Page 365 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 365

352            Mode-Summation Procedures for Continuous Systems   Chap. 11


                              Eq.  (11.1-3),  but  by the  equation
                                                                       0    if j   i
                                            / [m{x)<pj<p,  + y(x)(A^.iA,]  cbc           ( 11.2-1)
                                                                       M,   if j  =  i
                              whieh  ean be proved  in  the following manner.
                                  For  eonvenience,  we  rewrite  Eqs.  (9.6-5)  and  (9.6-6),  ineluding  a  distributed
                              moment  per unit  length  2??(x, t):
                                          A         + ^ g ( ^   - < a )          = 0      (9.6-5)
                                          dx
                                              my   A  k A G \ ^   -   ^  P{x,t)  =  0     (9.6-6)
                                                   dx
                              For  the  foreed  oseillation  with  exeitation  p{x,t)  and  3?î(x,/)  per  unit  length  of
                              beam,  the  deflection  y{x,t)  and  the  bending  slope  ijjix.t)  can  be  expressed  in
                              terms  of the generalized coordinates:

                                                        '
                                                       >  =  E'?,(0<P;(-*')
                                                                                         (11.2-2)
                                                       •A =  E'7/(0'A.,(-ï )

                              With these  summations  substituted  into the  two beam  equations, we  obtain
                                               =  E ^ ,        +  kAG(<p'^  -   ^2  -h  23î( jc, t)
                                                                                         (11.2-3)
                                       m       =  'LQi-jz{kAG{tp)  -   (Ay))  + p ( x , t )

                              However,  normal  mode vibrations  are of the  form
                                                         y  =  <p^{x)e“^'‘
                                                                                         (11.2-4)
                                                         Ip  =  4>j(x)e'‘“i'
                              which, when  substituted  into the beam  equations with zero excitation,  lead  to


                                                         ^                               (11-2-5)
                                               -  cojmipj  =   -j^[kAG{<p'j  -  lA)]
                                                                       ,
                              The  right  sides  of  this  set  of  equations  are  the  coefficients  of  the  generalized
                              coordinates  Qj  in the forced vibration equations,  so that we can write  Eqs. (11.2-3)
                              as
                                                        =  -   Ei'yWyViAy   ® i(x ,i)
                                                                                         ( 11.2-6)
                                                 'H P j^Pj  =  -     + p { x , t )
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