A theory is presented that makes it possible to apply one-dimensional techniques to compressible striated nozzle flow with small radius of curvature ratio throats. The throat plane solution is shown to approximate the two-dimensional axisymmetric flowfield and can be used for analyzing the throat plane in converging-diverging type nozzles with striated flow for radius of curvature throat ratios down to 0.25.


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    Titel :

    Striated nozzle flow with small radius of curvature ratio throats


    Beteiligte:
    Norton, D. J. (Autor:in) / White, R. E. (Autor:in)


    Erscheinungsdatum :

    01.11.1973


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :