Alumina-filled epoxies are composites having constituents with highly dissimilar mechanical properties. Complex behavior during shock compression and release can result, particularly at higher alumina loadings. In the current study, a particular material containing 43% alumina by volume was examined in planar-impact experiments. Laser interferometry was used to measure particle velocity histories in both reverse-impact and transmitted-wave configurations. Hugoniot states and release-wave velocities were obtained at shock stresses up to 10GPa, and represented smooth extensions of previous data at lower stresses. Surprisingly high release-wave velocities continued to be the most notable feature. Measured profiles of transmitted waves show a gradual transition from viscoelastic behavior at high shock stresses to a more complex behavior at lower stresses in which viscous mechanisms produce a broadened wave structure. This wave structure was examined in some detail for peak stress dependence, evolution towards steady-wave conditions, and initial temperature effects.

1.
For example, see papers in
Shock Compression of Condensed Matter-2001
, edited by
M. D.
Furnish
,
N. N.
Thadhani
, and
Y.
Horie
(
American Institute of Physics
, Melville, NY,
2002
), and in earlier proceedings of this biennial conference.
2.
D. E.
Munson
,
R. R.
Boade
, and
K. W.
Schuler
,
J. Appl. Phys.
49
,
4797
(
1978
).
3.
D. E.
Munson
and
K. W.
Schuler
,
J. Compos. Mater.
5
,
286
(
1971
).
4.
L. C.
Chhabildas
and
J. W.
Swegle
,
J. Appl. Phys.
53
,
954
(
1982
).
5.
L. M.
Lee
,
B. D.
Jenrette
, and
A.
Greb
, Air Force Weapons Laboratory Report AFWL-TR-87-133,
1987
(unpublished).
6.
L. M.
Barker
,
J. Compos. Mater.
5
,
140
(
1971
).
7.
D. S.
Drumheller
,
J. Appl. Phys.
53
,
957
(
1982
).
8.
A product of Resolution Performance Products.
9.
Previously available from Shell Chemical Company.
10.
Ground T-64 tabular alumina (325 mesh) from Alcoa Industrial Chemicals Division.
11.
J. H.
Gieske
and
S. J.
Younghouse
, Sandia National Laboratories (private communication).
12.
H. J.
Sutherland
,
J. Compos. Mater.
13
,
35
(
1979
).
13.
L. M.
Barker
and
R. E.
Hollenbach
,
J. Appl. Phys.
43
,
4669
(
1972
).
14.
R. E.
Setchell
,
J. Appl. Phys.
91
,
2833
(
2002
).
15.
R. E.
Setchell
,
J. Appl. Phys.
50
,
8186
(
1979
).
16.
L. M.
Barker
and
R. E.
Hollenbach
,
J. Appl. Phys.
41
,
4208
(
1970
).
17.
R. A.
Graham
and
W. P.
Brooks
,
J. Phys. Chem. Solids
32
,
2311
(
1971
).
18.
PVDF shock sensors from Ktech Corporation, Albuquerque, NM.
19.

The steady-shock velocity, or Hugoniot shock velocity, is defined by the conservation relation for a steady shock wave: Us=σHρ0uH, where σH and uH identify a stress-velocity point on the Hugoniot curve and ρ0 is initial density. Although unsteady evolution occurs in ALOX wave profiles, the motion of the half-maximum point on wave profiles appears to be nearly steady and accurately represented by the Hugoniot shock velocity (Sec. III). The rise time to the half-maximum point becomes very small at higher shock pressures (Fig. 6).

20.
R. A.
Graham
, Sandia National Laboratories (private communication).
21.
K. W.
Schuler
,
J. W.
Nunziato
, and
E. K.
Walsh
,
Int. J. Solids Struct.
9
,
1237
(
1973
).
22.
L.
Davison
and
R. A.
Graham
,
Phys. Rep.
55
,
255
(
1979
).
23.
J. W.
Swegle
and
D. E.
Grady
,
J. Appl. Phys.
58
,
692
(
1985
).
24.
D. R.
Bland
,
J. Inst. Math. Appl.
1
,
56
(
1965
).
25.
V. F.
Nesterenko
, University of California at San Diego (private communication).
26.
H. J.
Sutherland
,
J. Appl. Phys.
49
,
3941
(
1978
).
27.
D.
Adolf
,
C.
Childress
, and
D.
Hannum
, Sandia National Laboratories Report SAND89-0748,
1989
.
28.
M. U.
Anderson
,
R. E.
Setchell
, and
D. E.
Cox
, in
Shock Compression of Condensed Matter-2001
, edited by
M. D.
Furnish
,
N. N.
Thadhani
, and
Y.
Horie
(
American Institute of Physics
, Melville, NY,
2002
), p.
669
.
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