Page 253 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 253

240                                    Computational Methods   Chap. 8


                                  Thus,  the  frequency of the  lovs/cst  mode  is
                                                                  =  0.457-1/ —
                                                       ^  V  it : 32m   V  ^
                                  with  the  mode  shape
                                                                 0.250)
                                                           c/>,  == {0.790

                                                                 1.000  j
                                       It  should  be  mentioned  here  that  if the  equation  of motion  was  forriiulated  in
                                  terms of the  stiffness  matrix,  the  iteration  equation would be
                                                                AX = AX
                                                          [M~'K]X = co"X
                                  Because  the  iteration  procedure  always  converges  to  the  largest  eigenvalue,  the
                                  stiffness equation would converge to the highest mode.  In vibration analysis, the lower
                                  modes  arc  generally  of  greater  interest  than  the  higher  modes,  so  that  the  matrix
                                  iteration  procedure  will  find  its  use  mainly  for  equations  formulated  in  terms  of
                                  flexibility where  the  eigenvalues are  proportional  to the  reciprocal of co^.


                       8.4  CONVERGENCE OF THE ITERATION  PROCEDURE

                              To show that the iteration proeedure eonverges to the largest eigenvalue, whieh for
                              the equation formulated  in terms of flexibility is the lowest fundamental mode, the
                              assumed  trial  veetor  X^  is  expressed  in  terms  of  the  normal  modes  (/>,  by  the
                              expansion  theorem:

                                                 X^  =    +  r*2^2   ^3^3  T  ■■‘  T      (8.4-1)

                              where   are  constants.  Multiplying  this  equation  by  the  dynamic  matrix  A,  we
                              have
                                           A X ^   —  X 2  —  c^Acf)^  +   C2v4</>2  T   c^Acf)^  +   *  *  ■ +    (8.4-2)

                              Because  each  normal  mode  satisfies the  following equation

                                                                                          (8.4-3)

                              the  right side  of Eq.  (8.4-2) becomes
                                             4^2  =  C| —  <(>|  +   C2 —  <I>2  +    —    ■  +
                                                   CU 1     CO 2    OJ 2
                              which  is  the  new  displacement  vector  X 2.  Again,  premultiplying  X 2  by  the
                              dynamic matrix and  using  Eq.  (8.4-3),  the  result  is

                                          AX^  =  X 2  =  Cj —  -f  C2 —  4>2  +  <^ 3 ~4 ^ 3  T  * •  '  T
                                                      O),      CO 2
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