Evaluation of Complex Cooling Geometries with Jet Impingement and Effusion for Gas Turbine Combustor Liners.

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dc.contributor.advisorSrinath Ekkad, Chair
dc.contributor.advisorRichard Gould, Member
dc.contributor.advisorAlexei Saveliev, Member
dc.contributor.advisorTiegang Fang, Member
dc.contributor.advisorJoel Ducoste, Member
dc.contributor.authorBonds, Michael Andrew
dc.date.accepted2022-11-02
dc.date.accessioned2022-11-04T12:30:23Z
dc.date.available2022-11-04T12:30:23Z
dc.date.defense2022-10-25
dc.date.issued2022-10-25
dc.date.released2022-11-04
dc.date.reviewed2022-10-28
dc.date.submitted2022-10-28
dc.degree.disciplineAerospace Engineering
dc.degree.leveldissertation
dc.degree.nameDoctor of Philosophy
dc.identifier.otherdeg31294
dc.identifier.urihttps://www.lib.ncsu.edu/resolver/1840.20/40078
dc.titleEvaluation of Complex Cooling Geometries with Jet Impingement and Effusion for Gas Turbine Combustor Liners.

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