Theses and Dissertations
The effect of varying secondary Mach number and injection angle on secondary gaseous injection into a supersonic flow.
The Effect of Stagnation Temperature and Molecular Weight Variation on Gaseous Injection Into A Supersonic Stream.
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Advisor
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Collins, Daniel J. (2)
Author
Branch Of Service
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Lieutenant, United States Navy (2)
Date Issued
Degree
Department
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Aeronautical Engineering (2)