Theses and Dissertations
The Effect of Stagnation Temperature and Molecular Weight Variation on Gaseous Injection Into A Supersonic Stream.
Analog simulation of automatic glide slope control using wing lift spoilers as direct lift control
An investigation of penetration and spreading for various fluids injected into a supersonic stream
An Experimental Determination of Two Dimensional Ribbed Wall Diffusor Performance
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Lieutenant, United States Navy (4)
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1968 (4)
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Aeronautical Engineering (4)