURE 9.6.5
                       A rigid body B moving in an inertial reference
                       frame R and a reference point Q.
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