Technical Papers
Apr 15, 2014

Ballistic Impact Testing of Aluminum 2024 and Titanium 6Al-4V for Material Model Development

Publication: Journal of Aerospace Engineering
Volume 27, Issue 3

Abstract

Ballistic impact testing was conducted on aluminum (Al) 2024 and titanium (Ti) 6Al-4Vanadium (V) sheet and plate samples of different thicknesses. The tests were conducted on flat panels with two different areal dimensions: 61×61cm (24×24in.) (large panel) and 38×38cm (15×15in.) (small panel), with projectile velocities between 150and300m/s (500and1,000ft/s). The smaller panels were impacted in a normal direction with cylindrical projectiles ranging in diameter from 1.27 cm to 1.91 cm (0.5 to 0.75 in.). The larger panels involved a more complex projectile, with some features representing those of real turbine engine fan blades, impacting the panel in an oblique orientation. For the large panels, data are reported on the impact velocity and whether the projectile penetrated the panel; for the small panels, data are reported on the residual velocities. For thick panels, friction between the projectile and the panel as the projectile translated through the panel appear to play a large role in penetration. Projectile hardness affects the penetration velocity. The data presented here provide a useful tool for developing and validating impact models.

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References

Anderson, C. E., Jr., Hohler, V., Walker, J. D., and Stilp, A. J. (1999). “The influence of projectile hardness on ballistic performance.” Int. J. Impact Eng., 22(6), 619–632.
Forrestal, M. J., and Piekutowski, A. J. (2000). “Penetration experiments with 6061-T6511 aluminum targets and spherical-nose steel projectiles at striking velocities between 0.5and3.0km/s.” Int. J. Impact Eng., 24(1), 57–67.
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Pereira, J. M., Revilock, D. M., Lerch, B. A., and Ruggeri, C. R. (2013). “Impact testing of aluminum 2024 and titanium 6AL-4V for material model development.” NASA/TM-2013-217869, National Aeronautics and Space Administration (NASA), Washington, DC.
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Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 27Issue 3May 2014
Pages: 456 - 465

History

Received: Feb 5, 2013
Accepted: May 29, 2013
Published online: Apr 15, 2014
Published in print: May 1, 2014

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Authors

Affiliations

J. Michael Pereira [email protected]
Research Aerospace Engineer, National Aeronautics and Space Administration Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135 (corresponding author). E-mail: [email protected]
Duane M. Revilock [email protected]
Aerospace Engineer, National Aeronautics and Space Administration Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135. E-mail: [email protected]
Charles R. Ruggeri [email protected]
Aerospace Engineer, National Aeronautics and Space Administration Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135. E-mail: [email protected]
William C. Emmerling [email protected]
General Engineer, ANG-E231 Structures and Materials Section, Federal Aviation Administration William J. Hughes Technical Center, Bldg. 292, Atlantic City International Airport, Atlantic City, NJ 08405. E-mail: [email protected]
Donald J. Altobelli
Retired, Federal Aviation Administration William J. Hughes Technical Center, Bldg. 292, Atlantic City International Airport, Atlantic City, NJ 08405.

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