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Influence of Stress State on the Ductile Fracture of Ti-6Al-4V

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Abstract

The ductile fracture behavior of Ti-6Al-4V is investigated experimentally. The objective of the test program is to generate experimental data that can be used to calibrate a failure model for numerical simulations. Various stress states are achieved by conducting mechanical tests on multiple sample geometries subjected to several different loading conditions. Tension tests are conducted on thin flat specimens, thick flat specimens and axisymmetric specimens with varying notch radii. In addition, thin walled tube specimens are subjected to combined axial-torsional loading. Digital image correlation is used to measure specimen surface strain for all experiments. Parallel LS-DYNA simulations are used to determine the stress states and fracture strains for tension tests. A fracture locus for Ti-6Al-4V is created in the stress triaxiality and Lode parameter stress space. The results show that the stress triaxiality alone is unable to properly capture the failure characteristics Ti-6Al-4V.

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Acknowledgements

The research was supported by the U.S.A. Federal Aviation Administration. The authors would like to thank William Emmerling, Donald Altobelli and Chip Queitzsch of the FAA.

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Correspondence to J. D. Seidt .

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© 2014 The Society for Experimental Mechanics

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Hammer, J.T., Seidt, J.D., Gilat, A. (2014). Influence of Stress State on the Ductile Fracture of Ti-6Al-4V. In: Jay, C. (eds) Fracture and Fatigue, Volume 7. Conference Proceedings of the Society for Experimental Mechanics Series. Springer, Cham. https://doi.org/10.1007/978-3-319-00765-6_13

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  • DOI: https://doi.org/10.1007/978-3-319-00765-6_13

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-00764-9

  • Online ISBN: 978-3-319-00765-6

  • eBook Packages: EngineeringEngineering (R0)

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