Page 406 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 406

Sec. 12.6   Mykiestad’s Method for Beams                       393

















                                                                     Figure  12.5-4.


                                  The  mode  shapes  ean  be  found  by  printing  out   for  each  of  the  preceding
                                  frequencies.





                       12.6  MYKLESTAD’S METHOD FOR  BEAMS
                              When a beam is replaced by lumped masses connected by massless beam sections,
                              a method developed by N. O. Myklestad^ can be used to progressively compute the
                              deflection,  slope,  moment,  and  shear  from  one  section  to  the  next,  in  a  manner
                              similar to the  Holzer method.


                                  Uncoupled flexural vibration.  Figure  12.6-1  shows a  typical section  of an
                              idealized beam with lumped masses. By taking the free-body section in the manner
                              indicated,  it will be possible to write equations for the shear and moment at  /  +  1
                              entirely  in  terms  of  quantities  at  /.  These  can  then  be  substituted  into  the
                              geometric equations for  6  and  y.
                                  From  equilibrium considerations, we  have

                                                       K+i  =    m ^ y ,                 ( 12.6-1)
                                                      M „ ,  = M ,  -   1^.,,/,          ( 12.6-2)

                              From  geometric  considerations,  using  influence  coefficients  of  uniform  beam


                                  ^N.  O.  Myklestad,  “A  New  Method  of  Calculating  Natural  Modes  of  Uncoupled  Bending
                              Vibration  of Airplane  Wings  and  Other  Types  of Beams,”  J.  Aero.  Sci.  (April  1944),  pp.  153-162.
                                  N.  O.  Myklestad,  “Vibration  Analysis,”  McGraw-Hill,  N.Y.  (1944).
   401   402   403   404   405   406   407   408   409   410   411