Channel Based Internal Cooling of Gas Turbine Blade Leading Edge Utilizing Crossover Jets Incorporating Effects of Turbine Rotation.

Simple item page
dc.contributor.advisorSrinath Ekkad, Chair
dc.contributor.advisorGregory Buckner, Member
dc.contributor.advisorChi-An Yeh, Member
dc.contributor.authorPadachh, Het Deepak
dc.date.accepted2023-06-19
dc.date.accessioned2023-06-21T12:30:26Z
dc.date.available2023-06-21T12:30:26Z
dc.date.defense2023-04-19
dc.date.issued2023-04-19
dc.date.released2023-06-21
dc.date.reviewed2023-04-27
dc.date.submitted2023-04-22
dc.degree.disciplineMechanical Engineering
dc.degree.levelthesis
dc.degree.nameMaster of Science
dc.identifier.otherdeg33263
dc.identifier.urihttps://www.lib.ncsu.edu/resolver/1840.20/41030
dc.titleChannel Based Internal Cooling of Gas Turbine Blade Leading Edge Utilizing Crossover Jets Incorporating Effects of Turbine Rotation.

Files

Original bundle

Now showing 1 - 1 of 1
No Thumbnail Available
Name:
etd.pdf
Size:
5.89 MB
Format:
Adobe Portable Document Format
Download

Collections

Theses