Title:
Shock-compression of Ni-Al nanolayered foils using controlled laser-accelerated thin foil impact

dc.contributor.advisor Thadhani, Naresh N.
dc.contributor.author Kelly, Sean Christopher
dc.contributor.committeeMember Jang, Seung Soon
dc.contributor.committeeMember Gokhale, Arun M.
dc.contributor.committeeMember Jordan, Jennifer
dc.contributor.committeeMember Hanagud, Sathya
dc.contributor.committeeMember Kelly, Sean Christopher
dc.contributor.department Materials Science and Engineering
dc.date.accessioned 2014-01-13T16:22:31Z
dc.date.available 2014-01-13T16:22:31Z
dc.date.created 2013-12
dc.date.issued 2013-08-30
dc.date.submitted December 2013
dc.date.updated 2014-01-13T16:22:31Z
dc.description.abstract A laser-driven flyer impact system was constructed, characterized, and validated for performing uniaxial-strain experiments to investigate the shock equation-of-state (EOS) and processes leading to reaction initiation in thin, fully-dense Ni-Al nanolayered foils. Additionally, various fully-dense Ni-Al mixtures with highly heterogeneous microstructures and widely varying length scales were investigated to understand influence of meso-scale features on the shock compression and reaction response. Ni-Al composites are a class of reactive materials also called Structural Energetic Materials (SEMs), which aim to combine stiffness and strength with the ability to release large amounts of energy through highly exothermic reactions when the constituents are intimately mixed during shock loading. While porous reactive materials have been studied extensively, the processes leading to reaction initiation in fully-dense mixtures consisting of phases with disparate mechanical properties is more ambiguous. A table-top, small-scale laser system was developed for studying shock-induced effects in extremely thin reactive materials. Laser accelerated thin foil impact experiments utilizing time-resolved interferometry allowed for measuring the Hugoniot of the nanolayered Ni-Al foil over a range of particle velocities/pressures. Separate recovery experiments were performed by shock-loading Ni-Al foils slightly below the reaction initiation threshold and performing post-mortem TEM/STEM analysis to identify the constituent mixing processes leading to reaction. Direct-shock experiments were performed on the different fully-dense Ni-Al mixtures and hydrodynamic simulations using real microstructures allowed direct correlations with the experiment results, which yielded an improved understanding of the effect of phase arrangement on the shock propagation and reaction initiation response. The EOS experiments performed at particle velocities > 200 m/s showed a deviation from the predicted inert trend and recovered targets showed complete reaction to the B2-NiAl intermetallic phase. The measured deviation from inert behavior and state of recovered material suggests the occurrence of a shock-induced chemical reaction. The shocked (but unreacted) Ni-Al materials contained distinct constituent mixing features (layer jets and intermixed zones), where significant elemental penetration occurred and are likely sources of reaction initiation. The observed results provide the first clear evidence of shock-induced reactions in fully-dense nanolayered Ni-Al foils.
dc.description.degree Ph.D.
dc.format.mimetype application/pdf
dc.identifier.uri http://hdl.handle.net/1853/50288
dc.language.iso en_US
dc.publisher Georgia Institute of Technology
dc.subject Shock compression
dc.subject Nanolayered foils
dc.subject Hugoniot
dc.subject Laser flyer system
dc.subject Ni-Al composites
dc.subject.lcsh Metal foils
dc.subject.lcsh Nanostructured materials
dc.subject.lcsh Nickel-aluminum alloys
dc.subject.lcsh Shock (Mechanics)
dc.title Shock-compression of Ni-Al nanolayered foils using controlled laser-accelerated thin foil impact
dc.type Text
dc.type.genre Dissertation
dspace.entity.type Publication
local.contributor.advisor Thadhani, Naresh N.
local.contributor.corporatename School of Materials Science and Engineering
local.contributor.corporatename College of Engineering
relation.isAdvisorOfPublication ec14adca-203a-4973-b6ac-65dab1b1f44d
relation.isOrgUnitOfPublication 21b5a45b-0b8a-4b69-a36b-6556f8426a35
relation.isOrgUnitOfPublication 7c022d60-21d5-497c-b552-95e489a06569
thesis.degree.level Doctoral
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