Abstract
Titanium alloys are widely used in aerospace, defence, automotive, and biomedical engineering owing to their high specific strength and excellent corrosion resistance. Additive manufacturing has emerged as a promising alternative to conventional production methods, offering the capability to fabricate complex geometries while reducing processing time and material waste. In this study, the high strain rate deformation behaviour of Ti6Al4V produced by selective laser melting is investigated using a Split Hopkinson Tension Bar system equipped with a multi-camera high-speed imaging setup. A comprehensive experimental programme is conducted on specimens manufactured in three different build orientations to assess the influence of processing direction on dynamic strain localisation and true stress–strain response. The post-necking behaviour is examined and compared with that of conventionally forged Ti6Al4V, revealing notable differences in ductility and strain localisation mechanisms. In addition, the high strain rate compressive behaviour of both material variants and their temperature dependence are investigated using a Split Hopkinson Compression Bar system equipped with thermal conditioning. The deformation and failure mechanisms of additively manufactured specimens produced in different orientations are further examined through post-mortem analysis of the fracture surfaces.
| Original language | English |
|---|---|
| Article number | 100228 |
| Journal | Journal of Alloys and Metallurgical Systems |
| Volume | 13 |
| Early online date | 6 Dec 2025 |
| DOIs | |
| Publication status | E-pub ahead of print - 6 Dec 2025 |
Bibliographical note
Publisher Copyright:Copyright © 2025. Published by Elsevier B.V.
Funding
The present research was conducted independently and was not associated with any specific funding. However, Antonio Pellegrino and Govind Gour would like to thank Rolls-Royce PLC and the EPSRC for their previous support under the Prosperity Partnership Grant ‘Cornerstone: Mechanical Engineering Science to Enable Aero Propulsion Futures’ (Grant Ref: EP/R004951/1). The authors would like to express their sincere gratitude to the technicians pool at the Impact Engineering Laboratory in Oxford for the manufacturing of the samples.
| Funders | Funder number |
|---|---|
| Rolls-Royce | |
| Engineering and Physical Sciences Research Council | EP/R004951/1 |
Keywords
- necking, high strain rate
- Titanium alloys
- High strain rate
- Hopkinson Bar
- Necking
- Additive manufacturing
ASJC Scopus subject areas
- Materials Science (miscellaneous)
- Surfaces, Coatings and Films
- Metals and Alloys
