Title:
Fragmentation and reaction of structural energetic materials

dc.contributor.advisor Thadhani, Naresh N.
dc.contributor.author Aydelotte, Brady Barrus
dc.contributor.committeeMember McDowell, David L.
dc.contributor.committeeMember Gokhale, Arun M.
dc.contributor.committeeMember Zhou, Min
dc.contributor.committeeMember Homan, Barrie
dc.contributor.committeeMember Sanders, Tom
dc.contributor.department Materials Science and Engineering
dc.date.accessioned 2014-01-13T16:20:54Z
dc.date.available 2014-01-13T16:20:54Z
dc.date.created 2013-12
dc.date.issued 2013-08-20
dc.date.submitted December 2013
dc.date.updated 2014-01-13T16:20:54Z
dc.description.abstract Structural energetic materials (SEM) are a class of multicomponent materials which may react under various conditions to release energy. Fragmentation and impact induced reaction are not well characterized phenomena in SEMs. The structural energetic systems under consideration here combine aluminum with one or more of the following: nickel, tantalum, tungsten, and/or zirconium. These metal+Al systems were formulated with powders and consolidated using explosive compaction or the gas dynamic cold spray process. Fragment size distributions of the indicated metal+Al systems were explored; mean fragment sizes were found to be smaller than those from homogeneous ductile metals at comparable strain rates, posing a reduced risk to innocent bystanders if used in munitions. Extensive interface failure was observed which suggested that the interface density of these systems was an important parameter in their fragmentation. Existing fragmentation models for ductile materials did not adequately capture the fragmentation behavior of the structural energetic materials in question. A correction was suggested to modify an existing fragmentation model to expand its applicability to structural energetic materials. Fragment data demonstrated that the structural energetic materials in question provided a significant mass of combustible fragments. The potential combustion enthalpy of these fragments was shown to be significant. Impact experiments were utilized to study impact induced reaction in the indicated metal+Al SEM systems. Mesoscale parametric simulations of these experiments indicated that the topology of the microstructure constituents, particularly the stronger phase(s), played a significant role in regulating impact induced reactions. Materials in which the hard phase was topologically connected were more likely to react at a lower impact velocity due to plastic deformation induced temperature increases. When a compliant matrix surrounded stronger, simply connected particles, the compliant matrix accommodated nearly all of the deformation, which limited plastic deformation induced temperature increases in the stronger particles and reduced reactivity. Decreased difference between the strength of the constituents in the material also increased reactivity. The results presented here demonstrate that the fragmentation and reaction of metal+Al structural energetic materials are influenced by composition, microstructure topology, interface density, and constituent mechanical properties.
dc.description.degree Ph.D.
dc.format.mimetype application/pdf
dc.identifier.uri http://hdl.handle.net/1853/50253
dc.language.iso en_US
dc.publisher Georgia Institute of Technology
dc.subject Structural energetic materials
dc.subject Reactive materials
dc.subject Fragmentation
dc.subject Impact
dc.subject High strain rate
dc.subject Composite
dc.subject.lcsh Explosives
dc.subject.lcsh Propellants
dc.subject.lcsh Materials Compression testing
dc.subject.lcsh Impact
dc.title Fragmentation and reaction of structural energetic materials
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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