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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    Title :

    Striated nozzle flow with small radius of curvature ratio throats


    Contributors:


    Publication date :

    1973-11-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English