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ne Environment Effect on Fatigue Crack Gmwth Rates in  7049 Aluminium Alloy at ...   311


            CONCLUSIONS
            The fatigue crack growth threshold behaviour of an A1 7049 (UA-OA)  alloy was studied by
            comparing differently aged materials with identical chemical composition and yield strength,
            but  different microstructure. These two alloys exhibit the same crystallographic texture and
            grain morphology, but differ in precipitate microstructure. Experiments at different R-ratios
            and different environment (ambient air and vacuum)  showed that thresholds depend on the
            different microstructure and the associated deformation mechanisms. These are homogeneous
            slip in the overaged (OA) condition and localised slip with crystallographic cracking and  a
            tendency to crack branching in the underaged (UA) material. The microstructural differences
            manifested in terms of planar vs. wavy slip, indicate that the resistance to crack growth in the
            planar slip alloy is  significantly higher than  that  of  the  overaged  alloy  (OA)  due to  the
            contributions from crack branching and environment  in the tension-tension load region. In the
            compression-tension region, the underaged alloy shows a loss in the fatigue resistance, which
            is probably caused by a change in the slip and fracture modes.  The second most important
            influence comes from the  environment. It shows that  the threshold cyclic stress intensity
            factor is reduced by approximately 50%  probably mainly by hydrogen embrittlement. The
            overall behaviour is due to the complex relationship between the effect of environment with
            microstructure and loading. The key to the understanding such complex mechanisms lies in
            quantifying the  role  of  crack  tip  chemistry  and  decoupling the  role  of  time  dependent
            environmental effects on  crack  growth  from  the  cycle  dependent  fatigue  loading.  Such
            understanding  is only possible through careful systematic measurements of fatigue data under
            high vacuum  and  in the selected environments. The parameters C and  m of the Paris  law,
            traditionally considered as a specific property of the material, significantly differ for  each
            microstructure and environment.

            REFERENCES

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