Internal Cooling of Gas Turbine Blade with High Performance Features Under High Reynolds Number Condition.

Simple item page
dc.contributor.advisorSrinath Ekkad, Chair
dc.contributor.advisorSajjad Bigham, Member
dc.contributor.advisorTim Horn, Member
dc.contributor.advisorChristopher Rock, Member
dc.contributor.authorPandya, Naimish Sanjaybhai
dc.date.accepted2025-05-27
dc.date.accessioned2025-06-18T12:30:45Z
dc.date.available2025-06-18T12:30:45Z
dc.date.defense2025-04-10
dc.date.issued2025-04-10
dc.date.released2025-06-18
dc.date.reviewed2025-04-23
dc.date.submitted2025-04-19
dc.degree.disciplineMechanical Engineering
dc.degree.leveldissertation
dc.degree.nameDoctor of Philosophy
dc.identifier.otherdeg41862
dc.identifier.urihttps://www.lib.ncsu.edu/resolver/1840.20/45442
dc.titleInternal Cooling of Gas Turbine Blade with High Performance Features Under High Reynolds Number Condition.

Files

Original bundle

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

Collections

Dissertations