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BiaxiaVMultiaxial Fatigue and Fracture
          Andrea Carpinten, Manuel de Freitas and Andrea Spagnoli (EMS.)
          0 Elsevier Science Ltd. and ESIS.  All rights reserved.              483








              GEOMETRY VARIATION AND LIFE ESTIMATES OF BIAXIAL FATIGUE
                                         SPECIMENS


                                  Giora SHATIL and Nuri ERSOY
                                 Structural Zntegrity Group, CEMS,
                 University of the West of England, Frenchay Campus, Bristol BS16 IQX  UK





          ABSTRACT
          Results are reported from an  investigation into the geometrical aspects of  multiaxial fatigue
          using a newly developed method for testing of rhombic specimens. The new method is used to
          obtain biaxial stress by applying simultaneously reversed tension and compression bending in
          perpendicular directions to a rectangular plate (anticlastic bending). Constant-load amplitude
          fatigue tests of aluminium alloy 2024 T351 specimens were conducted at several load levels.
          The specimen’s critical surface and subsurface strains and stresses were evaluated by using a
          3D  elastic-plastic  finite  element  analysis  (ITA).  Results  from  the  numerical  simulation
          indicated  that  the  critical  maximum  shear  strain  plane  is  both  geometrically  and  loading
          dependent. A fair predtction of the specimens’ life is obtained by using the material data, the
          simulated maximum shear strains and a subsurface strain damage model. The experimental and
          the predicted results are discussed, and further development of the subsurface strain model is
          presented.
          KEYWORDS

          Subsurface strain, geometrical aspects, anticlastic bending, critical plane, aluminium alloy.


          INTRODUCTION

          Previous experimental work has used different geometries to show that, even for the same state
          of surface stress or strain, a difference in life could arise between specimens. Some examples
          are the comparisons between pure bending and torsion tests  [I] and between thin and thick
          walled specimens under torsion  [2]. Previously, biaxial fatigue results of  hollow thin walled
          specimens were compared to solid bar results using a multiaxial fatigue strain parameter [3],
          and it was shown that the life of thin walled specimens were approximately three to five times
          shorter than those of solid bars [4].
            The geometrical aspect has been considered in the past by using several models, for example
          by  introducing  a  triaxiality  stress  parameter  and  a  critical  layer  stress  parameter  [5]
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