Page 180 - Biaxial Multiaxial Fatigue and Fracture
P. 180

BiaxiallMultiaxial Fatigue and Fracture
           Andrea Carpinteri, Manuel de Freitas and Andrea Spagnoli (Eds.)
           Published by Elsevier Science Ltd. and ESIS.                        165






                  SEQUENCED AXIAL AND TORSIONAL CUMULATIVE FATIGUE:
                  LOW AMPLITUDE FOLLOWED BY HIGH AMPLITUDE LOADING


                                       Peter BONACUSE
                                   US Army Research Laboratory,
                                   NASA Glenn Research Center,
                                      Brook Park, OH, USA
                                             and
                                      Sreeramesh WLURI
                                     Ohio Aerospace Institute,
                                   NASA Glenn Research Center,
                                      Brook Park, OH, USA





           ABSTRACT
           The experiments described herein were performed to determine whether damage imposed by
           axial loading interacts with damage imposed by torsional loading,  This paper is a follow on to
           a study [ 11 that investigated effects of  load-type sequencing on the cumulative fatigue behavior
           of  a cobalt base superalloy, Haynes  188, at 538°C.  Both the current and the previous study
           were used to test the applicability of  cumulative fatigue damage models to conditions where
           damage is imposed by different loading modes.  In the previous study, axial and torsional two
           load level cumulative fatigue experiments were conducted, in  varied combinations, with the
           low-cycle fatigue (high amplitude loading) applied first.  In  present study, the low amplitude
           fatigue loading was  applied initially.  As  in  the previous study, four sequences (axial/axial,
           torsion/torsion,  axial/torsion,  and  torsion/axial)  of  two  load  level  cumulative  fatigue
           experiments  were  performed.  The  amount  of  fatigue  damage  contributed by  each  of  the
           imposed loads was estimated by both the Palmgren-Miner linear damage rule (LDR) and the
           non-linear, damage curve approach (DCA).  Life predictions for the various cumulative loading
           combinations  are compared with  experimental results. Unlike the previous study where  the
           DCA  proved  markedly  superior,  no  clear  advantage  can  be  discerned  for  either  of  the
           cumulative fatigue damage models for the loading sequences performed.  In addition, the cyclic
           deformation behavior under the various combinations of loading is presented.

           KEYWORDS

           Multiaxial, cumulative fatigue, axial loading, torsional loading, tubular specimens.
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