Page 55 - Biaxial Multiaxial Fatigue and Fracture
P. 55

40                           G. SAVAIDIS ET AL.

           material data, but  this is not  the subject of  the current paper.  On  the other hand the  result
           reveals  some  aspects  of  the  problems when  dealing  with  life  prediction  in  an  industrial
           environment: As  the  tapered tube  is  known  from experience to  survive quite  a number of
           truck lives further investigations on the component have minor priority. Nevertheless, gaining
           experience with life prediction techniques is the prerequisite to apply them in design process.



















               Failure-critical  location calculated
               with hot spot approach and local
               approach


           Fig. 23. Experimental tested new geometry, crack initiation at tapering of tube


           CONCLUSIONS
           The mechanical behaviour and fatigue life of  a thin-walled tube joined to a forged component
           by fillet welding has been  investigated. The component is loaded by nonproportional random
            sequences of  bending and torsion as measured during operation. The stresses in the welded
            structure  have  been  calculated  using  finite  element  analysis.  The  fatigue  life  has  been
           determined theoretically, by  means of  the hot  spot and local stresses in conjunction with the
           critical  plane  approach,  and  experimentally. Though  the  experimental  data  base  is  quite
           narrow, basic trends can be  derived from the present  investigation concerning the possible
           field  of  application  and  capability of  the  theoretical approaches calculating fatigue  life  of
           vehicle components.
            1.  A coarse finite element model of  the component has been created in accordance with the
              IIW guideline for application of  the hot  spot stress approach. Comparison of numerically
              and experimentally determined end-results (fatigue lifetimes) shows that the coarse model
              is suitable to determine lifetimes with  the hot spot stress approach, if  a reliable hot spot
              stress-life  curve  at  constant  amplitude  loading  is  existing  for  the  detail  investigated.
              Because  of  the  coarse  mesh,  the  geometry of  the  weld  is  not  modelled  in  detail.  For
              instance, in this investigation only one failure-critical location has been detected.
           2.  If experimental results are missing, appropriate S-N curves from publications, e.g.  the IIW
              guideline or Eurocode can  be  used.  In  cases of  multiaxial loading causing normal  and
              shear stresses, attention must be  paid to the  slope of  the S-N curve used, since various
              suggestions  are  reported  in  the  literature. The  major  advantage of  the  hot  spot  stress
              approach is a relatively low expense to model and calculate.
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