Page 358 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 358

11






                                  Mode-Summation Procedures

                                       for Continuous Systems












                              Structures made up of beams are common in engineering.^ They constitute systems
                              of  an  infinite  number  of degrees  of freedom,  and  the  mode-summation  methods
                              make  possible  their  analysis  as  systems  of a  finite  number of degrees of freedom.
                              The effect of rotary inertia and shear deformation is sometimes of interest in beam
                              problems.  Constraints are often found  as additional supports of the structure,  and
                              they  alter  the  normal  modes  of  the  system.  In  the  use  of  the  mode-summation
                              method,  convergence  of  the  series  is  of  importance,  and  the  mode-acceleration
                              method offers a varied approach. The modes used in representing the deflection of
                              a  system  need  not  always  be  orthogonal.  The  synthesis  of  a  system  using
                              nonorthogonal functions is illustrated.
                                  Large structures such as space stations are generally composed of continuous
                              sections which can be  analyzed by the mode  participation  methods.  Shown  in  Fig.
                              11.1-1  is  one  such  design,  parts  of  which  offer  opportunities  for  challenging
                              analysis.



                       11.1  MODE-SUMMATION  METHOD
                              In Sec. 6.8, the equations of motion were decoupled by the modal matrix to obtain
                              the  solution  of forced vibration  in  terms  of the  normal  coordinates of the  system.
                              In  this  section,  we  apply  a  similar  technique  to  continuous  systems  by  expanding
                              the deflection  in  terms  of the  normal  modes of the  system.


                                  ^The  Olympus  Satellite,  shown  in  Figure  11.1-1,  is  one  of  several  configurations  proposed  for
                              deployment  in  space.  The  large  panels  of  solar  cells  are  deployed  by  lightweight  booms  of glass  fiber,
                              ingeniously  designed  to  extend  the  panels  for  hundreds  of feet.

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