Three-dimensional interaction of a swept shock wave with a turbulent boundary layer and the effects of air injection on separation.

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Creator: 

Peake, David John

Date: 

1975

Language: 

English

Publisher: 

Carleton University

Thesis Degree Name: 

Doctor of Philosophy: 
Ph.D.

Thesis Degree Level: 

Doctoral

Thesis Degree Discipline: 

Engineering, Aeronautical

Parent Collection: 

Theses and Dissertations

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