An investigation on the effects of the high maximum-thickness-to- chord ratio on the performance of nozzle guide vanes in a transonic planar cascade.

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Creator: 

Radmard, Rama

Date: 

1993

Subject: 

Aerofoils
Turbomachines -- Aerodynamics
Turbomachines -- Computer Programs
Turbines -- Blades

Language: 

English

Publisher: 

Carleton University

Identifier: 

Proquest Record
Library Catalogue Record
https://doi.org/10.22215/etd/1993-02458

Thesis Degree Name: 

Master of Engineering: 
M.Eng.

Thesis Degree Level: 

Master's

Thesis Degree Discipline: 

Engineering, Mechanical

Parent Collection: 

Theses and Dissertations

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