Technical Papers
Feb 3, 2011

Development and Investigation of a Slotted Beam Impact Experiment for Intermediate Strain Rates

Publication: Journal of Aerospace Engineering
Volume 25, Issue 2

Abstract

Quantifying the strain rate–sensitive mechanical properties of structural materials is an important area of research in the field of solid mechanics. Property evaluation is typically accomplished using dynamic tests that involve rapid loading or impact of specimens. These tests generate inertial forces and wave propagation, which make it difficult to accurately record the material response to a loading condition at an equivalent location. Furthermore, dynamic impact tests typically generate high strain rates (in excess of 103s-1) and an experimental method for generating rates of strain in the intermediate strain rate regime that is simple and reliable is still lacking. This research develops and investigates an experimental technique for generating tensile plastic strain rates up to 102s-1 in ductile metals. The technique relies on the impact from a vertical drop weight machine capable of delivering suitable impact velocity and energy to globally deform a slotted beam specimen. At impact, a state of predominantly plastic uniaxial tensile stress is created in the ligament beneath the slot. The ligament is instrumented with an electrical resistance strain gauge, and the strain history is measured and stored in a digital oscilloscope. Experiments are conducted on commercially pure (CP) titanium, 2024-T3 aluminum, and 1018 steel samples at four distinct impact velocities, and collected data illustrate the capability to create predominantly uniaxial tensile strain rates up to 102s-1. An analysis of the material response identifies where plastic flow initiates. Furthermore, a numerical analysis of the impact event is conducted where the Johnson-Cook constitutive equation is assumed to reflect the material behavior and published parameters are utilized to illustrate good agreement between experimental strain data and the numerical model.

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Acknowledgments

The views expressed in this article are those of the authors and do not reflect the official policy or position of the U.S. Air Force, Department of Defense, or the U.S. government. This work was funded by the U.S. Air Force Research Laboratory, Structural Science Center. The authors would like to acknowledge Brian Smyers and Brett Hauber of AFRL/RBS and Kevin Poormon of University of Dayton Research Institute for their help in this effort.

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Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 25Issue 2April 2012
Pages: 294 - 307

History

Received: May 7, 2010
Accepted: Feb 1, 2011
Published online: Feb 3, 2011
Published in print: Apr 1, 2012

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Authors

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Hugh E. Gardenier IV [email protected]
Air Force Institute of Technology, 2950 Hobson Way, Wright-Patterson AFB, OH 45431 (corresponding author). E-mail: [email protected]
Anthony N. Palazotto, Ph.D., F.ASCE
P.E.
Air Force Institute of Technology, 2950 Hobson Way, Wright-Patterson AFB, OH 45431.
Reid A. Larson, Ph.D.
P.E.
Air Force Institute of Technology, 2950 Hobson Way, Wright-Patterson AFB, OH 45431.

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