Issue |
EPJ Web of Conferences
Volume 26, 2012
DYMAT 2012 - 10th International Conference on the Mechanical and Physical Behaviour of Materials under Dynamic Loading
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Article Number | 04017 | |
Number of page(s) | 4 | |
Section | Modeling and Numerical Simulation | |
DOI | https://doi.org/10.1051/epjconf/20122604017 | |
Published online | 31 August 2012 |
https://doi.org/10.1051/epjconf/20122604017
Constitutive equations of a ballistic steel alloy as a function of temperature
1 Royal Military Academy, Department of Civil and Material Engineering, 1000 Brussels, Belgium
2 Royal Military Academy, Department of Weapon Systems and Ballistics, 1000 Brussels, Belgium
In the present work, dynamic tests have been performed on a new ballistic steel alloy by means of split Hopkinson pressure bars (SHPB). The impact behavior was investigated for strain rates ranging from 1000 to 2500 s−1, and temperatures in the range from − 196 to 300∘C. A robotized sample device was developed for transferring the sample from the heating or cooling device to the position between the bars. Simulations of the temperature evolution and its distribution in the specimen were performed using the finite element method. Measurements with thermocouples added inside the sample were carried out in order to validate the FEM simulations. The results show that a thermal gradient is present inside the sample; the average temperature loss during the manipulation of the sample is evaluated. In a last stage, optimal material constants for different constitutive models (Johnson-Cook, Zerilli-Amstrong, Cowper-Symonds) has been computed by fitting, in a least square sense, the numerical and experimental stress-strain curves. They have been implemented in a hydrocode for validation using a simple impact problem: an adapted projectile geometry with a truncated nose (.50 calibre fragment simulating projectiles) was fired directly against an armor plate. The parameters of the selected strength and failure models were determined. There is a good correspondence between the experimental and computed results. Nevertheless, an improved failure model is necessary to get satisfactory computed residual projectile velocities.
© Owned by the authors, published by EDP Sciences, 2012
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