Page 350 - Thomson, William Tyrrell-Theory of Vibration with Applications-Taylor _ Francis (2010)
P. 350

Chap. 10   Problems                                            337


                              equation for  w,.
                                                                 420 £/      420A, £ /
                                                        Ù),  =  w A     =  4
                                              420£:/            m {l/2 y       m r

                              With  this  change,  the  computer  results  for  A,  and  the  natural  frequencies  of  a
                              two-element  beam  of  length  /  are  shown  in  Table  10.8-1.  The  case  for  il  =  0  is
                              compared to exact values, which  shows that the  results are quite  good for the first
                              two modes.
                                  Shown  in Figures  10.8-4 and  10.8-5  are two helicopters of different size. The
                              Robinson  Helicopter,  Model  R22,  shown  in  Figure  10.8-4  is  a  small  two-seater
                              vehicle  used  mainly  for  pleasure  flying.  The  descriptive  data  accompanying  the
                              photo  indicates some of its specifications and  size.
                                  In  contrast,  the  commercial  helicopter,  shown  in  Figure  10.8-5,  used  for
                              hauling  material  and  workers  between  shore  and  oil  platforms  is  a  large  vehicle
                              capable of transporting a maximum load of 6000 lbs. As in all helicopters, the rotor
                              blades  are very flexible.  Their  rotational  speed  is  governed by  the  requirement  of
                              keeping the tip speed below the speed  of sound.



                                                        R E F E R E N C E S
                              111  Cook,  R.  D.  Concepts  and Applications  of Finite  Element Analysis.  New  York:  John
                                  Wiley &  Sons,  1974.
                              12]  Gallagher,  R.  H.  Finite  Element  Analysis  Fundamentals.  Englewood  Cliffs,  NJ:
                                  Prentiee-Hall,  1975.
                              131   Rockey,  K.  C.,  Evans,  H.  R.,  G rieehh,  D.  W.  and  N etheroot,  D.  A.  The  Finite
                                 Element Method.  New York:  Halsted  Press  Book, John  Wiley  &  Sons,  1975.
                              [4]  Yang,  T.  Y.,  Finite Element Structural Analysis.  Englewood  Cliffs,  NJ:  Prentiee-Hall,
                                  1986.
                              [5]  Weaver,  W.,  and  Johnston,  P.  R.  Structural  Dynamics  by  Finite  Elements.  Engle­
                                 wood Cliffs,  NJ:  Prentiee-Hall,  1987.
                              [6]  Clough,  R.  W.  and  Penzien,  J.  Dynamics  of Structures.  New  York:  McGraw-Hill,
                                  1975.
                              [71  Craig,  R.  R.  Jr.  Structural Dynamics.  John  Wiley  &  Sons,  1981.



                                                         P R O B L E M S

                              10-1  Determine  the two natural  frequencies in  axial vibration  for the  uniform  rod, fixed at
                                  one  end  and  free  at  the  other end,  using  two  elements with  the  intermediate  station
                                  at  //3  from  the  fixed  end.  Compare  results with  those  when  the  station  is  chosen  at
                                  midlength. What  conclusion  do you  come  to regarding choice  of station  location?
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