Theses and Dissertations
The effects of nozzle geometry on particle size distribution in a small two dimensional rocket motor
The use of a microcomputer system as an aid to classical and digital control system design and analysis.
Finite element program for calculating flows in turbomachines with results for NASA Task-1 compressor
Automatic control and data acquisition system for combustion laboratory applications.
A study of state rate feedback implicit model following control for VSTOL aircraft.
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Lieutenant, United States Navy (5)
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Aeronautical Engineering (5)