Study of irrotational adiabatic motion of gas in transition from subsonic to supersonic velocities; shape of de Laval nozzle given, which transforms homogeneous planeparallel flow at large subsonic velocity into supersonic flow without any shock beyond transition line from subsonic to supersonic regions of flow. English translation from Prikladnaia Matematika i Mekhanika v 11 1947.
Class of de Laval Nozzles
Class of de Laval Nozzles
1949
15 pages
Report
English
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NTRS | 1949
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