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.


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    Title :

    Class of de Laval Nozzles


    Additional title:

    Class of de Laval Nozzles


    Contributors:


    Publication date :

    1949


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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