Effects of fuel nozzle condition upon gas turbine combustion chamber exit temperture profiles = effets de condition d'ajutage du carburant sur le champs de température de sortie de chambre du combustion de turbine a gaz

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Creator: 

Bishop, Kristen Marie

Date: 

2009

Subject: 

Aerospace engineering.
Mechanical engineering.

Language: 

English

Publisher: 

Carleton University

Thesis Degree Name: 

Master of Applied Science: 
M.App.Sc.

Thesis Degree Level: 

Master's

Thesis Degree Discipline: 

Engineering, Aerospace

Parent Collection: 

Theses and Dissertations

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