H George Krull, William T Beale
Abstract
An evaluation of the internal performance characteristics of short nozzles designed by the method of characteristics was obtained over a range of nozzle pressure ratios from 1.5 to 22.
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An evaluation of the internal performance characteristics of short nozzles designed by the method of characteristics was obtained over a range of nozzle pressure ratios from 1.5 to 22.
Key concepts: Nozzle, Thrust, Conical surface, Discharge coefficient, Mechanics, Reduction (mathematics), Expansion ratio, Materials science