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Generation of ramp waves using variable areal density flyers
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art%3A10.1007%2Fs00193-015-0558-3.pdf | Published version | 1.97 MB | Adobe PDF | View/Open |
Title: | Generation of ramp waves using variable areal density flyers |
Authors: | Winter, RE Cotton, M Harris, EJ Chapman, DJ Eakins, D |
Item Type: | Journal Article |
Abstract: | Ramp loading using graded density impactors as flyers in gas-gun-driven plate impact experiments can yield new and useful information about the equation of state and the strength properties of the loaded material. Selective Laser Melting, an additive manufacturing technique, was used to manufacture a graded density flyer, termed the “bed-of-nails” (BON). A 2.5-mm-thick ×× 99.4-mm-diameter solid disc of stainless steel formed a base for an array of tapered spikes of length 5.5 mm and spaced 1 mm apart. The two experiments to test the concept were performed at impact velocities of 900 and 1100 m/s using the 100-mm gas gun at the Institute of Shock Physics at Imperial College London. In each experiment, a BON flyer was impacted onto a copper buffer plate which helped to smooth out perturbations in the wave profile. The ramp delivered to the copper buffer was in turn transmitted to three tantalum targets of thicknesses 3, 5 and 7 mm, which were mounted in contact with the back face of the copper. Heterodyne velocimetry (Het-V) was used to measure the velocity–time history, at the back faces of the tantalum discs. The wave profiles display a smooth increase in velocity over a period of ∼2.5μs∼2.5μs , with no indication of a shock jump. The measured profiles have been analysed to generate a stress vs. volume curve for tantalum. The results have been compared with the predictions of the Sandia National Laboratories hydrocode, CTH. |
Issue Date: | 19-Feb-2015 |
Date of Acceptance: | 31-Jan-2015 |
URI: | http://hdl.handle.net/10044/1/21830 |
DOI: | http://dx.doi.org/10.1007/s00193-015-0558-3 |
ISSN: | 0938-1287 |
Publisher: | Springer Verlag |
Start Page: | 395 |
End Page: | 401 |
Journal / Book Title: | Shock Waves |
Volume: | 26 |
Issue: | 4 |
Copyright Statement: | © The Author(s) 2015. This article is distributed under the terms of the Creative Commons Attribution License which permits any use, distribution, and reproduction in any medium, provided the original author(s) and the source are credited. |
Sponsor/Funder: | AWE PLC |
Funder's Grant Number: | 30266045/0 |
Keywords: | Aerospace & Aeronautics Classical Physics |
Publication Status: | Published |
Appears in Collections: | Physics Plasma Physics Faculty of Natural Sciences |
This item is licensed under a Creative Commons License