The Stress and Strain-Rate Dependence of Spall Strength in Two Aluminum Alloys

  • Ek D
  • Asay J
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Abstract

The spallation behavior of 6061-T6 and AMg-6 aluminum alloys was studied as a function of loading stress and initial pulse duration for stress amplitudes ranging from 5-20 GPa and for pulse durations spanning the range of 0.06-0.9 p.s. These experiments show that the spallation strength varies from about 0.7-1.4 GPa for strain rates varying from 0.15-1 p.s-I and for impact stresses from 5-20 GPa.

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Ek, D. R., & Asay, J. R. (1986). The Stress and Strain-Rate Dependence of Spall Strength in Two Aluminum Alloys. In Shock Waves in Condensed Matter (pp. 413–418). Springer US. https://doi.org/10.1007/978-1-4613-2207-8_58

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