Influence of loading distribution on the performance of high pressure turbine blades

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Creator: 

Corriveau, Daniel

Date: 

2005

Subject: 

Gas turbines -- Blades -- Testing.
Boundary layer -- Mathematics.
Reynolds number.
Mach number.
Turbines -- Aerodynamics.

Language: 

English

Publisher: 

Carleton University

Thesis Degree Name: 

Doctor of Philosophy: 
Ph.D.

Thesis Degree Level: 

Doctoral

Thesis Degree Discipline: 

Engineering, Mechanical and Aerospace

Parent Collection: 

Theses and Dissertations

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