Page 185 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 185

172                              Properties of Vibrating Systems   Chap. 6


                       6.1  FLEXIBILITY INFLUENCE COEFFICIENTS
                              The flexibility matrix written  in  terms of its coefficients  a^j  is
                                                               ^12  « 13 '
                                                          «21                             ( 6.1-1)
                                                   x A   =     ^22  ^23  r
                                                   x ^ j  «31  ^32  ^33  1/3
                                  The  flexibility  influence coefficient a^j  is defined  as the  displacement  at  i  due
                              to  a  unit  force  applied  at  j  with  all  other  forces  equal  to  zero.  Thus,  the  first
                              column  of  the  foregoing  matrix  represents  the  displacements  corresponding  to
                              /,  =  1  and  /2  = /3  =  0.  The  second  column  is  equal  to  the  displacements  for
                              /2  =  1 and  /j  = /3  =  0,  and  so on.

                              Example 6.1-1
                                  Determine  the  flexibility matrix for the  three-spring system  of Fig.  6.1-1.
                              Solution:  By  applying  a  unit  force  ]\  =  1  at  (1) with  /2  =   =  0,  the  displacements,  X|,
                                  ^2,  and  X3,  are  found  for the  first column of the  flexibility matrix
                                                            l/ki  0  o'  f/,  =  l
                                                            l/kt  0  0
                                                            l/k,  0  0
                                                                         0
                                  Here  springs  k2  and   are  unstretched  and  are  displaced  equally with station (1).
                                       Next,  apply  forces  /j  =  0,  /2  =  1,  and   =  0 to obtain
                                                          “
                                                    i  \
                                                           0     ^       0
                                                                1
                                                    •^2 >  ==  -1—   - f
                                                                    L )
                                                                1   1
                                                    X3     0   7— +  T-  0

                                                    V    )
                                  In  this case,  the  unit  force  is transmitted  through  k^  and  ^2,  and  k^  is  unstretched.
                                       In  a  similar manner,  for /j  = 0, f 2 =  0,  and  /3  =  1, we  have
                                                          0   0

                                                          0        1   1
                                                   ^2        0    1-  +  -T-

                                                          0  0
                                                                             V

                             I—VNM^  (1)           (2)  ^AAA/—  (3)

                                                 I— >             3   Figure 6.1-1.
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