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Williams-2014-On the shock stress, substructur
On the shock stress, substructure evolution, and spall response
of commercially pure 1100-O aluminum
C.L. Williams a,n, C.Q. Chen b, K.T. Ramesh b, D.P. Dandekar a
a U.S. Army Research Laboratory, Aberdeen Proving Ground, MD 21005-5066, USA
b The Johns Hopkins University, Baltimore, MD 21218-2681, USA
a r t i c l e i n f o
Article history:
Received 1 July 2014
Received in revised form
3 September 2014
Accepted 5 September 2014
Available online 16 September 2014
Keywords:
Shock stress
Shock hardening
Dynamic recovery
Substructure
Evolution
Recovery
a b s t r a c t
Plate impact shock and spall recovery experiments were conducted to study the effects of peak shock
stress on the substructure evolution and spall response of fully annealed 1100 aluminum. The
substructure of the material evolves substantially with increase in peak shock stress ranging from
4 GPa to 9 GPa with dislocation debris uniformly distributed throughout the interior of the subgrain.
Observations from substructure evolution in conjunction with spall failure results suggest that ductile
fracture by void nucleation, growth, and coalescence was perhaps the dominant fracture mode for shock
stresses up to approximately 8.3 GPa. Whereas, beyond 8.3 GPa the material softened possibly due to
dislocation reorganization (dynamic recovery) and brittle intergranular fracture by decohesion with
isolated pockets of nanovoids was perhaps the dominant fracture mode. The contributions of nanovoids
to the dynamic recovery process, if any, were unresolved. Microhardness measurements show an
increase in residual hardness throughout the shock stress range studied implying shock hardening up to
approximately 8.3 GPa. This observation also suggests that thermal softening was not operative
throughout the shock stress range studied. However, dynamic recovery was thermally influenced during
shock loading.
Published by Elsevier B.V.
1. Introduction
Aluminum alloys such as the 2xxx, 5xxx, and 7xxx series are
widely used in appl
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