Theses and Dissertations
Measurements of the scattering matrix of obstacles in multimode wave guides.
Dynamic response testing of transient pressure transducers for liquid propellant rocket combustion chambers
Part I. Analysis of a multi-stage axial compressor with high reaction blading. Part II. A design study of a multi-stage axial compressor with blading of high aspect ratio.
Liquid hydrogen: high energy rocket fuel
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Lieutenant, United States Navy (4)
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1963 (4)
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Aeronautical Engineering (4)