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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    Titel :

    Class of de Laval Nozzles


    Weitere Titelangaben:

    Class of de Laval Nozzles


    Beteiligte:


    Erscheinungsdatum :

    1949


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    A Class of De Laval Nozzles

    Falkovich, S. V. | NTRS | 1949


    A class of de Laval nozzles

    Falkovich, S. V. | TIBKAT | 1949


    Minimum Length Axisymmetric Laval Nozzles

    LUCIAN Z. DUMIRESCU | AIAA | 1975


    Investigation of Two-Phase Laval Nozzles

    I. T. Aladyev | NTIS | 1968


    Cryogenic homogeneous two-phase flows in choked Laval nozzles

    Akmandor, I. / Nagashima, Toshio | AIAA | 1998