Effects of shock wave passing on turbine blade heat transfer in a transonic turbine cascade

The effects of a shock wave passing through a blade passage on surface heat transfer to turbine blades were measured experimentally. The experiments were performed in a transonic linear cascade which matched engine Reynolds number, Mach number, and shock strength. Unsteady heat flux measurements wer...

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Bibliographic Details
Main Author: Nix, Andrew Carl
Other Authors: Mechanical Engineering
Format: Others
Language:en
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/44360
http://scholar.lib.vt.edu/theses/available/etd-08222008-063734/