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0593_C07_fm  Page 222  Monday, May 6, 2002  2:42 PM





                       222                                                 Dynamics of Mechanical Systems


                       and
                                                          aa [
                                                                       aa ]
                                                 a = ( I − )  I +( I − ) 2  12
                                                              2
                                                  2   11  I   12   11  I                       (7.9.46)
                        When a plane of symmetry is identified or when a system or body is planar, the analysis
                       is two dimensional, as above. In this case, the transformation between different unit vector
                       sets is also simplified. Recall from Eqs. (7.5.5) and (7.5.7) that the moments and products
                       of inertia referred to unit vectors  ˆ n   and n  are related by the expression:
                                                      k      i
                                                          ˆ I =
                                                               ik jl
                                                          kl  S S I ij                         (7.9.47)
                       where the transformation matrix components are defined by Eq. (7.5.6) as:

                                                                ⋅
                                                          S = nn ˆ                             (7.9.48)
                                                           ik  i  k
                        Suppose the unit vectors n , n , and n  are principal unit vectors, with n  being normal
                                                          c
                                                                                         c
                                                   b
                                                a
                       to a plane of symmetry. Let n , n , and n  be mutually perpendicular unit vectors, with
                                                     2
                                                            3
                                                  1
                       n  being parallel to n . Let θ be the angle between n  and n  as in Figure 7.9.2. Then, the
                        3
                                                                            a
                                          c
                                                                     1
                       transformation matrix components between the n  (i = 1, 2, 3) and the n  (α = a, b, c) are:
                                                                                       α
                                                                   i
                                                         cos θ   sin θ    0
                                                         
                                                    ⋅
                                                  nn = −sin   θ   cos θ  0                    (7.9.49)
                                                   i  α                  
                                                         0       0        1
                       Using Eq. (7.9.47), the moments and products of inertia I , relative to n  and n , then become:
                                                                                         j
                                                                                   i
                                                                       ij
                                                     I = cos θ I + sin θ I                     (7.9.50)
                                                            2
                                                                    2
                                                     11       aa       bb
                                                                     aa (
                                                              θ
                                                  I =  I = −sin cosθ  I − )                    (7.9.51)
                                                                        I
                                                  12   21                bb
                                                     I = sin θ I + cos θ I                     (7.9.52)
                                                           2
                                                                    2
                                                     22       aa       bb
                                                     I =  I =  I = I =  0                      (7.9.53)
                                                      13  31   23  32
                                                           I =  I                              (7.9.54)
                                                            33  cc
                        Equations (7.9.50), (7.9.51), and (7.9.52) may be expressed in an even simpler form by
                       using the trigonometric identities:
                                                        sin θ ≡  1 −  1 cos2θ
                                                          2
                                                               2  2
                                                         cos ≡  1 +  1 cos2θ                   (7.9.55)
                                                           2
                                                               2  2
                                                       θ
                                                    sin cosθ ≡  1 sin2θ
                                                               2
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