Abstract
Unloading wave experiments were used to determine the material strength and release adiabats in pure and 6061-T6 aluminum alloy over the stress range of 50–100 GPa. The experimental adiabats are in good agreement with theoretical calculations, assuming a constant ργ. The strength measurements show that a maximum occurs for shock states above 20 GPa and that a general softening of the strength is evident between 40 and 100 GPa.
This work performed by Sandia National Laboratories supported by the U. S. Department of Energy under contract #DEAC04-76-DP00789.
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© 1986 Plenum Press, New York
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Asay, J.R., Chhabildas, L.C., Kerley, G.I., Trucano, T.G. (1986). High Pressure Strength of Shocked Aluminum. In: Gupta, Y.M. (eds) Shock Waves in Condensed Matter. Springer, Boston, MA. https://doi.org/10.1007/978-1-4613-2207-8_16
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DOI: https://doi.org/10.1007/978-1-4613-2207-8_16
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