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Investigation of the development of the trailing vortex system behind a swept-back wing.

Collection: Theses and Dissertations
Creator: ElRamly, Zakaria M.
Date: 1975
Degree Discipline: Engineering, Aeronautical
Degree Name: Doctor of Philosophy

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

Collection: Theses and Dissertations
Creator: Peake, David John
Date: 1975
Degree Discipline: Engineering, Aeronautical
Degree Name: Doctor of Philosophy

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