For several years, the Air Force has been engaged in the development of high velocity air to surface missiles to defeat hard targets, such as concrete, sand, and soil. The objective is to replace larger, high mass weapons with smaller, more versatile projectiles that can achieve the same goals. The reduction of mass requires that the impact velocity be increased to meet the performance requirements. This has presented researchers with several challenges. First, the steel must be such that it survives the initial shock at impact. Second, because the travel distance in the target is long, the material must resist friction and wear, which could erode the projectile nose, thereby degrading performance. The purpose of this paper is to present the results of dynamic testing of an experimental high-strength steel, also called Eglin steel. Using a one-dimensional model for the Taylor cylinder test, the constitutive behavior of the steel as a function of strain and strain rate can be assessed through a strain rate of roughly 105s. This behavior is consistent with that required for successful modeling of the response of a penetrator casing in the ultra-ordinance velocity range.

1.
Taylor
,
G. I.
, 1948, “
The Use of Flat-Ended Projectiles for Determining Dynamic Yield Stress: I. Theoretical Considerations
,”
Proc. R. Soc. London, Ser. A
1364-5021,
194
, pp.
289
299
.
2.
Jones
,
S. E.
,
Maudlin
,
P. J.
,
Gillis
,
P.
, and
Foster
,
J. C.
, Jr.
, 1992, “
An Analytical Interpretation of High Strain Rate Material Behavior During Early Time Plastic Deformation in the Taylor Impact Test
,”
Proceedings of the 1992 ASME Computers in Engineering Conference and Exposition
,
San Francisco
,
CA
, Vol.
2
, p.
173
.
3.
House
,
J. W.
, 1989, “
Taylor Impact Testing
,” Technical Report No. AFATL-TR-89–41.
4.
Jones
,
S. E.
,
Barkey
,
M.
,
Rule
,
W. K.
, and
Huber
,
E.
, 1996, “
Mechanical Characterization of Hardened Astralloy-V® Using the Taylor Impact Test
,” Technical Paper No. AIAA-96–4294, pp.
1
8
.
5.
Barenblatt
,
G. I.
, and
Ishlinskii
,
A. I.
, 1962, “
On the Impact of a Visco-Plastic Bar on a Rigid Obstacle
,”
J. Appl. Math. Mech.
0021-8928,
26
(
3
), pp.
740
748
.
6.
Ting
,
T. C. E.
, 1966, “
Impact of a Nonlinear Visco-Plastic Rod on a Rigid Wall
,”
ASME J. Appl. Mech.
0021-8936,
33
, pp.
505
513
.
7.
Hawkyard
,
J. B.
,
Eaton
,
D.
, and
Johnson
,
W.
, 1968, “
The Mean Dynamic Yield Strength of Copper and Low Carbon Steel at Elevated Temperatures From Measurements of the ‘Mushrooming’ of Flat-Ended Projectiles
,”
Int. J. Mech. Sci.
0020-7403,
10
, pp.
929
930
.
8.
Hawkyard
,
J. B.
, 1969, “
A Theory for the Mushrooming of Flat-Ended Projectiles Impinging on a Flat Rigid Anvil, Using Energy Considerations
,”
Int. J. Mech. Sci.
0020-7403,
11
, pp.
313
324
.
9.
Jones
,
S. E.
,
Gillis
,
P. P.
, and
Foster
,
J. C.
, Jr.
, 1987, “
On the Equation of Motion of the Undeformed Section of a Taylor Specimen
,”
J. Appl. Phys.
0021-8979,
61
(
2
), pp.
499
502
.
10.
Jones
,
S. E.
,
Drinkard
,
J. A.
,
Rule
,
W. K.
, and
Wilson
,
L. L.
, 1998, “
An Elementary Theory for the Taylor Impact Test
,”
Int. J. Impact Eng.
0734-743X,
21
, pp.
1
13
.
11.
Jones
,
S. E.
,
Maudlin
,
P. J.
, and
Foster
,
J. C.
, Jr.
, 1995, “
Constitutive Modeling Using the Taylor Impact Test
,”
High Strain Rate Effects on Polymer, Metal and Ceramic Matrix Composites and Other Advanced Materials, 1995 ASME International Mechanical Engineering Congress and Exposition
,
Y. D. S.
Rajapakse
, and
J. R.
Vinson
, eds.,
San Francisco
,
CA
.
12.
Stevenson
,
M. E.
,
Jones
,
S. E.
, and
Bradt
,
R. C.
, 2003, “
The High Strain Rate Dynamic Stress-Strain Curve for OFHC Copper
,”
Mater. Sci. Res. Int.
1341-1683,
9
(
3
), pp.
187
195
.
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