Page 19 - Biaxial Multiaxial Fatigue and Fracture
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4                  K. DANG  VAN, A. BIGNONNETAND 1L. FAYARD

            fatigue cannot be reduced to plane cracks simply characterised by their length a, submitted to
            simple  in  mode  I  loading  and  in  a  linear elastic  regime. This  makes the  calculation  of  the
            parameters which are supposed to govern the propagation extremely difficult. The transcription
            of some parameters which are justified in Fracture Mechanics to fatigue is still poorly founded
            and therefore ambiguous for a structure. It is the case for instance of the J parameter and the J
            derived parameter  usually invoked to correlate fatigue testing results  on  specimens. For  all
            these reasons the local approaches based on crack initiation are still preferred by engineers.
              As  for welded structures, the structural method developed for the offshore industry in the
            70’ and the 80’s (AWS and API codes) and particularly following Radenkovic’s proposals [3],
            is without any doubt the one which allows the most interesting industrial calculations. In this
            method,  the  welded  connection  is  characterised by  a  design  stress  S, more  or  less  clearly
            defined, which better describes the local stress at the <<Hot Spot),. The latter is obtained either
            by  the extrapolation  of  strain values measured by  strain gauges close to the Hot Spot of  the
            structure or by a thin-shell finite element calculation. S is a ccgeometricalv stress which can be
            deduced from the nominal stress using a Stress Concentration Factor obtained by experiment
            and parametric formula. This stress is used to predict the fatigue tests on welded tubular nodes
            submitted to various service loading by means of a unique S-N line.
              It  is this  idea which  is considered in  the following, giving a clearer interpretation of  the
            design stress based on the Dang Van classical fatigue criterion.


            DANG VAN CLASSICAL FATIGUE CRITERION

            This model is presented in detail in  [4]; at the same time, different structural applications are
            given.  In  this  model  the  material  is  considered  as  a  heterogeneous structure  submitted  to
            cyclic loading.
              The investigation of the asymptotic behaviour of elasto-plastic structures submitted to cyclic
            loading is a very important topic in solid mechanics; a great deal of research work is devoted to
            this  subject  and  direct  analysis  methods  are  derived  theoretically: the  techniques  used  for
            estimating the limit cycle of  stress are based on a cinematic and a static approach. Melan [5],
            Koiter [6] theorems for elasto-perfectly plastic materials and their extensions by Mandel et al.
            [7]  for  combined  isotropic  and  cinematic  hardening  material  and  more  recently  by  Q.S.
            Nguyen [8] for a wide class of  inelastic materials called generalised standard materials (which
            contains the previous  ones), are the main  theoretical results supporting the proposed fatigue
            model. These theorems give (sufficient or necessary) conditions for the existence of an elastic
            shakedown regime for a given cyclic loading of an elasto-plastic structure. The key point of the
            proof  is  the  associative  property  of  the  plastic  model, i.e. the  fact that the  plastic  flow  (or
            plastic flow and generalised hardening parameters) is  normal to the convex plasticity domain
            (or to  the  convex  domain  defined by  the  function on  the  ccgeneralised  force spacew for  the
            generalised  standard  material).  The  existence  of  an  elastic  shakedown  state  means  that  a
            residual stress pattern builds up and reaches a stabilised state which does not change anymore
            under further cycling: the stabilised stress cycle is then purely elastic; it also means that the
            dissipated  energy  is  bounded  as  well  as  plastic  strain.  These  properties  are  elegantly
            summarised in the following citation due to Professor W. Koiter [6]: ccif  the total amount of
            plastic work performed in the loading process is accepted as suitable criterion for assessing the
            overall deformation, boundedness of the overall deformation may be proven if the structure has
            a safety factor greater than one with respect to shakedown)>.
               In  Dang Van’s fatigue model, since the material is  considered as a structure, the previous
            results hold with some adaptation: its theoretical foundation is based on  an elastic shakedown
            hypothesis  at  all  scales  of  material  description  near  the  fatigue  limit  which  corresponds
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