Page 209 - The Combined Finite-Discrete Element Method
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192    TEMPORAL DISCRETISATION

            However, the angular momentum at time t is easier to calculate using the element frame
            of reference:
                                                             
                                                     0   0
                                       −t H x    I x          t ω x
                               −t H =    −t H y    =    0  I y  0     t ω y    (5.70)
                                       −t H z     0  0   I z  t ω z
            Thus the transformation matrix (5.46) is employed to obtain the components of angular
            velocity, which after substitution in (5.70) yields
                                                                 
                                                   ˜    ˜   ˜       
                               −t H x     I x  0  0    t i x  t j x  t k x  t ω ˜x
                                                                ˜
                                                            ˜
                                                                  
                       −t H =    −t H y    =    0  I y  0      ˜  t j y  t k y    t ω ˜y    (5.71)
                                                      t i y
                               −t H z     0   0  I z    ˜   ˜   ˜     t ω ˜z
                                                       t i z  t j z  t k z
            The same angular momentum in the inertial frame of reference is given by
                                                      
                             −t H ˜x   t i ˜x  t j ˜x  t k ˜x  −t H x
                     −t H =    −t H ˜y    =    t i ˜y  t j ˜y  t k ˜y    −t H y    (5.72)
                             −t H ˜z   t i ˜z  t j ˜z  t k ˜z  −t H z
                                                                   
                                                      ˜   ˜    ˜      
                             t i ˜x  t j ˜x  t k ˜x  I x  0  0  t i x  t j x  t k x  t ω ˜x
                                                              ˜
                                                                   ˜
                                                                    
                         =    t i ˜y  t j ˜y  t k ˜y     0  I y  0      ˜  t j y  t k y     t ω ˜y  
                                                        t i y
                             t i ˜z  t j ˜z  t k ˜z  0  0  I z  ˜  ˜  ˜  t ω ˜z
                                                         t i z  t j z  t k z
            In the inertial frame of reference, rotational motion of the discrete element is governed
            by the Euler second law, equation (5.57). At time t the total forces and moments acting
            on the discrete element are calculated using the usual contact routines, which include
            detection of contacts and solving contact interaction between each couple of interacting
            discrete elements. These are expressed as the resultant force and moment acting on the
            centre of mass of the discrete element. At time t the latter is given in the inertial reference
            frame as
                                                               
                                                            t M ˜x
                                         ˜      ˜     ˜                          (5.73)
                                 t M = t M ˜x i + t M ˜y j + t M ˜z k =    t M ˜y  
                                                            t M ˜z
            At this point an assumption that the change in angular momentum due to the external
            moment from equation (5.73) can be approximated by

                                             H = Mh                              (5.74)

            is introduced. The physical meaning of this approximation is equivalent to the assumption
            that the external moment is applied as impulse at time t. Thus the total external moment
            on the discrete element is approximated as a sum of impulse loads acting at specified
            time intervals, i.e. at the beginning of each time step (Figure 5.5).
              The updated angular momentum at time t is therefore given as follows:

                                                           
                                       t H ˜x    −t H ˜x   t M ˜x h
                                t H =    t H ˜y    =    −t H ˜y    +    t M ˜y h    (5.75)
                                       t H ˜z    −t H ˜z   t M ˜z h
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