Aerothermodynamic Design Sensitivities for a Reacting Gas Flow Solver on an Unstructured Mesh Using a Discrete Adjoint Formulation.

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dc.contributor.advisor Hassan Hassan, Co-Chair
dc.contributor.advisor Peter Gnoffo, Co-Chair
dc.contributor.advisor Jack Edwards, Member
dc.contributor.advisor John Griggs, Graduate School Representative
dc.contributor.advisor Hong Luo, Member
dc.contributor.author Thompson, Kyle Bonner
dc.date.accessioned 2017-04-01T12:32:40Z
dc.date.available 2017-04-01T12:32:40Z
dc.date.issued 2017-03-17
dc.date.submitted 2017-03-17
dc.identifier.other deg6174
dc.identifier.uri http://www.lib.ncsu.edu/resolver/1840.20/33558
dc.rights
dc.title Aerothermodynamic Design Sensitivities for a Reacting Gas Flow Solver on an Unstructured Mesh Using a Discrete Adjoint Formulation.
dc.degree.name Doctor of Philosophy
dc.degree.level dissertation
dc.degree.discipline Aerospace Engineering
dc.date.accepted 2017-03-28
dc.date.defense 2017-03-17
dc.date.released 2017-04-01
dc.date.reviewed 2017-03-23


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