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

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dc.contributor.advisorHassan Hassan, Co-Chair
dc.contributor.advisorPeter Gnoffo, Co-Chair
dc.contributor.advisorJack Edwards, Member
dc.contributor.advisorJohn Griggs, Graduate School Representative
dc.contributor.advisorHong Luo, Member
dc.contributor.authorThompson, Kyle Bonner
dc.date.accepted2017-03-28
dc.date.accessioned2017-04-01T12:32:40Z
dc.date.available2017-04-01T12:32:40Z
dc.date.defense2017-03-17
dc.date.issued2017-03-17
dc.date.released2017-04-01
dc.date.reviewed2017-03-23
dc.date.submitted2017-03-17
dc.degree.disciplineAerospace Engineering
dc.degree.leveldissertation
dc.degree.nameDoctor of Philosophy
dc.identifier.otherdeg6174
dc.identifier.urihttp://www.lib.ncsu.edu/resolver/1840.20/33558
dc.rights
dc.titleAerothermodynamic Design Sensitivities for a Reacting Gas Flow Solver on an Unstructured Mesh Using a Discrete Adjoint Formulation.

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